Garmin G1000 NXi: Beechcraft King Air 300/B300 Cockpit Reference Guide, G1000 NXi King Air 300/B300 Series - SSV 2286.01
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® Cockpit Reference Guide Beechcraft 300/B300 Series FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM (EIS) NAV/COM/TRANSPONDER/AUDIO PANEL FLIGHT MANAGEMENT SYSTEM HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES ANNUNCIATIONS & ALERTS APPENDIX INDEX Copyright © 2017 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 2286.01 or later for the Beechcraft 300 and B300. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc. 1200 East 151st Street Olathe, Kansas 66062, U.S.A. Tel: 913.397.8200 Fax: 913.397.8282 Aircraft On Ground (AOG) Hotline: 913.397.0836 Aviation Dealer Technical Support: 888.606.5482 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. Tel: 503.581.8101 Fax 503.364.2138 Garmin (Europe) Ltd. Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.K. Tel: +44 (0) 238 052 4000 Fax: +44 (0) 238 052 4004 Aviation Support: +44 (0) 370 850 1243 Garmin Corporation No. 68, Zhangshu 2nd Road Xizhi District, New Taipei City, Taiwan Tel: 34-93-357-2608 Fax: 34-93-429-4484 Website Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin®, G1000® NXi, WATCH®, FliteCharts®, and SafeTaxi® are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin ESP™, Garmin SVT™, SurfaceWatch™, and Connext™ are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Skywatch® and Stormscope® are registered trademarks of L-3 Communications. Ryan®, TCAD® and Avidyne® are registered trademarks of Avidyne Corporation. AC-U-KWIK® is a registered trademark of Penton Business Media Inc. Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc. Becker® is a registered trademark of Becker Flugfunkwerk GmbH. NavData® is a registered trademark of Jeppesen, Inc. Wi-Fi® is a 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series registered trademark of the Wi-Fi Alliance. SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc. The Bluetooth® word mark and logos are owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under license. AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you. AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to licensee. Printed in the U.S.A. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Warnings, Cautions & Notes WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot independently verify the accuracy of the information. WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical information. Displayed aeronautical data may not incorporate the latest NOTAM information. WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The primary barometric altimeter must be used for compliance with all air traffic control altitude regulations, requirements, instructions, and clearances. WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered only an aid to enhance situational awareness. WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be older than the indicated weather product age. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Warnings, Cautions & Notes WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: Always obtain qualified instruction prior to operational use of this equipment. WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable. WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. WARNING: When using the autopilot to fly an approach with vertical guidance, the autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect. WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories, ATC guidance, or positive visual acquisition of conflicting traffic. WARNING: Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and heading indications (GRS 77 installations only) in the following geographic areas: North of 72° North latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Warnings, Cautions & Notes WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to documentation from the lightning detection system manufacturer for detailed information about the system. WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. WARNING: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing. WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear as a partial symbol. WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within the MPEL boundary. WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only to enhance situational awareness. CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will harm the anti-reflective coating. CAUTION: Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and affect the airworthiness of the aircraft. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Warnings, Cautions & Notes NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. NOTE: All visual depictions contained within this document, including screen images of the system panel and displays, are subject to change and may not reflect the most current system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. NOTE: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Warnings, Cautions & Notes NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no comparison is possible. NOTE: The system responds to a terminal procedure based on data coded within that procedure in the Navigation Database. Differences in system operation may be observed among similar types of procedures due to differences in the Navigation Database coding specific to each procedure. NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin databasedependent avionics of the following: • It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. • Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’ • Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment. NOTE: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.flygarmin. com by selecting ‘Database Exclusions List.’ 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Warnings, Cautions & Notes NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation Database Alerts.’ NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate the revised DQRs. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select ‘Aviation Data Error Report’. NOTE: System navigation utilities may not reliably calculate range and bearing information when the aircraft is operating north of 89° North latitude or south of 89° South latitude. This may result in the system displaying small gaps in racetrack holding pattern depictions (GRS 7800 installations only). NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: Operate G1000 NXi system power through at least one cycle in a period of four days of continuous operation to avoid an autonomous system reboot. NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the Pilot’s Guide for this aircraft. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Warnings, Cautions & Notes NOTE: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag (EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Warnings, Cautions & Notes Blank Page Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Record of Revisions Part Number 190-02042-00 Change Summary Production Release Revision Date of Revision Affected Pages A February 2017 All B 190-02042-00 Rev. B March 2017 All Description Initial release at GDU 20.05 Added SurfaceWatch Setup user interface Added phone contacts Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series RR-1 Record of Revisions Blank Page RR-2 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Table of Contents FLIGHT INSTRUMENTS................................................................................................................. 1 Selecting the Altimeter Barometric Pressure Setting....................................................... 1 Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1 Change Altimeter Barometric Pressure Setting Units....................................................... 1 Synchronizing the Altimeter Barometric Pressure Settings............................................ 1 Synchronize CDI......................................................................................................................... 2 Selecting DG Mode (GRS 7800 Installations Only):............................................................ 2 Change Navigation Sources.................................................................................................... 2 Displaying The DME Information Window........................................................................... 3 Enable/Disable OBS Mode While Navigating with A GPS Flight Plan............................ 3 Generic Timer (PFD)................................................................................................................... 3 Configure Vspeed Bugs Individually...................................................................................... 3 Modifying Vspeeds (On, Off, Restore Defaults).................................................................. 4 Set Barometric/Radar Altimeter Minimum Descent Altitude/Decision Height and Bug................................................................................................................................................ 4 Testing the Radar Altimeter (KRA 405B only)..................................................................... 5 Displaying Wind Data............................................................................................................... 5 Activating And Deactivating SVT........................................................................................... 5 ENGINE INDICATION SYSTEM.................................................................................................. 7 NAV/COM/TRANSPONDER/AUDIO PANEL.......................................................................... 9 ADF Tuning (Optional)............................................................................................................... 9 DME Tuning................................................................................................................................. 9 Enter a Transponder Code....................................................................................................... 9 Selecting a COM Radio............................................................................................................. 9 Selecting a NAV Radio............................................................................................................ 10 NAV/COM Tuning...................................................................................................................... 10 Intercom..................................................................................................................................... 10 Passenger Address (PA) System............................................................................................ 11 Clearance Recorder and Player............................................................................................ 11 FLIGHT MANAGEMENT.............................................................................................................. 13 Changing A Field In The MFD Navigation Status Box...................................................... 13 USING MAP DISPLAYS............................................................................................ 13 Changing The Navigation Map Orientation....................................................................... 13 Configuring Automatic Zoom................................................................................................ 13 Panning The Map..................................................................................................................... 14 Reviewing Information For An Airport, NAVAID, Or User Waypoint............................ 14 Viewing Airspace Information For A Special-Use Or Controlled Airspace.................. 14 Displaying/Removing Topographic Data On The PFD Inset Map Or The HSI Map..... 15 Displaying/Removing Topographic Data Using The Navigation Map Page Menu..... 15 Setting Up The ‘Land’, ‘Aviation’ Or ‘Airspace’ Group Items........................................... 15 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series i Table of Contents Decluttering The Map............................................................................................................. 16 Decluttering The PFD Inset Map........................................................................................... 16 Displaying/Removing Airways.............................................................................................. 16 Selecting An Airway Range (Low ALT Airways or High ALT Airways)......................... 16 Displaying/Removing The Track Vector............................................................................... 17 Displaying/Removing The Fuel Range Ring And Selecting A Fuel Range Time.......... 17 Displaying/Removing The Selected Altitude Intercept Arc............................................ 17 WAYPOINTS............................................................................................................ 18 Selecting An Airport For Review By Identifier, Facility Name, Or Location................ 18 Selecting A Runway................................................................................................................. 18 Viewing A Destination Airport............................................................................................. 18 Viewing Information For A Nearest Airport On The PFD................................................ 18 Viewing Information For A Nearest Airport On The MFD............................................... 19 Viewing Runway Information For A Specific Airport...................................................... 19 Selecting An Intersection....................................................................................................... 19 Selecting An NDB..................................................................................................................... 20 Selecting A VOR........................................................................................................................ 20 Selecting A VRP........................................................................................................................ 20 Selecting A User Waypoint.................................................................................................... 20 Creating User Waypoints From The User Waypoint Information Page........................ 20 Creating User Waypoints From Map Pages........................................................................ 21 Changing The Altitude Buffer Distance Setting................................................................ 22 AIRSPACES.............................................................................................................. 22 Turning An Airspace Alert On Or Off................................................................................... 22 Selecting And Viewing An Airspace Alert With Its Associated Information............... 23 Turning Smart Airspace On Or Off....................................................................................... 23 DIRECT-TO NAVIGATION........................................................................................ 23 Entering A Waypoint Identifier, Facility Name, Or City As A Direct-To Destination. 23 Selecting An Active Flight Plan Waypoint As A Direct-To Destination........................ 24 Selecting A Nearest, Recent Or User Waypoint As A Direct-To Destination............... 24 Cancelling A Direct-To............................................................................................................. 25 Selecting A Manual Direct-To Course.................................................................................. 25 Entering A VNV Altitude And Along-Track Offset For The Waypoint............................ 25 Removing A VNV Altitude Constraint.................................................................................. 25 FLIGHT PLANNING.................................................................................................. 26 Creating An Active Flight Plan.............................................................................................. 26 Adding A Waypoint To The Active Flight Plan................................................................... 27 Creating And Adding User Waypoints To The Active Flight Plan................................... 27 Adding An Airway To A Flight Plan...................................................................................... 28 ii Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Table of Contents Storing An Active Flight Plan From The Active Flight Plan Page or the Active Flight Plan Window............................................................................................................................. 28 Activating A Stored Flight Plan On The MFD..................................................................... 28 Inverting And Activating A Stored Flight Plan On The MFD.......................................... 29 Import a Flight Plan from an SD Card................................................................................. 29 Export a Flight Plan to an SD Card...................................................................................... 30 Previewing a flight plan transfer from a wireless connection:.................................... 30 Ignoring a flight plan transfer from a wireless connection:......................................... 30 Storing a pending flight plan:.............................................................................................. 30 Activating a pending flight plan:......................................................................................... 31 Deleting a pending flight plan:............................................................................................ 31 Deleting all pending flight plans:........................................................................................ 31 Deleting The Active Flight Plan............................................................................................ 32 Deleting An Individual Waypoint From The Active Flight Plan...................................... 32 Deleting An Entire Airway From The Active Flight Plan.................................................. 32 Deleting An Entire Procedure From The Active Flight Plan............................................ 33 Entering An Along Track Offset Distance........................................................................... 33 Activating Parallel Track........................................................................................................ 33 Cancelling Parallel Track........................................................................................................ 34 Activating A Flight Plan Leg.................................................................................................. 34 Inverting The Active Flight Plan........................................................................................... 34 Inverting And Activating A Stored Flight Plan.................................................................. 35 Switching Between Leg-To-Leg Waypoint Distance And Cumulative Waypoint Distance................................................................................................................... 35 Determining The Closest Point Along The Active Flight Plan To A Selected Waypoint................................................................................................................... 35 Creating A User-Defined Hold At An Active Flight Plan Waypoint................................ 36 Creating A User-Defined Hold At The Aircraft Present Position.................................... 36 Creating A User-Defined Hold At A Direct-To Waypoint.................................................. 37 Exiting A User-Defined Hold Inserted Into The Active Flight Plan................................ 37 Removing A User-Defined Hold Inserted Into The Active Flight Plan.......................... 38 Removing A User-Defined Hold At An Off-Route Direct-To............................................ 38 VERTICAL NAVIGATION.......................................................................................... 38 Enabling VNV Guidance.......................................................................................................... 38 Disabling VNV Guidance......................................................................................................... 38 Altitude Constraints................................................................................................................ 39 Designating A Waypoint Altitude To Be Used For Vertical Guidance........................... 40 Designating A Procedure Waypoint Altitude To Be Used For Vertical Guidance....... 41 Entering/Modifiying An Altitude Constraint...................................................................... 41 Activating A Vertical Navigation Direct-To........................................................................ 42 Modifying The VS TGT And FPA............................................................................................. 42 Deleting An Altitude Constraint Provided By The Navigation Database.................... 42 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series iii Table of Contents Deleting An Altitude Constraint That Has Been Manually Entered.............................. 42 Reverting A Manually Entered Altitude Constraint Back To The Navigation Database Value................................................................................................... 43 Modifying A System Calculated Altitude Constraint....................................................... 43 PROCEDURES.......................................................................................................... 43 Loading A Departure Into The Active Flight Plan Using The PROC Key....................... 43 Viewing Available Departures At An Airport.................................................................... 44 Removing A Departure Procedure From The Active Flight Plan................................... 44 Loading An Arrival Into The Active Flight Plan Using The PROC Key........................... 45 Viewing Available Arrivals At An Airport........................................................................... 45 Loading An Approach Into The Active Flight Plan Using The PROC Key...................... 46 Viewing Available Approaches At An Airport.................................................................... 47 Activating A Previously Loaded Approach With Vectors To Final................................. 48 Removing An Approach From The Active Flight Plan...................................................... 48 Activating A Missed Approach In The Active Flight Plan................................................ 48 Activating Temperature Compensated Altitude............................................................... 49 Cancelling Temperature Compensated Altitude............................................................... 49 TRIP PLANNING...................................................................................................... 49 Selecting Automatic Or Manual Page Mode..................................................................... 49 Selecting Flight Plan Or Waypoint Mode........................................................................... 49 Selecting A Flight Plan And Leg For Trip Statistics.......................................................... 50 Selecting Waypoints For Waypoint Mode.......................................................................... 50 Entering Manual Data For Trip Statistics Calculations.................................................... 50 Entering Basic Empty Weight................................................................................................ 50 Entering A Pilot And Stores Weight..................................................................................... 51 Entering The Number Of Passengers................................................................................... 51 Entering The Average Passenger Weight........................................................................... 51 Entering The Cargo Weight.................................................................................................... 51 Entering A Fuel On Board Weight......................................................................................... 51 Entering Fuel Reserve............................................................................................................. 52 RAIM PREDICTION.................................................................................................. 52 Predicting RAIM Availability At A Selected Waypoint..................................................... 52 Predicting RAIM Availability At The Aircraft Present Position...................................... 53 Enabling/Disabling SBAS........................................................................................................ 53 HAZARD AVOIDANCE................................................................................................................. 55 Customizing the Hazard Displays on the Navigation Map............................................. 55 STORMSCOPE® (Optional)...................................................................................................... 55 SiriusXM Satellite Weather (Optional)................................................................................ 57 Connext Weather (Optional)................................................................................................. 59 iv Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Table of Contents FIS-B Weather........................................................................................................................... 68 Airborne Color Weather Radar............................................................................................. 71 Terrain Awareness & Warning System (TAWS-A and TAWS-B)....................................... 77 Vertical Situation Display (VSD)........................................................................................... 80 Traffic Avoidance Systems..................................................................................................... 81 Traffic Advisory System (TAS)/Traffic Collision Avoidance System (TCAS I)............... 81 ADS-B Traffic (GTX 345 Only) (Optional)............................................................................. 86 Traffic Collision Avoidance System (TCAS II) (Optional)................................................. 87 AUTOMATIC FLIGHT CONTROL SYSTEM........................................................................... 91 Activating The Flight Director.............................................................................................. 91 Vertical Modes.......................................................................................................................... 92 Lateral Modes........................................................................................................................... 92 Combination Modes (VNV, APR, NAV, BC, GA).................................................................... 93 Suspected Autopilot Malfunction........................................................................................ 94 Overpowering Autopilot Servos.......................................................................................... 95 ADDITIONAL FEATURES............................................................................................................ 97 SYNTHETIC VISION................................................................................................. 97 TERMINAL PROCEDURE CHARTS........................................................................... 98 SafeTaxi®.................................................................................................................................... 98 ChartView.................................................................................................................................. 99 FliteCharts®............................................................................................................................... 99 Airport Directory................................................................................................................... 101 SATELLITE TELEPHONE AND DATA LINK SERVICES............................................. 101 TELEPHONE COMMUNICATION............................................................................ 103 Contacts................................................................................................................................... 104 Incoming Calls........................................................................................................................ 105 Outgoing Calls........................................................................................................................ 106 Text Messaging (SMS)........................................................................................................... 108 WI-FI CONNECTIONS............................................................................................ 116 SIRIUSXM™ RADIO ENTERTAINMENT.................................................................. 119 Active Channel and Channel List........................................................................................ 119 SCHEDULER........................................................................................................... 121 SURFACEWATCH (OPTIONAL)............................................................................... 122 PILOT PROFILES.................................................................................................... 123 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series v Table of Contents ELECTRONIC STABILITY & PROTECTION (ESP™) (OPTIONAL)............................ 126 Roll Engagement.................................................................................................................... 128 Pitch Engagement.................................................................................................................. 128 Angle of Attack Protection.................................................................................................. 128 High Airspeed Protection..................................................................................................... 128 ANNUNCIATIONS & ALERTS.................................................................................................. 129 WARNING Annunciation....................................................................................................... 129 Advisory Annunciations....................................................................................................... 129 Message Advisory Alerts...................................................................................................... 129 Comparator Annunciations.................................................................................................. 130 Reversionary Sensor Annunciations.................................................................................. 130 AFCS Alerts.............................................................................................................................. 131 TAWS Alerts............................................................................................................................. 132 SurfaceWatch Alerts.............................................................................................................. 137 GDL 69/69A SXM Data Link Receiver Messages.............................................................. 137 Flight Plan Import/Export Messages................................................................................. 138 Pilot Profile import/Export Messages............................................................................... 139 Voice Alerts............................................................................................................................. 139 System Message Advisories................................................................................................ 141 APPENDIX...................................................................................................................................... 163 PFD Softkey Maps.................................................................................................................. 163 Loading Updated Databases............................................................................................... 176 Loading Updated Databases Using Flight Stream 510.................................................. 178 INDEX..........................................................................................................................................Index-1 vi Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Instruments Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting. EIS SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG) Nav/Com/ XPDR/Audio Press the BARO Knob to select standard pressure; STD BARO is displayed in barometric setting box. Or: Press the PFD Opt Softkey to display the second-level softkeys. 2) Press the STD Baro Softkey; STD BARO is displayed in barometric setting box. Flight Management 1) Press the PFD Opt Softkey to display the second-level softkeys. 2) Press the ALT Units Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). AFCS 1) Hazard Avoidance CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS Or: 4) Additional Features Press the HPA Softkey to display the barometric pressure setting in hectopascals. Press the BACK Softkey to return to the top-level softkeys. Annun/Alerts SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 2) Turn the small FMS Knob to select the System Setup Page. 3) If necessary, press the SETUP 1 Softkey to display the System Setup 1 Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight Baro in the Synchronization box. 6) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 7) To cancel the selection, press the FMS Knob. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index Turn the large FMS Knob to select the AUX page group on the MFD. Appendix 1) 1 SYNCHRONIZE CDI Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Instruments 1) Turn the large FMS Knob to select the AUX page group on the MFD. 2) Turn the small FMS Knob to select the System Setup Page. 3) If necessary, press the Setup 1 Softkey to display the System Setup 1 Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the ‘CDI Sync’ in the Synchronization box. 6) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 1) Press the PFD Opt Softkey. 2) Press the Sensors Softkey. 3) Press the HDG Softkey. 4) Press the DG Slave Softkey to activate DG mode. Press the DG Free Softkey to deactivate DG mode. 5) • Pressing the HDG- or HDG+ softkey to slew the heading counterclockwise or clockwise. • Pressing the HDG SYNC softkey to synchronize the heading to the current selected heading. • Pressing the TRACK SYNC softkey to synchronize the heading to the current track. Press the Back Softkey three times to return to the top-level softkeys. CHANGE NAVIGATION SOURCES Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management SELECTING DG MODE (GRS 7800 INSTALLATIONS ONLY): 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the cyan tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the cyan tuning box over the NAV2 standby frequency. Press the CDI Softkey a third time to return to GPS. Index 3) 2 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Instruments Press the PFD Opt Softkey. 2) Press the DME Softkey to display the DME Information Window above the BRG1 Information Window. 3) To remove the DME Information Window, press the DME Softkey again. EIS 1) Flight Instruments DISPLAYING THE DME INFORMATION WINDOW ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH A GPS FLIGHT PLAN 2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to return to automatic waypoint sequencing. 1) 2) 3) 4) Press the Tmr/Ref Softkey. 6) With ‘Start?’ highlighted, press the ENT Key to start the timer. The field changes to ‘Stop?’. 7) To stop the timer, press the ENT Key with ‘Stop?’ highlighted. The field changes to ‘Reset?’. 8) To reset the timer, press the ENT Key with ‘Reset?’ highlighted. The field changes back to ‘Start?’ and the digits are reset. 9) To remove the window, press the CLR Key or the Tmr/Ref Softkey. Hazard Avoidance GENERIC TIMER (PFD) Flight Management Press the OBS Softkey to select OBS Mode. Nav/Com/ XPDR/Audio 1) Turn the large FMS Knob to select the timer field (HH:MM:SS). AFCS Use the FMS Knob to enter the desired time and press the ENT Key. With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction (Up/Dn) and press the ENT Key. Additional Features Annun/Alerts Appendix CONFIGURE VSPEED BUGS INDIVIDUALLY 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 1) Press the Tmr/Ref Softkey. 2) Turn the large FMS Knob to highlight the desired Vspeed. 3 Flight Instruments Flight Instruments 3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a speed has been changed from a default value, an asterisk appears next to the speed). 4) EIS 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. To remove the window, press the CLR Key or the Tmr/Ref Softkey. MODIFYING VSPEEDS (ON, OFF, RESTORE DEFAULTS) Flight Management Nav/Com/ XPDR/Audio 6) 1) 2) 3) 4) Press the Tmr/Ref Softkey. 5) To remove the window, press the CLR Key or the Tmr/Ref Softkey. Press the MENU Key. Turn the FMS Knob to highlight the desired selection. Press the ENT Key. SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE/ DECISION HEIGHT AND BUG 1) Press the Tmr/Ref Softkey. Annun/Alerts Additional Features AFCS Hazard Avoidance Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field 2) Turn the large FMS Knob to highlight the Minimums field. 3) Turn the small FMS Knob to select BARO, TEMP COMP, or RAD ALT. OFF is selected by default. Press the ENT Key or turn the large FMS Knob to highlight the next field. 4) Use the small FMS Knob to enter the desired altitude (from zero to 16,000 feet when BARO or TEMP COMP is selected, or up to 2,500 feet when ‘RAD ALT’ is selected). 5) If TEMP COMP was selected, press the ENT Key or turn the large FMS Knob to highlight the next field and then enter the temperature (-59˚C to Appendix 59˚C) To remove the window, press the CLR Key or the Tmr/Ref Softkey. Index 6) 4 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Instruments Turn the large FMS Knob to select the AUX page group on the MFD. 2) Turn the small FMS Knob to select the AUX - System Status Page. 3) Press the RA Test Softkey to enable or disable the test. EIS 1) Flight Instruments TESTING THE RADAR ALTIMETER (KRA 405B ONLY) Nav/Com/ XPDR/Audio The ‘RA TEST’ annunciation is displayed above the RA box. To cancel the test, press the RA TEST Softkey again, or turn the FMS Knob to exit the AUX - System Status Page. DISPLAYING WIND DATA Press the PFD Opt Softkey. 2) Press the WIND Softkey to display wind data below the Selected Heading. 3) Press one of the Option softkeys to change how wind data is displayed: Flight Management 1) • Option 1: Wind direction arrow and speed • Option 3: Wind direction arrows with headwind, tailwind, and crosswind speed components To remove the window, press the Off Softkey. AFCS 4) Hazard Avoidance • Option 2: Wind direction arrow with true digital direction and speed ACTIVATING AND DEACTIVATING SVT 2) Press the SVT Softkey. 3) Press the Terrain Softkey. The SVT display will cycle on or off with each press of the Terrain Softkey. 4) Press the Back Softkey twice to return to the top-level softkeys. Annun/Alerts Press the PFD Opt Softkey. Additional Features 1) Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 5 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Instruments Index Appendix Annun/Alerts Additional Features AFCS Blank Page 6 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Engine Indication System Flight Instruments ENGINE INDICATION SYSTEM EIS 1 1 Nav/Com/ XPDR/Audio 2 2 Flight Management 3 4 4 Hazard Avoidance 5 5 AFCS 6 Additional Features 6 Annun/Alerts 7 7 (Normal Mode) Appendix 8 8 (Reversionary Mode) Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 7 1 Interstage Turbine Temperature (ITT) Displays Interstage Turbine Temperature in degrees Celsius (°C) 2 Torque (%) 3 Propeller Sync 4 Tachometer (PROP RPM) 5 Turbine Speed (% RPM) Displays torque as a percentage of maximum safe torque Displays a diamond when propellers are in sync. Indicates when propellers are out of sync by the diamond transitioning to an arrowhead. The arrowhead points towards the propeller turning at a higher-speed. Displays propeller speed in revolutions per minute (rpm); the red band indicates propeller overspeed Displays turbine speed in a percentage of the revolutions per minute (rpm) 6 Fuel Flow (FFLOW PPH) Displays current fuel flow in pounds per hour (pph) 7 Oil Pressure (OIL PSI) Displays pressure of oil supplied to the engines in pounds per square inch (psi) 8 Oil Temperature (OIL Displays the oil temperature in degrees Celsius (°C) °C) Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Engine Indication System 8 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Nav/Com/XPDR/Audio Panel Flight Instruments NAV/COM/TRANSPONDER/AUDIO PANEL ADF TUNING (OPTIONAL) EIS Tune the ADF using the remote ADF control head. DME TUNING 2) Turn the large FMS to select the DME source field. 3) Turn the small FMS Knob to select the desired Nav radio. 4) Press the ENT Key to complete the selection. Flight Management Press the DME Softkey. Nav/Com/ XPDR/Audio 1) ENTER A TRANSPONDER CODE Press the XPDR1 or XPDR2 Softkey to select the active transponder. 3) Press the Code Softkey to display the transponder code selection softkeys, for digit entry. 4) Press the digit softkeys to enter the code in the code field. When entering the code, the next key in sequence must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Five seconds after the fourth digit has been entered, the transponder code becomes active. SELECTING A COM RADIO Annun/Alerts Transmit/Receive Additional Features 2) AFCS Press the XPDR Softkey to display the transponder mode selection softkeys. Hazard Avoidance 1) Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if installed) on the audio panel. Appendix Receive Only Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the audio panel. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 9 SELECTING A NAV RADIO 1) To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2). 2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together. NAV/COM TUNING 1) Press the small tuning knob to select the desired radio for tuning. A light blue box highlights the radio frequency to be tuned. 2) Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz. 3) Press the Frequency Transfer Key to place the frequency into the active frequency field. INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may select or deselect the intercom. The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin. The annunciator is lit when the cabin intercom is active on either Audio Panel. The MAN SQ Key allows either automatic or manual control of the intercom squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated by the MAN SQ annunciator. During manual squelch operation, pressing the ICS Knob switches between volume and squelch adjustment, lighting the associated annunciator beneath the knob. When the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When the MAN SQ annunciator is extinguished, the ICS Knob controls only volume. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Nav/Com/XPDR/Audio Panel 10 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Nav/Com/XPDR/Audio Panel EIS A passenger address system is provided by pressing the PA Key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels. PA messages are one way from the flight deck to the passengers. Flight Instruments PASSENGER ADDRESS (PA) SYSTEM CLEARANCE RECORDER AND PLAYER Flight Management Hazard Avoidance AFCS Additional Features Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. The PLAY Key controls the play function. The PLAY annunciator is illuminated to indicate when play is in progress. The PLAY annunciator extinguishes after playback is finished. Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation. Pressing the PLAY Key again during play of a memory block stops play. If a COM input signal is detected during play of a recorded memory block, play is halted. Pressing the PLAY Key twice within one-half second while audio is playing plays the previous block of recorded audio. Each subsequent two presses of the PLAY Key within one-half second backtracks through the recorded memory blocks to reach and play any recorded block. Nav/Com/ XPDR/Audio NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded audio to the Copilot. Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 11 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Nav/Com/XPDR/Audio Panel Index Appendix Annun/Alerts Additional Features AFCS Blank Page 12 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Flight Instruments FLIGHT MANAGEMENT Changing A Field In The MFD Navigation Status Box Select the System Setup 1 Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box. 4) Turn the small FMS Knob to display and scroll through the data options list to select the desired data. 5) Press the ENT Key. Pressing the Defaults Softkey returns all fields to the default setting. EIS 1) Nav/Com/ XPDR/Audio Flight Management USING MAP DISPLAYS Hazard Avoidance CHANGING THE NAVIGATION MAP ORIENTATION 2) Press the ENT Key to display the Map Settings Window. 3) Turn the large FMS Knob, or press the ENT Key once, to select the ‘Orientation’ field. 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. 6) Press the FMS Knob to return to the base page. Additional Features With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Settings’ option. Annun/Alerts CONFIGURING AUTOMATIC ZOOM 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘Auto Zoom’ on/off field, and select ‘Off’ or ‘On’ using the small FMS Knob. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. Appendix 1) 190-02042-00 Rev. B AFCS 1) 13 EIS Flight Instruments Flight Management 6) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘Auto Zoom’ display selection field. 7) Select ‘MFD’, ‘PFD’, or ‘ALL’ using the small FMS Knob. 8) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘Max Look FWD’ field. Times are from zero to 999 minutes. 9) Use the FMS Knobs to set the time. Press the ENT Key. Nav/Com/ XPDR/Audio 10) Repeat step 9 for ‘Min Look FWD’ (zero to 99 minutes) and ‘Time Out’ (zero to 99 minutes). 11) Press the FMS Knob to return to the Navigation Map Page. Hazard Avoidance Flight Management PANNING THE MAP 1) Press the Joystick to display the Map Pointer. 2) Move the Joystick to move the Map Pointer around the map. 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. 1) Place the Map Pointer on a waypoint. 2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint. 3) Press the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page and return to the Navigation Map showing the selected waypoint. VIEWING AIRSPACE INFORMATION FOR A SPECIAL-USE OR CONTROLLED AIRSPACE 1) Place the Map Pointer on the boundary of an airspace. 2) Press the Joystick to remove the Map Pointer and center the map on the aircraft. Index Appendix Annun/Alerts Additional Features AFCS REVIEWING INFORMATION FOR AN AIRPORT, NAVAID, OR USER WAYPOINT 14 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management 2) Press the TOPO Softkey. 3) Press the TOPO Softkey again to remove topographic data from the PFD Inset Map or the HSI Map. When topographic data is removed from the PFD Map or HSI Map, all navigation data is presented on a black background. Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘Terrain Display’ field. 6) Select ‘Topo’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. Hazard Avoidance 1) AFCS Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Turn the small FMS Knob to select the desired group. 4) Press the ENT Key. The cursor flashes on the first field. 5) Turn the large FMS Knob to select the desired option. 6) Turn the small FMS Knob to select the desired setting (e.g. On/Off or maximum range). 7) Press the ENT Key to accept the selected option and move the cursor to the next item. 8) Repeat steps 5-7 as necessary. 9) Press the FMS Knob to return to the Navigation Map Page. Appendix 15 Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Annun/Alerts 1) Additional Features SETTING UP THE ‘LAND’, ‘AVIATION’ OR ‘AIRSPACE’ GROUP ITEMS 190-02042-00 Rev. B Flight Management DISPLAYING/REMOVING TOPOGRAPHIC DATA USING THE NAVIGATION MAP PAGE MENU Nav/Com/ XPDR/Audio Press the Map/HSI or Map Opt Softkey. EIS 1) Flight Instruments DISPLAYING/REMOVING TOPOGRAPHIC DATA ON THE PFD INSET MAP OR THE HSI MAP DECLUTTERING THE MAP Press the Detail Softkey with the Navigation Map Page displayed. The current declutter level is shown. With each softkey selection, another level of map information is removed. DECLUTTERING THE PFD INSET MAP 1) Press the Map/HSI Softkey. 2) Press the Detail Softkey. The current declutter level is shown. With each selection, another level of map information is removed. DISPLAYING/REMOVING AIRWAYS 1) Press the MAP Opt Softkey. 2) Press the AWY Softkey. Both High and Low Altitude Airways are displayed (AWY On). 3) Press the softkey again to display Low Altitude Airways only (AWY LO). 4) Press the softkey again to display High Altitude Airways only (AWY HI). 5) Press the softkey again to remove High Altitude Airways. No airways are displayed (AWY Off). AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management Index Appendix Annun/Alerts Additional Features SELECTING AN AIRWAY RANGE (LOW ALT AIRWAYS OR HIGH ALT AIRWAYS) 16 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key. 4) Highlight the ‘Low ALT Airways’ or ‘High ALT Airways’ range field. 5) To change the range setting, turn the small FMS Knob to display the range list. 6) Select the desired range using the small FMS Knob. 7) Press the ENT Key. 8) Press the FMS Knob to return to the Navigation Map Page. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setting’ option. 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘Track Vector’ field. 6) Select ‘On’ or ‘Off’. Press the ENT Key to accept the selected option. The flashing cursor highlights the look ahead time field. Use the FMS Knob to select the desired time. Press the ENT Key. 7) Press the FMS Knob to return to the Navigation Map Page. EIS 1) Flight Management 2) Press the ENT Key. The Map Settings Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘Fuel Range (RSV)’ field. 6) Select ‘On’ or ‘Off’. 7) Highlight the fuel reserve time field. This time should be set to the amount of flight time equal to the amount of fuel reserve desired. 8) To change the reserve fuel time, enter a time (00:00 to 23:59; hours:minutes). The default setting is 00:45 minutes. 9) Press the ENT Key. AFCS Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. Hazard Avoidance 1) Additional Features Annun/Alerts Appendix 10) Press the FMS Knob to return to the Navigation Map Page. DISPLAYING/REMOVING THE SELECTED ALTITUDE INTERCEPT ARC Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Settings’ option. 2) Press the ENT Key. The Map Settings Menu is displayed. 17 Index 1) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Nav/Com/ XPDR/Audio DISPLAYING/REMOVING THE FUEL RANGE RING AND SELECTING A FUEL RANGE TIME 190-02042-00 Rev. B Flight Instruments DISPLAYING/REMOVING THE TRACK VECTOR EIS Flight Instruments Flight Management 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘SEL ALT ARC’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. SELECTING AN AIRPORT FOR REVIEW BY IDENTIFIER, FACILITY NAME, OR LOCATION 1) From the Airport Information Page, press the FMS Knob. 2) Use the FMS Knobs and enter an identifier, facility name, or location. 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. SELECTING A RUNWAY 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor in the ‘Runways’ Box, on the runway designator. 3) Turn the small FMS Knob to display the desired runway (if more than one) for the selected airport. 4) To remove the flashing cursor, press the FMS Knob. VIEWING A DESTINATION AIRPORT From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination Airport is displayed. VIEWING INFORMATION FOR A NEAREST AIRPORT ON THE PFD Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio WAYPOINTS 18 1) Press the Nearest Softkey to display the Nearest Airports Window. Press the FMS Knob to activate the cursor. 2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information Window. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management 4) Press the CLR Key or the Nearest Softkey to close the PFD Nearest Airports Window. Nav/Com/ XPDR/Audio VIEWING INFORMATION FOR A NEAREST AIRPORT ON THE MFD EIS To return to the Nearest Airports Window press the ENT Key (with the cursor on ‘Back’) or press the CLR Key. The cursor is now on the next airport in the nearest airports list. (Repeatedly pressing the ENT Key moves through the airport list, alternating between the Nearest Airports Window and the Airport Information Window.) Flight Instruments 3) Turn the small FMS Knob to select the Nearest Airports Page (it is the first page of the group, so it may already be selected). If there are no Nearest Airports available, “None Within 200nm” is displayed. 3) Press the APT Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Airport Window’ and press the ENT Key. The cursor is placed in the ‘Nearest Airports’ Box. The first airport in the nearest airports list is highlighted. 4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport.) 5) Press the FMS Knob to remove the flashing cursor. AFCS 2) Hazard Avoidance Turn the large FMS Knob to select the NRST page group. Flight Management 1) VIEWING RUNWAY INFORMATION FOR A SPECIFIC AIRPORT 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor. Annun/Alerts With the Nearest Airports Page displayed, press the RNWY Softkey; or press the MENU Key, highlight ‘Select Runway Window’; and press the ENT Key. The cursor is placed in the ‘Runways’ Box. Additional Features 1) SELECTING AN INTERSECTION 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index With the Intersection Information Page displayed, enter an identifier in the Intersection Box. Appendix 1) 19 SELECTING AN NDB EIS Flight Instruments Flight Management 1) With the NDB Information Page displayed, enter an identifier, the name of the NDB, or the city in which it’s located in the NDB Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Additional Features AFCS With the VOR Information Page displayed, enter an identifier, the name of the VOR, or the city in which it’s located in the VOR Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. 1) With the VRP Information Page displayed, enter the identifier or the name of the VRP in the VRP Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. SELECTING A USER WAYPOINT 1) With the User Waypoint Information Page displayed, enter the name of the User Waypoint, or scroll to the desired waypoint in the User Waypoint List using the large FMS Knob. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. CREATING USER WAYPOINTS FROM THE USER WAYPOINT INFORMATION PAGE Index Appendix Annun/Alerts 1) SELECTING A VRP Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio SELECTING A VOR 20 1) Press the New Softkey, or press the MENU Key and select ‘Create New User Waypoint’. 2) Enter a user waypoint name (up to six characters). 3) Press the ENT Key. The current aircraft position is the default location of the new waypoint. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management If desired, define the type and location of the waypoint in one of the following ways: Flight Instruments 4) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the Reference Waypoints window using the FMS Knobs. EIS Or: Or: Press the ENT Key to accept the new waypoint. 6) If desired, change the storage method of the waypoint to “Temporary” or “Normal” by moving the cursor to “Temporary” and pressing the ENT Key to check or uncheck the box. 7) Press the FMS Knob to remove the flashing cursor. AFCS CREATING USER WAYPOINTS FROM MAP PAGES Press the ENT Key. The User Waypoint Information Page is displayed with the captured position. 3) Enter a user waypoint name (up to six characters). 4) Press the ENT Key to accept the selected name. The first reference waypoint box is highlighted. 5) If desired, define the type and location of the waypoint in one of the following ways: Appendix 2) Annun/Alerts Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint. Additional Features 1) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the Reference Waypoints window using the FMS Knobs. Index Or: 190-02042-00 Rev. B Hazard Avoidance 5) Flight Management Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the Information window using the FMS Knobs. Nav/Com/ XPDR/Audio Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the Reference Waypoints window using the FMS Knobs. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 21 Flight Management Flight Instruments Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the Reference Waypoints window using the FMS Knobs. Or: 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “Temporary” or “Normal” by moving the cursor to “Temporary” and pressing the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. 9) Press the Go Back Softkey to return to the map page. CHANGING THE ALTITUDE BUFFER DISTANCE SETTING 1) Use the FMS Knob to select the AUX - System Setup 1 Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box. 4) Use the FMS Knob to enter an altitude buffer value and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. AIRSPACES TURNING AN AIRSPACE ALERT ON OR OFF Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the Information window using the FMS Knobs. 22 1) Use the FMS Knob to select the AUX - System Setup 1 Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. 5) Press the FMS Knob to remove the flashing cursor. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Flight Instruments SELECTING AND VIEWING AN AIRSPACE ALERT WITH ITS ASSOCIATED INFORMATION 2) Press the Alerts Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Alerts Window’, and press the ENT Key. The cursor is placed in the ‘Airspace Alerts’ Box. 3) Select the desired airspace. 4) Press the FMS Knob to remove the flashing cursor. Nav/Com/ XPDR/Audio Select the Nearest Airspaces Page. EIS 1) TURNING SMART AIRSPACE ON OR OFF Flight Management 2) Press the MENU Key, and press the ENT Key. The cursor is placed in the ‘Group’ Box. 3) Turn the small FMS Knob to highlight the ‘Airspace’ in the ‘Group’ Box and press the ENT Key. 4) Turn the large FMS Knob to highlight the ‘Smart Airspace’ field in the Aviation Map Setup Window. 5) Turn the small FMS Knob clockwise to turn smart airspace ‘On’ or counterclockwise to turn smart airspace ‘Off’. 6) Press the FMS Knob to remove the flashing cursor. AFCS Use the FMS Knob to select the Navigation Map Page. Additional Features DIRECT-TO NAVIGATION Appendix Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan wayoint as the default selection or a blank waypoint field if no flight plan is active). Annun/Alerts ENTERING A WAYPOINT IDENTIFIER, FACILITY NAME, OR CITY AS A DIRECTTO DESTINATION 1) Hazard Avoidance 1) Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 23 2) Turn the small FMS Knob clockwise to begin entering a waypoint identifier (turning it counter-clockwise brings up the waypoint selection submenu press the CLR Key to remove it), or turn the large FMS Knob to select the facility name, or city field and turn the small FMS Knob to begin entering a facility name or city. If duplicate entries exist for the entered facility or city name, additional entries can be viewed by turning the small FMS Knob during the selection process. 3) Press the ENT Key. The ‘Activate?’ field is highlighted. 4) Press the ENT Key to activate the direct-to. SELECTING AN ACTIVE FLIGHT PLAN WAYPOINT AS A DIRECT-TO DESTINATION 1) While navigating an active flight plan, press the Direct-to Key. The Directto Window is displayed with the active flight plan waypoint as the default selection. 2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). 3) Select the desired waypoint. 4) Press the ENT Key. The cursor is now displayed on ‘Activate?’. 5) Press the ENT Key again to activate the direct-to. SELECTING A NEAREST, RECENT OR USER WAYPOINT AS A DIRECT-TO DESTINATION Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management 24 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan destination as the default selection or a blank destination if no flight plan is active). 2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). 3) Turn the small FMS Knob clockwise to display the Nearest, Recent or User waypoints. 4) Turn the large FMS Knob clockwise to select the desired waypoint. 5) Press the ENT Key. The cursor is now displayed on ‘Activate?’. 6) Press the ENT Key again to activate the direct-to. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the system resumes navigating the flight plan along the closest leg. EIS 1) Flight Instruments CANCELLING A DIRECT-TO 2) Highlight the course field. 3) Enter the desired course. 4) Press the ENT Key. The cursor is now displayed on ‘Activate?’. 5) Press the ENT Key again to activate the direct-to. Hazard Avoidance Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted. Flight Management 1) Nav/Com/ XPDR/Audio SELECTING A MANUAL DIRECT-TO COURSE ENTERING A VNV ALTITUDE AND ALONG-TRACK OFFSET FOR THE WAYPOINT 3) Enter the desired altitude. 4) Press the ENT Key. The option to select MSL or AGL is now displayed. 5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 6) Press the ENT Key. The cursor is now flashing in the VNV offset distance field. 7) Enter the desired along-track distance before the waypoint. 8) Press the ENT Key. The ‘Activate?’ field is highlighted. 9) Press the ENT Key to activate. Appendix Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. Annun/Alerts 2) Additional Features Press the Direct-to Key to display the Direct-to Window. AFCS 1) REMOVING A VNV ALTITUDE CONSTRAINT Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. 3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 1) 25 FLIGHT PLANNING CREATING AN ACTIVE FLIGHT PLAN EIS Flight Instruments Flight Management 1) Press the FPL Key. 2) Press the small FMS Knob to activate the cursor (only on MFD). 3) Select the origin airport and runway. Flight Management Nav/Com/ XPDR/Audio a) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, or user waypoints). Hazard Avoidance b) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The Set Runway Window is displayed with the Runway field highlighted. c) Turn the small FMS Knob to select the runway and press the ENT Key. AFCS d) Press the ENT Key again to add the runway to the flight plan. 4) Turn the large FMS Knob to highlight the destination airport identifier field. 5) Select the destination airport and runway. Annun/Alerts b) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The Set Runway Window is displayed with the Runway field highlighted. Appendix Additional Features a) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, or user waypoints). c) Turn the small FMS Knob to select the runway and press the ENT Key. d) Press the ENT Key again to add the runway to the flight plan. Index 6) 26 Turn the large FMS Knob to highlight the the Enroute Header, an enroute waypoint, or the dashes below the header. (If the header is selected, the new waypoint is placed following the header. If an enroute waypoint or the dashes are selected, the new waypoint will be placed ahead of the selected item.) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management EIS b) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. Repeat step number 6 to enter each additional enroute waypoint. 8) When all waypoints have been entered, press the FMS Knob to remove the cursor. Flight Management ADDING A WAYPOINT TO THE ACTIVE FLIGHT PLAN Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Select the point in the flight plan before which to add the new waypoint. The new waypoint is placed directly in front of the highlighted waypoint. 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 5) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. Hazard Avoidance 1) AFCS Additional Features Annun/Alerts CREATING AND ADDING USER WAYPOINTS TO THE ACTIVE FLIGHT PLAN 2) Press the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of the active flight plan. 27 Index Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location of the desired user waypoint. Appendix 1) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Nav/Com/ XPDR/Audio 7) 190-02042-00 Rev. B Flight Instruments a) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, or user waypoints). ADDING AN AIRWAY TO A FLIGHT PLAN 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time. 4) Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey, or press the MENU Key and select “Load Airway”. The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when a valid airway entry waypoint has been chosen (the waypoint ahead of the cursor position). 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘Load?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. STORING AN ACTIVE FLIGHT PLAN FROM THE ACTIVE FLIGHT PLAN PAGE OR THE ACTIVE FLIGHT PLAN WINDOW Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management 1) Press the MENU Key. 2) Highlight ‘Store Flight Plan’. 3) Press the ENT Key. 4) With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the next available position in the flight plan list on the Flight Plan Catalog Page. Index Appendix ACTIVATING A STORED FLIGHT PLAN ON THE MFD 28 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the Activate Softkey; or press the ENT Key twice; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The ‘Activate Stored Flight Plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Flight Instruments 3) EIS INVERTING AND ACTIVATING A STORED FLIGHT PLAN ON THE MFD Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Press the Invert Softkey; or press the MENU Key, highlight ‘Invert & Activate FPL?’, and press the ENT Key. The ‘Invert and activate stored flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Nav/Com/ XPDR/Audio 1) Flight Management Hazard Avoidance IMPORT A FLIGHT PLAN FROM AN SD CARD 2) Press the FPL Key on the MFD to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn either FMS Knob to highlight an empty or existing flight plan. 6) Press the Import Softkey. Additional Features Insert the SD card containing the flight plan in the top card slot on the MFD. AFCS 1) Annun/Alerts If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed. Or: Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 29 Index 190-02042-00 Rev. B Appendix If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card. If overwriting the existing flight plan is not desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select another existing or empty flight plan, and again press the Import Softkey. Flight Instruments Flight Management 7) Turn the small FMS Knob to highlight the desired flight plan for importing. 8) Press the ENT Key to confirm the import. 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the Export Softkey. 7) Press the ENT Key to confirm the export. Flight plans can be transferred to or from a mobile device via the Flight Stream 510 Bluetooth wireless connection. Transfer of a flight plan to a mobile device is controlled by the mobile device. PREVIEWING A FLIGHT PLAN TRANSFER FROM A WIRELESS CONNECTION: 1) When a flight plan transfer has been initiated from a mobile device, a Pending Flight Plan pop-up alert appears in the lower right corner of the MFD, and a Connext annunciation appears to the right of the MFD page name. 2) Press the ENT Key to display the Preview Flight Plan Page on the MFD. IGNORING A FLIGHT PLAN TRANSFER FROM A WIRELESS CONNECTION: Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS EXPORT A FLIGHT PLAN TO AN SD CARD 1) When a flight plan transfer has been initiated from a mobile device, a Pending Flight Plan pop-up alert appears in the lower right corner of the MFD, and an Connext annunciation appears to the right of the MFD page name. 2) Press the CLR Key to remove the pop-up alert and ignore the pending flight plan. The pending flight plan will still be available on the Flight Plan Catalog page. Index STORING A PENDING FLIGHT PLAN: 30 1) Press the FPL Key. 2) Turn the small FMS Knob to display the Flight Plan Catalog Page. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management 4) Turn the FMS Knob to highlight the pending flight plan. 5) Press the ENT Key to display the Preview Flight Plan Page on the MFD. 6) Press the Store Softkey to store the flight plan. The pending flight plan is stored and the pending annunciation is removed. EIS Press the FMS Knob to activate the cursor, and Flight Instruments 3) ACTIVATING A PENDING FLIGHT PLAN: Nav/Com/ XPDR/Audio 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the pending flight plan. 3) Press the ENT Key to display the Preview Flight Plan Page on the MFD. 4) Press the Activate Softkey. The ‘Activate Flight Plan?’ window is displayed. 5) With ‘OK’ highlighted, press the ENT Key to activate the pending flight plan. The pending flight plan becomes the active flight plan and is removed from the Flight Plan Catalog Page. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. AFCS DELETING A PENDING FLIGHT PLAN: Press the FPL Key. 2) Turn the small FMS Knob to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the FMS Knob to highlight the desired pending flight plan. 5) Press the Delete Softkey. The ‘Delete Flight Plan XX?’ window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to delete the pending flight plan. The pending flight plan is removed from the Flight Plan Catalog Page. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Additional Features 1) Turn the small FMS Knob to display the Flight Plan Catalog Page. 3) Press the MENU Key. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 2) Appendix Press the FPL Key. Annun/Alerts DELETING ALL PENDING FLIGHT PLANS: 1) Hazard Avoidance Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. Flight Management 1) 31 4) Turn the FMS Knob to highlight ‘Delete All Pending’. 5) Press the ENT Key. A ‘Delete all pending flight plans?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to delete all pending flight plans. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. EIS Flight Instruments Flight Management Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete all waypoints in flight plan?’ window is displayed. 3) With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Additional Features 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint to be deleted. 3) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. DELETING AN ENTIRE AIRWAY FROM THE ACTIVE FLIGHT PLAN Index Appendix Annun/Alerts 1) DELETING AN INDIVIDUAL WAYPOINT FROM THE ACTIVE FLIGHT PLAN AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio DELETING THE ACTIVE FLIGHT PLAN 32 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the white header of the airway to be deleted. 3) Press the CLR Key. The ‘Remove <airway name> from flight plan?’ window is displayed. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Flight Instruments 4) DELETING AN ENTIRE PROCEDURE FROM THE ACTIVE FLIGHT PLAN EIS Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the white header of the procedure to be deleted. 3) Press the CLR Key. The ‘Remove <procedure name> from flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Hazard Avoidance 2) ENTERING AN ALONG TRACK OFFSET DISTANCE 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the along track offset. 3) Press the ATK OFS Softkey (MFD only); or press the MENU Key, highlight ‘Create ATK Offset Waypoint’, and press the ENT Key. 4) Enter a positive or negative offset distance in the range of +/- 1 to 999 nm (limited by leg distances). 5) Press the ENT Key to create the offset waypoint. 6) Press the FMS Knob to remove the flashing cursor. Additional Features Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). Annun/Alerts Appendix ACTIVATING PARALLEL TRACK Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with the ‘Direction’ field highlighted. 33 Index 1) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series AFCS 1) 190-02042-00 Rev. B Flight Management Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). Nav/Com/ XPDR/Audio 1) EIS Flight Instruments Flight Management 3) Turn the small FMS Knob to select ‘LEFT’ or ‘RIGHT’ and press the ENT Key. The ‘Distance’ field is highlighted. 4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘Activate Parallel Track’ is highlighted. 5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track activation. 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with ‘Cancel Parallel Track?’ highlighted. 3) Press the ENT Key. ACTIVATING A FLIGHT PLAN LEG 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the destination waypoint for the desired leg. 3) Press the ACT Leg Softkey (MFD only); or press the MENU Key, highlight ‘Activate Leg’, and press the ENT Key. A confirmation window is displayed with ‘Activate’ highlighted. 4) Press the ENT Key to activate the flight plan leg. To cancel, press the CLR Key, or highlight ‘Cancel’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio CANCELLING PARALLEL TRACK Index Appendix INVERTING THE ACTIVE FLIGHT PLAN 34 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key. An ‘Invert Active Flight Plan?’ confirmation window is displayed. 3) Select ‘OK’. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the ENT Key to invert and activate the active flight plan. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Flight Instruments 4) INVERTING AND ACTIVATING A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Press the Invert Softkey; or press the MENU Key, highlight ‘Invert & Activate FPL?’, and press the ENT Key. The ‘Invert and activate stored flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. EIS 1) Press the View Softkey to display the CUM and Leg-Leg Softkeys. 3) Press the CUM Softkey to view cumulative waypoint distance, or press the Leg-Leg Softkey to view leg-to-leg waypoint distance. 4) Press the Back Softkey to return to the top level active flight plan softkeys. Additional Features DETERMINING THE CLOSEST POINT ALONG THE ACTIVE FLIGHT PLAN TO A SELECTED WAYPOINT Press the MENU Key, highlight ‘Closest Point Of FPL’’, and press the ENT Key. A window appears with the reference waypoint field highlighted. 3) Enter the identifier of the reference waypoint and press the ENT Key. The system displays the bearing (BRG) and distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference waypoint. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 35 Index 2) Appendix Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). Annun/Alerts 1) 190-02042-00 Rev. B AFCS 2) Hazard Avoidance Press the FPL Key on the MFD to display the Active Flight Plan Page. Flight Management 1) Nav/Com/ XPDR/Audio SWITCHING BETWEEN LEG-TO-LEG WAYPOINT DISTANCE AND CUMULATIVE WAYPOINT DISTANCE Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the hold. 3) Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key. The HOLD AT window appears with the course field highlighted. 4) Use the FMS Knobs to edit the entry course, and press the ENT Key. 5) Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction, and press the ENT Key. 6) Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press the ENT Key. 7) Use the FMS Knobs to edit the length, and press the ENT Key. 8) Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the ENT Key. 9) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and press the ENT Key. Hazard Avoidance EIS 1) Nav/Com/ XPDR/Audio CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT Flight Management Flight Instruments Flight Management AFCS 10) Press the ENT Key while ‘Load?’ is highlighted to insert the hold into the flight plan. Index Appendix Annun/Alerts Additional Features CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION 36 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Hold At Present Position’, and press the ENT Key. The ‘Hold at’ window appears with the course field highlighted. 3) If desired, use the FMS Knobs to edit the entry course, and press the ENT Key. 4) Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction, and press the ENT Key. 5) Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press the ENT Key. 6) Use the FMS Knobs to edit the length, and press the ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management 8) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time), and press the ENT Key. 9) Press the ENT Key while ‘Activate?’ is highlighted to create an Offroute Direct-to hold waypoint at the aircraft present position and activate the hold. EIS Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the ENT Key. Flight Instruments 7) Nav/Com/ XPDR/Audio CREATING A USER-DEFINED HOLD AT A DIRECT-TO WAYPOINT 2) Use the FMS Knobs to edit the entry course, and press the ENT Key. 3) Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction, and press the ENT Key. 4) Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and press the ENT Key. 5) Use the FMS Knobs to edit the length, and press the ENT Key. 6) Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press the ENT Key. 7) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 8) Press the ENT Key while ‘Activate?’ is highlighted to activate the direct-to with the user-defined hold defined at the direct-to waypoint. (If the directto wayoint is part of the active flight plan, the HOLD is inserted into the active flight plan. If the direct-to waypoint is not part of the active flight plan, an off-route direct-to hold is created.) Hazard Avoidance Press a Direct-to Key and set up the direct-to waypoint as desired, but select ‘Hold?’ instead of ‘Activate?’ when finished (MFD or PFD). Flight Management 1) Additional Features Annun/Alerts Appendix Press the SUSP Softkey. The system will provide guidance to follow the holding pattern to the inbound course and resume automatic waypoint sequencing. AFCS EXITING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT PLAN Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 37 REMOVING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT PLAN AFCS 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the HOLD waypoint. 3) Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. The holding pattern is removed from the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal of the holding pattern. REMOVING A USER-DEFINED HOLD AT AN OFF-ROUTE DIRECT-TO Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management 1) Press a Direct To Key to display the Direct To Window (PFD or MFD). 2) Press the MENU Key to display the Page Menu with the cursor on the ‘Cancel Direct-To NAV’ selection. 3) Press the ENT Key. The holding pattern is removed. VERTICAL NAVIGATION 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’, and press the ENT Key. Vertical navigation is enabled, and vertical guidance begins with the waypoint shown in the Active VNV Profile box (defaults first waypoint in the active flight plan with an altitude enabled for vertical navigation (e.g., HABUK)). DISABLING VNV GUIDANCE Index Appendix Annun/Alerts Additional Features ENABLING VNV GUIDANCE 38 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the Cncl VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management EIS The system system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation. These altitudes are, depending on the specific instance, manually entered or retrieved from the published altitudes in the navigation database. Flight Instruments ALTITUDE CONSTRAINTS Displayed Text Examples Nav/Com/ XPDR/Audio White Text White Text with Altitude Restriction Bar Hazard Avoidance Cyan Text Flight Management Cyan Text with Pencil Icon AFCS 23OOFT 5OOOFT Cross AT 2,300 ft Cross AT or ABOVE 5,000 ft Additional Features Altitude Constraint Examples Annun/Alerts 3OOOFT Cross AT or BELOW 3,000 ft Temperature Compensated Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 39 Flight Management Cyan Text 5OOOFT 5OOOFT Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. No white line above or below to indicate a potential constraint. Altitude is designated for use in determining vertical guidance. A pencil icon indicates manual designation or manual data entry. 5OOOFT 5OOOFT Altitude retrieved from the navigation database. White line above or below indicates the type of constraint, as shown in the preceding figure. These altitudes are provided as a reference, and are not designated to be used in determining vertical guidance. The system cannot use this altitude in determining vertical guidance because of an invalid constraint condition. Altitudes associated with arrival and approach procedures are “auto-designated”. This means the system automatically uses the altitudes loaded with the arrival or approach for giving vertical speed and deviation guidance. Note that these altitudes are displayed as cyan text up to, but not including, the FAF. The FAF is always a “reference only” altitude and cannot be designated, unless the selected approach does not provide vertical guidance. In this case, the FAF altitude can be designated. Altitudes that have been designated for use in vertical guidance can be “undesignated” using the CLR Key. The altitude is now displayed only as a reference. It is not used to give vertical guidance. Other displayed altitudes may change due to re-calculations or be rendered invalid as a result of manually changing an altitude to a non-designated altitude. DESIGNATING A WAYPOINT ALTITUDE TO BE USED FOR VERTICAL GUIDANCE 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Turn the small FMS Knob to enter editing mode. 4) Press the ENT Key. The altitude is now shown in cyan, indicating it is usable for vertical guidance. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments White Text 40 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Press the ENT Key. The altitude is now shown in cyan, indicating it is usable for vertical guidance. EIS 1) Flight Instruments DESIGNATING A PROCEDURE WAYPOINT ALTITUDE TO BE USED FOR VERTICAL GUIDANCE Nav/Com/ XPDR/Audio ENTERING/MODIFIYING AN ALTITUDE CONSTRAINT 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter the three digit flight level. Hazard Avoidance Press the FPL Key to display the Active Flight Plan Page on the MFD. Flight Management 1) 4) AFCS Press the ENT Key to accept the altitude constraint; if the selected waypoint is an airport, an additional choice is displayed. Turn the small FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude. An altitude constraint is invalid if: • Meeting the constraint requires the maximum flight path angle (6° down) or maximum vertical speed (-6000 fpm) to be exceeded • The constraint is within a leg type for which altitude constraints are not supported Appendix • The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS SBAS approach) Annun/Alerts • The altitude constraint results in a TOD behind the aircraft present position Additional Features • Meeting the constraint requires the aircraft to climb • The altitude constraint is added to a waypoint past the FAF. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 41 Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint. 3) Press the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed. 4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint. 5) Press the FMS Knob to remove the flashing cursor. MODIFYING THE VS TGT AND FPA Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the VNV Prof Softkey; or press the MENU Key, highlight ‘Select VNV Profile Window’, and press the ENT Key. The cursor is now located in the Active VNV Profile box. 3) Turn the FMS Knobs as needed to edit the values. 4) Press the FMS Knob to remove the flashing cursor. 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. DELETING AN ALTITUDE CONSTRAINT THAT HAS BEEN MANUALLY ENTERED Index Appendix 1) DELETING AN ALTITUDE CONSTRAINT PROVIDED BY THE NAVIGATION DATABASE Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management 1) EIS ACTIVATING A VERTICAL NAVIGATION DIRECT-TO Nav/Com/ XPDR/Audio Flight Instruments Flight Management 42 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available). Flight Instruments 3) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value. 5) Press the FMS Knob to remove the flashing cursor. Hazard Avoidance 2) Flight Management Press the FPL Key to display the Active Flight Plan Page on the MFD. Nav/Com/ XPDR/Audio 1) EIS REVERTING A MANUALLY ENTERED ALTITUDE CONSTRAINT BACK TO THE NAVIGATION DATABASE VALUE MODIFYING A SYSTEM CALCULATED ALTITUDE CONSTRAINT Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘EDIT’ and press the ENT Key. 5) Edit the value using the FMS Knobs, and press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor. Annun/Alerts 2) Additional Features Press the FPL Key to display the Active Flight Plan Page on the MFD. AFCS 1) PROCEDURES Appendix LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN USING THE PROC KEY Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘Select Departure’. 3) Press the ENT Key. The Departure Loading Page is displayed. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 1) 43 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select a departure from the list and press the ENT Key. 6) Select a runway (if required) and press the ENT Key. 7) Select a transition (if required) and press the ENT Key. ‘Load?’ is highlighted. 8) Press the ENT Key to load the departure procedure. From the Airport Information Page (first page in the WPT group), press the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Hazard Avoidance Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. 4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor moves to the Runway box. The departure is previewed on the map. 5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box (only if there are available transitions). The departure is previewed on the map. 6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Sequence box. The departure is previewed on the map. 7) Press the INFO-1 Softkey or the INFO-2 Softkey to return to the Airport Information Page. REMOVING A DEPARTURE PROCEDURE FROM THE ACTIVE FLIGHT PLAN Index Appendix Annun/Alerts Flight Management 1) AFCS VIEWING AVAILABLE DEPARTURES AT AN AIRPORT Additional Features Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management 44 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Departure’. 3) Press the ENT Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘Select Arrival’. 3) Press the ENT Key. The Arrival Loading Page is displayed. 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select an arrival from the list and press the ENT Key. 6) Select a transition (if required) and press the ENT Key. 7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the arrival procedure. EIS 1) Flight Instruments LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN USING THE PROC KEY To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the map. 4) Turn the small FMS Knob to view the available arrivals. Press the ENT Key to select the arrival. The cursor moves to the Transition box. The arrival is previewed on the map. 5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Runway box. The arrival is previewed on the map. 6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Sequence box. The arrival is previewed on the map. 7) Press the INFO-1 Softkey or the INFO-2 Softkey to return to the Airport Information Page. AFCS 2) Hazard Avoidance From the Airport Information Page (first page in the WPT group), press the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport Information Page. Flight Management 1) Nav/Com/ XPDR/Audio VIEWING AVAILABLE ARRIVALS AT AN AIRPORT Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 45 Flight Management Flight Instruments HSI Annunciation LNAV RNAV GPS approach using published LNAV minima RNAV GPS approach using published LNAV minima. Advisory vertical guidance is provided L/VNAV (available only if SBAS available) RNAV GPS approach using published LNAV/VNAV minima (downgrades to L/ VNAV (Baro VNAV) if SBAS unavailable) LP (available only if SBAS available) RNAV GPS approach using published LP minima (downgrades to LNAV if SBAS unavailable) LP+V (available only if SBAS available) RNAV GPS approach using published LP minima Advisory vertical guidance is provided (downgrades to LNAV if SBAS unavailable) LPV (available only if SBAS available) RNAV GPS approach using published LPV minima (downgrades to L/VNAV (Baro VNAV) if SBAS unavailable) Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS LNAV+V Description Approach Service Levels Additional Features AFCS LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN USING THE PROC KEY 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘Select Approach’, and press the ENT Key. The Approach Loading Page is displayed. 3) Select the airport and approach: a) Use the FMS Knob to select an airport and press the ENT Key. Annun/Alerts b) Select an approach from the list and press the ENT Key. Or: Appendix a) If necessary, push the FMS Knob to exit the approach list, and use the large FMS Knob to move the cursor to the Approach Channel field. b) Use the FMS Knob to enter the approach channel number, and press the ENT Key to accept the approach channel number. The airport and approach are selected. Index 4) 46 Select a transition (if required) and press the ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Minimums a) To set ‘Minimums’, turn the small FMS Knob to select ‘BARO’, ‘TEMP COMP’ or ‘RAD ALT’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key. To skip setting minimums, press the ENT Key. 6) VIEWING AVAILABLE APPROACHES AT AN AIRPORT 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on the map. 4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The cursor moves to the Transition box. The approach is previewed on the map. 5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Minimums box. The approach is previewed on the map. 6) Turn the small FMS Knob to select minimums on or off. Press the ENT Key. Appendix a) When minimums are selected on, the cursor moves to the minimum altitude field . Use the small FMS Knob to select the altitude. Press the ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 47 Index b) If temperature compensated minimums was selected, the cursor moves to the temperature field. Use the small FMS Knob to select the temperature. Press the ENT Key. The cursor moves to the Sequence box. The approach is previewed on the map. 190-02042-00 Rev. B Annun/Alerts To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. Additional Features 2) AFCS From the Airport Information Page (first page in the WPT group), press the APR Softkey. The Approach Information Page is displayed, defaulting to the airport displayed on the Airport information Page. Hazard Avoidance 1) Flight Management Press the ENT Key with ‘Load?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘Activate’ and press the ENT Key to load and activate the approach procedure. Nav/Com/ XPDR/Audio Or: EIS b) If ‘TEMP COMP’ was selected, the cursor moves to the temperature field. Turn the small FMS Knob to select the temperature, and press the ENT Key. Flight Instruments 5) Flight Management Flight Instruments Or: When minimums are selected off, the cursor moves to the Sequence box. The approach is previewed on the map. EIS 7) Press the INFO-1 or the INFO-2 Softkey to return to the Airport Information Page. 1) Press the PROC Key to display the Procedures Window. 2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key. REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio ACTIVATING A PREVIOUSLY LOADED APPROACH WITH VECTORS TO FINAL 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Approach’. 3) Press the ENT Key. A confirmation window is displayed listing the approach procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Annun/Alerts Additional Features ACTIVATING A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1) Press the PROC Key. 2) Turn the FMS Knob to highlight ‘Activate Missed Approach’. 3) Press the ENT Key. The aircraft automatically sequences to the MAHP. Or: Index Appendix Press the Go-Around Button. 48 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The Temperature Compensation Window is displayed. 4) Use the small FMS Knob to select the temperature at the <airport>. The compensated altitude is computed as the temperature is selected. 5) Press the ENT Key. ‘Activate Compensation?’ is highlighted. 6) Press the ENT Key. The compensated altitudes for the approach are Nav/Com/ XPDR/Audio From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. EIS 1) Flight Instruments ACTIVATING TEMPERATURE COMPENSATED ALTITUDE Flight Management shown in the flight plan. CANCELLING TEMPERATURE COMPENSATED ALTITUDE From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The Temperature Compensation Window is displayed. 4) Press the ENT Key. ‘Cancel Compensation?’ is highlighted. 5) Press the ENT Key. The temperature compensated altitude at the FAF Hazard Avoidance 1) AFCS is cancelled. Additional Features TRIP PLANNING SELECTING AUTOMATIC OR MANUAL PAGE MODE Annun/Alerts Press the Auto Softkey or the Manual Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and press the ENT Key. Appendix SELECTING FLIGHT PLAN OR WAYPOINT MODE Press the FPL Softkey or the WPTs Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints Mode’, and press the ENT Key. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 49 SELECTING A FLIGHT PLAN AND LEG FOR TRIP STATISTICS 1) Press the FMS Knob to activate the cursor in the flight plan number field. 2) Turn the small FMS Knob to select the desired flight plan number. 3) Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each leg can be viewed by turning the small FMS Knob to select the desired leg. The Inset Map also displays the selected data. SELECTING WAYPOINTS FOR WAYPOINT MODE Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management 1) Press the WPTs Softkey; or press the MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The cursor is positioned in the waypoint field directly below the FPL field. 2) Turn the FMS knobs to select the desired waypoint (or select from the Page Menu ‘Set WPT to Present Position’ if that is what is desired), and press the ENT Key. The cursor moves to the second waypoint field. 3) Turn the FMS knobs to select the desired waypoint, and press the ENT Key. The statistics for the selected leg are displayed. 1) Press the Manual Softkey or select ‘Manual Mode’ from the Page Menu, and press the ENT Key. The cursor may now be positioned in any field in the top right two boxes. 2) Turn the FMS Knobs to move the cursor onto the Departure Time field and enter the desired value. Press the ENT Key. The statistics are calculated using the new value and the cursor moves to the next entry field. Repeat until all desired values have been entered. ENTERING BASIC EMPTY WEIGHT Index Appendix Annun/Alerts Additional Features AFCS ENTERING MANUAL DATA FOR TRIP STATISTICS CALCULATIONS 50 1) Press the Empty WT Softkey; or press the MENU Key, highlight ‘Set Basic Empty Weight’, and press the ENT Key to select the ‘Basic Empty Weight’ field. 2) Turn the small FMS Knob to enter the basic empty weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Press the FMS Knob to activate the cursor and highlight the ‘Pilot & Stores’ field. 2) Turn the small FMS Knob to enter the pilot and stores weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. EIS 1) Press the FMS Knob to activate the cursor and highlight the ‘Passengers #’ field. 2) Turn the small FMS Knob to enter the number of passengers. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Hazard Avoidance ENTERING THE AVERAGE PASSENGER WEIGHT Turn the small FMS Knob to enter the average passenger weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Additional Features 2) AFCS Press the FMS Knob to activate the cursor and highlight the passenger weight field. ENTERING THE CARGO WEIGHT 2) Turn the small FMS Knob to enter the cargo weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Appendix Press the FMS Knob to activate the cursor and highlight the ‘Cargo’ field. Annun/Alerts 1) ENTERING A FUEL ON BOARD WEIGHT Press the FMS Knob to activate the cursor and highlight the ‘Fuel on Board’ field. 2) Turn the small FMS Knob to enter the fuel on board. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 51 Index 1) 190-02042-00 Rev. B Flight Management 1) Nav/Com/ XPDR/Audio ENTERING THE NUMBER OF PASSENGERS 1) Flight Instruments ENTERING A PILOT AND STORES WEIGHT Flight Instruments Flight Management 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. 1) Press the FMS Knob to activate the cursor and highlight the ‘Fuel Reserves’ field. 2) Turn the small FMS Knob to enter the fuel reserves amount. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. RAIM PREDICTION PREDICTING RAIM AVAILABILITY AT A SELECTED WAYPOINT 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The RAIM Prediction ‘Waypoint’ field is highlighted. 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘Compute RAIM?’ highlighted to begin the computation. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS ENTERING FUEL RESERVE 52 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Flight Management Flight Instruments PREDICTING RAIM AVAILABILITY AT THE AIRCRAFT PRESENT POSITION 2) Press the FMS Knob. The RAIM Prediction ‘Waypoint’ field is highlighted. 3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key. 4) Press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘Compute RAIM?’ highlighted to begin the computation. Nav/Com/ XPDR/Audio Select the AUX-GPS Status Page. Flight Management ENABLING/DISABLING SBAS 2) Press the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’, ‘MSAS’ or ‘WAAS’. 4) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS. AFCS Select the AUX-GPS Status Page. Hazard Avoidance 1) EIS 1) Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 53 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Flight Management Index Appendix Annun/Alerts Additional Features AFCS Blank Page 54 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments HAZARD AVOIDANCE With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select ‘Weather’ to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic. 3) Press the small FMS Knob to return to the Navigation Map Page. Hazard Avoidance 1) Additional Features Appendix Displaying Stormscope Lightning Data on the Navigation Map Page Press the STRMSCP Softkey. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 2) Annun/Alerts WARNING: Do not rely on information from the lightning detection system display as the sole basis for hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to the documentation from the lightning detection system manufacturer for detailed information about the system. Press the Map Opt Softkey. AFCS STORMSCOPE® (OPTIONAL) 1) Flight Management CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP Nav/Com/ XPDR/Audio WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. EIS WARNING: Do not use data link weather information for maneuvering in, near or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. 55 Hazard Avoidance EIS Flight Instruments Displaying Stormscope information on PFD maps: 1) On the PFD, press the Map/HSI Softkey (in TCAS II installations, press the Map Opt Softkey.) 2) Press the Lightning Softkey. 3) Press the STRMSCP Softkey. Nav/Com/ XPDR/Audio Lightning Age Strike is less than 6 seconds old Symbol Strike is between 6 and 60 seconds old Flight Management Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Additional Features AFCS Hazard Avoidance Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode 1) Press the MENU Key. 2) With ‘Map Settings’ selected, press the ENT Key. 3) Turn the FMS Knob to select the ‘Weather’ group and press the ENT Key. 4) Turn the large FMS Knob to select the Stormscope Mode field. 5) Turn the small FMS Knob to change between ‘Cell’ and ‘Strike’ options. When the desired item is selected, press the ENT Key. 6) Press the FMS knob to return to the Navigation Map Page. Annun/Alerts Manually Clearing Stormscope Data on the Navigation Map 1) Press the MENU Key. 2) Turn the FMS Knob to highlight ‘Clear Stormscope® Lightning’. 3) Press the ENT Key. Index Appendix Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’ 56 1) Select the Stormscope Page. 2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed. Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells. SIRIUSXM SATELLITE WEATHER (OPTIONAL) EIS Viewing the Weather Data Link (XM) Page: Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link (XM or CNXT or FIS-B) Page. 3) If the page title does not contain ‘(XM)’, it will be necessary to change the data link weather source to SiriusXM Weather. Refer to the next procedure to change the source. Nav/Com/ XPDR/Audio 1) With the Inset Map or HSI Map displayed, press the Map/HSI Softkey (Map Opt Softkey for TCAS II installations). 2) Press the NEXRAD or METAR Softkey. Hazard Avoidance 1) 2) Press the Layout Softkey. 3) Press the Wx LGND Softkey to enable/disable the display of weather product age information. Additional Features With the Inset Map or HSI Map displayed, press the Map/HSI Softkey (Map Opt Softkey for TCAS II installations). Annun/Alerts SiriusXM Weather Products and Symbols Refresh Rate (Minutes) NEXRAD 30 5 (U.S.) 10 (Canada) Cloud Top (CLD TOP) 60 15 (69/69A) 30 (69/69A SXM) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 57 Index 190-02042-00 Rev. B Symbol Appendix Expiration Time (Minutes) Weather Product AFCS Enabling/disabling weather product age information on the PFD maps: 1) Flight Management Enabling/disabling Weather Product Information on the PFD maps: Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance Expiration Time (Minutes) Refresh Rate (Minutes) Echo Top (ECHO TOP) 30 7.5 SiriusXM Lightning (LTNG) 30 5 Cell Movement (CELL MOV) 30 1.25 SIGMETs/AIRMETs (SIG/ AIR) 60 12 METARs 90 12 City Forecast (CITY) 90 12 Surface Analysis (SFC) 60 12 Freezing Levels (FRZ LVL) 120 12 Winds Aloft (WIND) 90 12 County Warnings (COUNTY) 60 5 Cyclone Warnings (CYCLONE) 60 12 90 22 90 12 90 12 Weather Product Icing Potential (CIP and SLD) (ICNG) Pilot Weather Report (PIREPs) Air Report (AIREPs) 58 Symbol Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Refresh Rate (Minutes) 180 12 30 5 60 12 60 12 Nav/Com/ XPDR/Audio TAFs No product image No product image No product image Expiration Time (Minutes) EIS Turbulence (TURB) Radar Coverage Not Available TFRs Symbol Flight Instruments Weather Product Flight Management CONNEXT WEATHER (OPTIONAL) Annun/Alerts Appendix Weather data is provided when the pilot initiates either a manual or automatic Connext data request on the Weather Data Link (CNXT) Page on the MFD. No weather data is displayed until the first Connext Weather Data Request is made. Additional Features NOTE: The availability of specific Garmin Connext Weather products varies by region. For product coverage information, refer to fly.garmin.com/fly-garmin/ gfds-weather. AFCS WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be older than the indicated weather product age. Hazard Avoidance WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 59 Registering with Garmin Flight Data Services A subscriber account must be established prior to receiving Connext Weather products. Contact Garmin Flight Data Services at https://fly.garmin.com/fly-garmin/ support/applications/satelliteservices/ or by calling 1-866-739-5687 in the United States or (011) 913-440-1135. The following information is required to register for Connext Weather services: G1000 NXi System ID, GSR56 (GSR1) Serial Number(s), Tail Number, Serail/Airframe Number, Country of Registration, Aircraft Manufacturer, and Aircraft Model. 1) Turn the large FMS Knob on the MFD to select the Aux page group. 2) Turn the small FMS Knob to select the Aux-System Status. Note the System ID and GSR1 Serial Number in the Airframe field. Activating Connext Weather Registration: After a subscriber account has been established, the system must be activated for data link features such as reporting services or Connext Weather. Activation is accomplished by entering the required access code. This process is only performed when initially setting up the system for Connext services. Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance 1) Ensure the aircraft is outside with a clear view of the sky. 2) Turn the large FMS Knob to select the MAP Page group. 3) Turn the small FMS Knob to select the MAP-WEATHER DATA LINK (CNXT) Page. 4) Press the MENU Key. If necessary, select ‘Display Connext Weather’. 5) Press ENT Key. The ‘CONNEXT REGISTRATION’ Window is now displayed. 6) Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field. 7) Press the ENT Key. REGISTER will now be highlighted. 8) Press the ENT Key. System registration is complete when ‘REGISTERED’ is displayed in the STATUS field. Index Accessing Connext Weather Products 60 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link (CNXT) Page. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance 60 Continuous Meteorological Aerodrome Report (METARs) 90 Continuous Winds Aloft (WIND) 90 Continuous Pilot Weather Report (PIREPs) 90 Continuous 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index SIGMETs/AIRMETs (SIG/AIR) Appendix Continuous Annun/Alerts 30 Additional Features Datalink Lightning (DL LTNG) AFCS 30 Hazard Avoidance 60 Flight Management Infrared Satellite (IR SAT) Nav/Com/ XPDR/Audio Radar Precipitation (PRECIP) Symbol Expiration Broadcast Rate Time (Minutes) (Minutes) U.S.: 3* Canada: 3*† 30 Europe: 15 Australia: 15ˆ EIS Garmin Connext Weather Product Flight Instruments When a weather product is selected for display on the Weather Data Link (CNXT) Page, a box containing a symbol for the product and its age (in minutes) are shown in the upper right. If weather data has not been requested, ‘N/A’ is shown next to the product symbol instead of age. The age of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time. Weather products are updated continuously or refreshed at specific intervals (defined in the Broadcast Rate column in the following table). If for any reason, a weather product is not refreshed within the defined Expiration Time intervals, the data is considered expired and is removed from the display. The age of the expired product is replaced by dashes. If more than half of the expiration time has elapsed, the color of the product age readout changes to yellow. The refresh rate represents the interval at which the Garmin Connext groundbased servers make available the most current known weather data. It does not necessarily represent the rate at which new content is received from weather sources. 61 Garmin Connext Weather Product Temporary Flight Restrictions (TFRs) Terminal Aerodrome Reports (TAFs) Symbol Expiration Broadcast Rate Time (Minutes) (Minutes) no product image 60 Continuous no product image 60 Continuous * The composite precipitation image is updated every 3 minutes, but individual radar sites may take between 3 and 10 minutes to provide new data. † Canadian radar precipitation data provided by Environment Canada. ˆ Australian radar precipitation data provided by the Australian Bureau of Meteorology. Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance Annun/Alerts Additional Features AFCS Hazard Avoidance Setting up and customizing the Weather Data Link (CNXT) Page: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’, and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/ OFF, maximum map range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Weather Data Link (CNXT) Page with the changed settings. Index Appendix Restoring default Weather Data Link (CNXT) Page settings: 62 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Press the MENU Key. 5) Highlight the desired default(s) to restore (all or for selection) and press ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments Viewing Legends for Displayed Connext Weather Products 1) Select the Weather Data Link (CNXT) Page. 2) Press the LEGEND Softkey to display the legends for the displayed weather products. EIS Or: a) Press the MENU Key. Turn the FMS Knob to scroll through the legends if more are available than fit in the window. 4) To remove the Legend Window, press the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. Setting up and customizing weather data for the Navigation Map Page: Hazard Avoidance 2) Press the MENU Key. 3) With ‘Map Settings’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/ OFF, range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Additional Features Select the Navigation Map Page. 2) Press the Legend Softkey to display the legends for the displayed weather products. 63 Index Select the Weather Data Link (CNXT) Page. Appendix 1) Annun/Alerts Viewing legends for displayed weather products on the Weather Data Link (CNXT) Page: Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series AFCS 1) 190-02042-00 Rev. B Flight Management 3) Nav/Com/ XPDR/Audio b) Select ‘Weather Legend’ and press the ENT Key. EIS Flight Instruments Hazard Avoidance Connext Weather Data Requests The Connext Data Request window provides the flight crew with the options to define the requested weather coverage area(s), choose automatic weather update intervals (if desired), and the ability to send or cancel weather data requests. The window also displays the status of the Connext data request process. Flight Management Nav/Com/ XPDR/Audio Manually Requesting Garmin Connext Weather information: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key. 4) Turn the large FMS Knob to highlight the desired coverage option(s) and press the ENT Key to show or hide a green check mark to select one of more of the following coverage selections: • Present Position – Requests data based on current location. Hazard Avoidance • Destination – Requests data based on the active flight plan destination (Direct-To destinations excluded). See the Flight Management section for more information about entering and activating flight plans. Additional Features AFCS • FPL – Requests data along an active flight plan, if one currently exists. Turn the small FMS Knob to select the desired flight plan lookahead distance option (or choose ‘Remaining FPL’ to request weather data for the remainder of the flight plan), then press the ENT Key. Index Appendix Annun/Alerts • Waypoint – Requests data based on a waypoint (which may be offroute). Turn the large and small FMS Knobs to enter a waypoint, then press the ENT Key. 5) Turn the large FMS Knob highlight to the ‘Diameter / Route Width’ distance field and turn the small FMS Knob to select the desired diameter and route width of the request, then press the ENT Key. 6) Turn the large FMS Knob until the ‘Send Request’ field is highlighted. Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Weather Data Link (CNXT) Page without requesting weather data. During a Connext Data Request, the REQUEST STATUS window initially displays “Contacting Connext...”. Once a connection is established, the REQUEST STATUS window displays “Receiving Wx Data... Time Remaining:” with an estimated data 64 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance 65 Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Appendix 190-02042-00 Rev. B Annun/Alerts Connext Comm Error [4] The system has disabled automatic weather data requests due to excessive errors. Automatic weather data requests have stopped. Send a manual weather data request to resume automatic updates. The system will attempt another automatic weather data request after an error occurred during the previous request. Timer counts down until the next automatic request occurs. A general error has occurred. If the error persists, the system should be serviced. A communications error has occurred with the GDL59 or GIA. The system should be serviced. A general error has occurred. If the error persists, the system should be serviced. This occurs if multiple automatic weather data requests have recently failed, or the GDL 59 or a GIA is off-line. Additional Features Connext Comm Error [3] AFCS Connext Comm Error [2] Hazard Avoidance Connext Comm Error [1] Flight Management Auto update retry: ## Seconds Nav/Com/ XPDR/Audio Auto requests inhibited Send manual request to reset. Description EIS Weather Request Status Message Flight Instruments transfer time (either in minutes or seconds). If desired, the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob; the data request will continue to process in the background. Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area(s), the amount of weather activity present (such as precipitation), and the Iridium signal strength. The system retrieves all available Garmin Connext weather products within the selected coverage area(s) during an initial Connext Data Request. Enabling or disabling the display of the weather product does not affect which weather products are retrieved during a Connext Data Request. To reduce data usage during subsequent requests, the system retains previously retrieved textual weather products such as METARs and TAFs, so long as they have not expired. The system also retrieves any new textual weather products matching the current coverage area, and all graphical weather products during each data request. If the Connext Data Request was successful, the REQUEST STATUS window (if shown) indicates ‘OK’. Refer to the Abnormal Operations discussion later in this section for more information on the messages received if the request is unsuccessful, with possible causes. Hazard Avoidance Flight Instruments Weather Request Status Message EIS Connext Comm Error [5] Connext Comm Error [7] Connext Comm Error [8] This can occur if the GDL 59 is off-line or not configured, or the Iridium or Garmin Connext services are not accessible. Check Iridium signal strength. If this error persists, the system should be serviced. A communications error has occurred. It this error persists, the system should be serviced. A weather data transfer has timed out. Check Iridium signal strength and re-send the data request. A server error has occurred or invalid data received. An error occurred while reading or writing data. If the error persists, the system should be serviced. There is a problem with the Garmin Connext registration. Contact Garmin at 1-866-739-5687 in the United States or Connext Login Invalid 913-397-8200, wait for the operator, and request Extension 1135 for assistance. The Garmin Connext Weather data server is temporarily out Connext Server Temp Inop of service, but is expected to return to service in less than 30 minutes. The Garmin Connext Weather data server will be out of Connext Server Inop service for at least 30 minutes. The weather data request coverage area does not contain at least one of the following: a waypoint, a flight plan, or a Invalid Coverage Area flight plan destination. Verify at least one of the coverage options is enabled (checked) and contains required criteria, then re-send the data request. The system is not be currently subscribed to Garmin Connext services or the access code is incorrect. Verify the access No Connext Subscription code. Contact Garmin at 1-866-739-5687 in the United States or 913-397-8200, wait for the operator, and request Extension 1135 for assistance. Connext Comm Error [9] Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio Connext Comm Error [6] Description 66 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Description The weather data request timed-out. Re-send data request. Transfer Preempted The GDL 59 is busy. Retry request later. Nav/Com/ XPDR/Audio Request Failed - Try Again EIS Request Canceled The size of the received weather data has exceeded system memory limits. Reduce the size of the coverage area and issue another Connext Data Request to ensure all available weather data has been received. The user has cancelled a Connext Data Request. Reduce Request Area Flight Instruments Weather Request Status Message Abnormal Weather Data Request Status Messages Flight Management Cancelling a Connext Data Request in Progress: 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key. 4) Turn the large FMS Knob to select the ‘Cancel Request’ field and press the ENT Key. The request status box indicates ‘Request Cancelled’. 5) Press the FMS Knob to return to the Weather Data Link (CNXT) Page. AFCS Select the Weather Data Link (CNXT) Page. Hazard Avoidance 1) Enabling/disabling automatic Connext Data Requests: Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key. 4) Choose the desired weather coverage options. 5) Turn the large FMS Knob to select the ‘Update Rate’ field. Then turn the small FMS Knob to highlight the desired automatic update frequency (Off, 5 Min, 10 Min, 15 Min, 20 Min, 30 Min, 45 Min, or 60 Min), then press the ENT Key. 6) The ‘Send Request’ field is highlighted and a countdown timer is displayed in the ‘Request Status’ Window based on the currently selected update rate. Press the ENT Key to immediately send an immediate Connext Data Request. Index 67 Appendix Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Annun/Alerts 190-02042-00 Rev. B Additional Features 1) FIS-B WEATHER WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. EIS Flight Instruments Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be older than the indicated weather product age. 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link (FIS-B, XM, or CNXT) Page. 3) If the page title displays a weather data link weather source other than ‘FIS-B’, such as ‘XM’ or ‘CNXT’, proceed to the following steps to change the data link weather source. 4) Press the MENU Key. 5) Turn the small FMS Knob to select ‘Display FIS-B Weather’ and press the ENT Key. The page title will display ‘Map - Weather Data Link (FIS-B)’ to indicate FIS-B is now the selected data link weather source. Additional Features AFCS Hazard Avoidance Viewing the Weather Data Link (FIS-B) Page: 1) Select the Weather Data Link (FIS-B) Page. 2) Press the MENU Key. 3) Turn the small FMS Knob to highlight ‘Enable FIS-B Weather’ or ‘Disable FIS-B Weather’, and press the ENT Key. Index Appendix Annun/Alerts Enabling/disabling the FIS-B weather feature: 68 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Broadcast Rate (Minutes) 30 15 30 2.5 90 5 90 10 90 10 60 5 no product image 30 2.5 no product image 60 10 FIS-B Weather Product Symbol NEXRAD Composite (US) Flight Instruments Expiration Time (Minutes) EIS no product image AFCS Terminal Aerodrome Forecast Temporary Flight Restriction (TFR) Hazard Avoidance No Radar Coverage Flight Management Winds Aloft (WIND) SIGMETs/AIRMETs (SIG/AIR) Nav/Com/ XPDR/Audio NEXRAD Composite (Regional) Meteorological Aerodrome Report (METARs Pilot Weather Report (PIREPs) 10 Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Settings’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/ OFF, range settings). Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Appendix 190-02042-00 Rev. B Annun/Alerts 1) Additional Features Setting up and customizing FIS-B weather data for the Navigation Map Page: 69 Flight Instruments Hazard Avoidance 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Setting up and customizing the Weather Data Link (FIS-B) Page: 1) Select the Weather Data Link (FIS-B) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select ‘Product Group 1’, and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/ OFF, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Weather Data Link (FIS-B) Page with the changed settings. Additional Features AFCS Displaying/removing the weather product information box on the PFD Inset Map: 1) On the PFD, press the Map/HSI Softkey (Map Opt Softkey in TCAS II installations). 2) Press the Layout Softkey. 3) Press the WX LGND Softkey. Appendix Annun/Alerts Viewing legends for displayed weather products on the Weather Data Link (FIS-B) Page: 1) Select the Weather Data Link (FIS-B) Page. 2) Press the Legend Softkey to display the legends for the displayed weather products. Index Viewing legends for displayed weather products (on the Navigation Map Page): 70 1) Select the Navigation Map Page. 2) Press the Map Opt Softkey. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Press the Legend Softkey (available if one or more FIS-B weather products are enabled for display). 4) To remove the Legend Window, press the Legend Softkey, the ENT or the CLR Key, or press the FMS Knob. EIS AIRBORNE COLOR WEATHER RADAR Hazard Avoidance Displaying Weather on the Weather Radar Page 2) Press the Mode Softkey. 3) While on the ground, press the Standby Softkey. For the GWX 68 only, a one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar enters the Standby Mode. The warm-up period is not applicable to the GWX 70. a) Press the Weather Softkey. A confirmation window is displayed. Or: The horizontal scan is initially displayed. If desired, press the Vertical Softkey to change to vertical scanning. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 5) Appendix If the aircraft is airborne, press the Weather Softkey. For the GWX 68 only, a one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar begins transmitting. The warm-up period is not applicable to the GWX 70. Annun/Alerts b) Turn the small FMS Knob to highlight YES and press the ENT Key to continue radar activation. Additional Features Select the Weather Radar Page in the Map Page Group with the FMS Knob. AFCS 1) Turn the Joystick to select the desired map range. Flight Management CAUTION: In Standby Mode, the antenna is parked at the center line. It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly. Nav/Com/ XPDR/Audio WARNING: Begin transmitting only when it is safe to do so. If it is desired to transmit while the aircraft is on the ground, no personnel or objects should be within 12 feet of the antenna. 4) Flight Instruments 3) 71 Weather Mode Color Intensity Approximate Precipitation Rate (in/hr.) Black < 23 dBZ < .01. Green 23 dBZ to < 32 dBZ .01 - 0.1. Yellow 32 dBZ to < 41 dBZ 0.1 - 0.5 Red 41 dBZ to < 50 dBZ 0.5 - 2 Magenta 50 dBZ and greater >2 Precipitation Intensity Levels in Weather Mode (GWX 68) Weather Mode Color Intensity Approximate Precipitation Rate (in/hr.) Black < 23 dBZ < .01 Green 23 dBZ to < 33 dBZ .01 - 0.1 Yellow 33 dBZ to < 41 dBZ 0.1 - 0.5 Red 41 dBZ and greater greater than 0.5 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance AFCS Magenta (Optional) TURB- (Optional) Turbulence Detection uses the color magenta to show areas of rain or hail that may also contain turbulence Precipitation Intensity Levels in Weather Mode (GWX 70) Additional Features Vertically Scan a Storm Cell Annun/Alerts NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant adjustment of the Bearing Line. 1) While in the Horizontal Scan view, press the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line. If the Bearing Line is not displayed, press the MENU Key and turn the large Index Appendix FMS Knob to select Show Bearing Line. Press the ENT Key. 72 2) Press the ENT Key. 3) Turn the small FMS Knob to place the Bearing Line on the desired storm cell or other area to be vertically scanned. 4) Press the Vertical Softkey. A vertical scan of the selected area is now displayed. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance 6) Turn the Joystick to adjust the range. 7) Press the FMS Knob to remove the cursor. 8) To select a new area to be vertically scanned, press the Horizon Softkey to return to the Horizontal Scan view and repeat the previous steps. Press the FMS Knob to activate the cursor in the TILT field. 2) Turn the small FMS Knob to select the desired antenna tilt angle. 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. Flight Management 1) Nav/Com/ XPDR/Audio Adjusting antenna tilt on the Horizontal Scan display Adjusting antenna tilt on the Vertical Scan display Press the Tilt Softkey to activate the cursor in the TILT field and display the Tilt Line. Hazard Avoidance 1) EIS The small FMS Knob may be used to move the scanned bearing line a few degrees right or left. Flight Instruments 5) If the Tilt Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Tilt Line. Press the ENT Key. Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is again selected. Additional Features The Joystick can also be used to adjust tilt. Enabling/disabling manual gain adjustment Turn the small FMS Knob to adjust the gain for the desirable level. The gain setting is visible in the Gain field as a movable horizontal bar in a flashing box. The line pointer is a reference depicting the calibrated position. 3) Press the FMS Knob to remove the cursor. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 2) Appendix Press the Gain Softkey to activate the cursor in the Gain field. Annun/Alerts WARNING: Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation. 1) AFCS 2) 73 Hazard Avoidance Flight Instruments 4) Press the Gain Softkey again to return to the calibrated gain setting. ‘Calibrated’ is displayed in the Gain field. Enabling/disabling Sector Scanning While in horizontal scan mode, press the BRG Softkey to display the Bearing Line and place the cursor in the BEARING field. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. 2) Press the ENT Key. 3) Turn the small FMS Knob to place the Bearing Line in the desired position. The location of the Bearing Line becomes the center point of the Sector Scan. 4) Turn the large FMS Knob to place the cursor in the Sector Scan field. 5) Turn the small FMS Knob to highlight the desired scan. Selecting ‘Full’ enables a 90º scan (GWX 68) or 120º scan (GWX 70). 6) If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan. 7) Press the BRG Softkey again to remove the Bearing Line and cursor. The bearing reference is reset to 0º. AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS 1) Annun/Alerts Additional Features Enabling/disabling antenna stabilization 1) On the Weather Radar Page, press the Mode Softkey. 2) Press the STAB Softkey to enable/disable antenna stabilization. The current stabilization condition is, ‘STAB ON’ or ‘STAB OFF’ is shown in the upper right of the Weather Radar Page. 1) Select the Weather Radar Page. 2) To activate or deactivate the turbulence detection feature, press the TURB Softkey. Turbulence detection is enabled when the softkey annunciator is green; turbulence detection is disabled when the softkey annunciator is gray. The system indicates the current turbulence detection feature status in the upper right of the Weather Radar Page. Index Appendix Enabling/Disabling Turbulence Detection during a Horizontal Scan 74 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Select the Weather Radar Page. 2) Press the Mode Softkey. 3) To enable or disable the ground clutter suppression feature, press the GCS Softkey. Ground clutter suppression is enabled when the softkey annunciator is green; ground clutter suppression is disabled when the annunciator is gray. EIS 1) Flight Instruments Enabling/disabling Ground Clutter Suppression Nav/Com/ XPDR/Audio Operation in Ground Map Mode 2) Press the Ground Softkey to place the radar in Ground Map mode. 3) Press the Back Softkey. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to place the cursor in the Tilt field. 6) Adjust the antenna tilt angle by turning the small FMS Knob to display ground returns at the desired distance. 7) Press the FMS Knob to remove the cursor. Cyan Yellow Blue 0 dB > 0 dB to < 9 dB 9 dB to < 18 dB 18 dB to < 27 dB 27 dB and greater Annun/Alerts Magenta Intensity Additional Features Black AFCS Ground Map Mode Color Hazard Avoidance Press the Mode Softkey. Flight Management 1) Ground Target Return Intensity Levels Select the Navigation Map Page. 2) Press the Map Opt Softkey. 3) Press the WX Radar Softkey. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 1) Appendix Enabling/disabling Airborne Weather Radar Overlay on the Navigation Map Page 75 Hazard Avoidance 1) With the weather radar overlay enabled, push the Joystick twice. The bearing and tilt legend is displayed. 2) Move the Joystick up to adjust the antenna tilt angle downward, or move the Joystick up to adjust the antenna tilt angle upward. 3) Move the Joystick left or right to adjust the bearing line in the desired direction. The bearing line is displayed during and momentarily after adjustment. Nav/Com/ XPDR/Audio EIS Flight Instruments Adjusting the bearing and antenna tilt angle on the Navigation Map Page 1) If necessary, enable the HSI Map on the PFD. 2) On the PFD, press the Map/HSI Softkey (in TCAS II installations, press the Map Opt Softkey). 3) Press the Wx Radar Softkey to enable/disable the airborne weather radar HSI Map overlay. 4) Press the RDR Opt Softkey. 5) To select a weather radar mode, press the Mode SEL Softkey AFCS Hazard Avoidance Flight Management Controlling weather radar information on the HSI Map: a) Press a softkey for the desired mode: Off, Standby, Weather, or Ground. The selected mode only affects the PFD on which the softkey is selected. Appendix Annun/Alerts Additional Features b) When finished, press the Back Softkey. 6) Press the Gain- Softkey to decrease the gain setting or press the Gain+ Softkey to increase the gain setting in increments of 0.5 with each press, or press and hold the softkey for continuous adjustment. A gain setting of 0.0 is equivalent to the calibrated gain setting. 7) Move the PFD Joystick up to adjust the antenna tilt angle downward, or move the Joystick down to adjust the antenna tilt angle upward. 8) Press the STAB Softkey to enable/disable antenna stabilization feature. 9) Press the ACT Softkey to enable/disable the Altitude Compensated Tilt feature. Index 10) When finished adjusting the HSI Map display of the airborne weather radar, press the Back Softkey. 76 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance WARNING: Do not use TAWS information for primary terrain avoidance. TAWS is intended only to enhance situational awareness. Flight Management Enabling/disabling relative terrain information on MFD navigation maps Nav/Com/ XPDR/Audio NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data. EIS NOTE: Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area. Flight Instruments TERRAIN AWARENESS & WARNING SYSTEM (TAWS-A AND TAWS-B) Press the Map Opt Softkey. 2) Press the TER Softkey to cycle through terrain options. The selected mode is displayed in cyan: Off, Topo, Rel. Press the TER Softkey until ‘Rel’ is displayed on the softkey. Hazard Avoidance 1) Displaying relative terrain information (PFD Maps) Press the Map/HSI Softkey (Map Opt Softkey for TCAS II installations). 2) Press the Rel Ter Softkey. AFCS 1) Additional Features TAWS On-Ground Legend TAWS In-Air Legend Annun/Alerts Appendix TAWS Relative Terrain Legends Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 77 Hazard Avoidance 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Settings’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. Nav/Com/ XPDR/Audio EIS Flight Instruments Customizing terrain and obstacle display on the Navigation Map Page: • Terrain Display – Selects the display of topo, relative terrain, or no terrain, and selects the maximum map range at which terrain is shown Hazard Avoidance Flight Management • Obstacle Data – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown 6) Turn the small FMS Knob to scroll through options for each product (ON/ OFF, range settings). 7) 8) Press the ENT Key to select an option. Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. AFCS Displaying the TAWS Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS-B Page. Additional Features Showing/hiding aviation information on the TAWS Page Annun/Alerts 1) Press the MENU Key. 2) Turn the FMS Knob to highlight ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key. 1) Select the TAWS Page. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight ‘Test TAWS System’ and press the ENT Key to confirm the selection. Index Appendix Manually testing the TAWS System 78 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments Inhibiting/enabling FLTA and PDA alerting 1) Select the TAWS Page. 2) Press the TAWS INH Softkey to inhibit or enable TAWS (choice dependent on current state). EIS Or: Press the MENU Key. 2) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key. Overriding Flaps-based FIT alerting (TAWS-A Only) Select the TAWS-A Page 2) Press the Flap OVR Softkey Flight Management 1) Or: Press the MENU Key. 2) Select ‘Flap Override’ or ‘Disable Flap Override’ (choice dependent on current state) and press the ENT Key. Hazard Avoidance 1) Nav/Com/ XPDR/Audio 1) Inhibiting/enabling GPWS alerting (TAWS-A Only) 2) Press the GPWS INH Softkey to inhibit or enable GPWS alerts (choice dependent on current state). Additional Features Select the TAWS-A Page. AFCS 1) Or: a) Press the MENU Key. Annun/Alerts b) Select ‘Inhibit GPWS’ or ‘Enable GPWS’ (choice dependent on current state) and press the ENT Key. Inhibiting/Enabling GSD alerting (only available during a GSD alert) (TAWS-A Only) Select the TAWS-A Page. 2) Press the GS INH or GP INH Softkey to inhibit or enable GSD alerts (softkey choice dependent on present GSD alert type). Appendix 1) 190-02042-00 Rev. B Index Or: Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 79 Flight Instruments Hazard Avoidance 1) Press the MENU Key. 2) Select the option to inhibit or enable the glideslope or glidepath alerting (choice dependent on present GSD alert type) and press the ENT Key. EIS VERTICAL SITUATION DISPLAY (VSD) Flight Management Nav/Com/ XPDR/Audio Enabling/Disabling the Vertical Situation Display (VSD) 1) Select the Navigation Map Page. 2) Press the Map Opt Softkey. 3) Press the Inset Softkey. 4) Press the VSD Softkey to enable or disable the VSD. Hazard Avoidance Enabling/Disabling VSD Relative Terrain on the Navigation Map (when VSD is enabled) 1) Select the Navigation Map Page. 2) Press the Map Opt Softkey. AFCS 3) Press the Terrain Softkey. Each selection cycles though an option displayed in cyan: Off (disables terrain), Topo (to show topographical data) or REL (to show relative terrain). Annun/Alerts Additional Features Selecting a VSD Mode 1) Select the Navigation Map Page. 2) Press the Inset Softkey. 3) Press the VSD Softkey displaying the VSD mode in cyan. Each press of the softkey cycles through a mode selection: FPL (flight plan), TRK (track), or Auto. Index Appendix Customizing the Track Mode Boundary display on the Navigation Map Page 80 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Settings’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select the ‘VSD’ Group and press the ENT Key. 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments • TRK Mode BNDRY – Enables/disables the display of the Track Mode Boundary and sets maximum range at which Track Mode Boundary is shown. Turn the small FMS Knob to scroll through options (ON/OFF, range settings). 7) 8) Press the ENT Key to select an option. Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Hazard Avoidance WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. Flight Management WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. Nav/Com/ XPDR/Audio TRAFFIC AVOIDANCE SYSTEMS EIS 6) AFCS Traffic Symbol Description Annun/Alerts • If a Traffic Advisory System (TAS) or Traffic Collision Avoidance System (TCAS I) is configured, a STANDBY, OPERATE, TEST, and ALT MODE Softkey will be displayed. Additional Features TRAFFIC ADVISORY SYSTEM (TAS)/TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS I) Non-Threat Traffic Appendix Proximity Advisory (PA)(TAS only, not available with TIS) Traffic Advisory (TA) Index Traffic Advisory Off Scale TAS/TCAS I Symbol Description 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 81 Hazard Avoidance Flight Instruments Traffic Symbol Description Traffic Advisory with ADS-B directional information. Points in the direction of the intruder aircraft track. EIS Proximity Advisory with ADS-B directional information. Points in the direction of the aircraft track. Other Non-threat traffic with ADS-B directional information. Points in the direction of the intruder aircraft track. Nav/Com/ XPDR/Audio TAS/TCAS I with ADS-B Symbology (GTX 33/335 Transponder) Flight Management Symbol Description Traffic Advisory with directional information. Points in the direction of the intruder aircraft track. Hazard Avoidance Traffic Advisory without directional information. Traffic Advisory out of the selected display range with directional information. Displayed at outer range ring at proper bearing. AFCS Traffic Advisory out of the selected display range without directional information. Displayed at outer range ring at proper bearing. Additional Features Proximity Advisory with directional information. Points in the direction of the aircraft track. Proximity Advisory without directional information. Annun/Alerts Other Non-Threat traffic with directional information. Points in the direction of the intruder aircraft track. Other Non-Threat traffic without directional information. Index Appendix Traffic located on the ground with directional information. Points in the direction of the aircraft track. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode or own aircraft is on the ground. Ground traffic without directional information. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode or own aircraft is on the ground. Non-aircraft ground traffic. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode or own aircraft is on the ground. TAS/TCAS I with ADS-B Symbology (GTX 345 Transponder) 82 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments Traffic Advisory System (TAS) or Traffic Collision Avoidance System (TCAS I) (Optional) Testing the traffic system: 1) Turn the large FMS Knob to select the Map Page Group. EIS 2) Turn the small FMS Knob to select the Traffic Map Page. 4) Press the Test Softkey. Nav/Com/ XPDR/Audio 3) Turn the Joystick to set the range to 2/6 nm to allow for full traffic test pattern display. Displaying Traffic on the Traffic Map Page: Flight Management 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 4) Press the TAS STBY Softkey to place the system in the Standby mode. ‘STANDBY’ is displayed in the Traffic mode field. AFCS Enabling/disabling traffic information (MFD maps other than the Traffic Map Page): Hazard Avoidance 3) Press the TAS OPER Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic mode field. 1) Press the Map Opt Softkey. Additional Features 2) Press the Traffic Softkey. Traffic is now displayed on the map. Enabling/disabling traffic information on the PFD Inset Map or HSI Map: Annun/Alerts 1) On the PFD, press the Map/HSI Softkey. 2) Press the Traffic Softkey to enable/disable the display traffic information on the Inset Map or HSI Map. Appendix Traffic Advisory System (TAS, L-3 Skywatch) (Optional) Switching from standby mode to operating mode: 2) If using the FMS menu, press the ENT Key to place the traffic system in the operating mode. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 83 Index 1) On the Traffic Page, press the TAS OPER Softkey or press the MENU Key and turn the small FMS knob to select Operating Mode. Hazard Avoidance Flight Instruments 3) To switch to Standby Mode from the Traffic Page, press the TAS STBY Softkey. Testing the traffic system: EIS 1) Set the range to 2/6 nm to allow for full test pattern display. 2) Press the Standby Softkey. 3) Press the Test Softkey. ‘TEST MODE’ is annunciated on the MFD. Nav/Com/ XPDR/Audio 4) Self test takes approximately eight seconds to complete. When completed successfully, traffic symbols display and a voice alert is heard to indicate the system test passed. Flight Management Displaying Traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. Hazard Avoidance 3) Press the Operate Softkey to begin displaying traffic. ‘Operating’ is displayed in the Traffic mode field. 4) Press the ALT Mode Softkey to change the altitude volume. AFCS 5) Press the Standby Softkey to place the system in the Standby mode. ‘Standby’ is displayed in the Traffic mode field. 6) Turn the Joystick clockwise to display a larger area or counterclockwise to display a smaller area. Additional Features Enabling/disabling traffic information (MFD maps other than the Traffic Map Page): Annun/Alerts 2) Press the Traffic Softkey. Traffic is now displayed on the map. Appendix 1) Press the Map Opt Softkey. 1) On the PFD, press the Map/HSI Softkey. Enabling/disabling traffic information on the PFD Inset Map or HSI Map: Index 2) Press the Traffic Softkey to enable/disable the display traffic information on the Inset Map or HSI Map. 84 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance Flight Instruments Traffic Advisory System (TAS, Honeywell KTA 870) (Optional) Switching from standby mode to operating mode: On the Traffic Page, press the Standby Softkey EIS Or: 1) Press the MENU Key and turn the small FMS knob to select Standby Mode. Nav/Com/ XPDR/Audio 2) Press the ENT Key. Testing the traffic system: 1) Set the range to 2/6 nm to allow for full test pattern display. Flight Management 2) Press the Test Softkey. Hazard Avoidance 3) Self test takes approximately eight seconds to complete. When completed successfully, traffic symbols are displayed and a voice alert “TAS System Test OK” is heard. In the event that the system test fails, the system reverts to Standby Mode and a voice alert “TAS System Test Fail” is heard. Displaying Traffic on the Traffic Map Page AFCS 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. Additional Features 3) Press the Normal Softkey to begin displaying traffic. OPERATING is displayed in the Traffic mode field. 4) Press the Alt Mode Softkey to change the altitude volume. Annun/Alerts 5) Press the Standby Softkey to place the system in the Standby mode. ‘STANDBY’ is displayed in the Traffic mode field. 6) Turn the Joystick clockwise to display a larger area or counterclockwise to display a smaller area. Appendix Enabling/disabling traffic information (MFD maps other than the Traffic Map Page): 1) Press the Map Softkey. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 2) Press the Traffic Softkey. Traffic is now displayed on the map. 85 Hazard Avoidance Flight Instruments Enabling/disabling traffic information on the PFD Inset Map or HSI Map: 1) Press the Map/HSI Softkey (Map Opt Softkey for TCAS II installations). EIS 2) Press the Traffic Softkey to enable/disable the display traffic information on the Inset Map or HSI Map. Nav/Com/ XPDR/Audio ADS-B TRAFFIC (GTX 345 ONLY) (Optional) Flight Management Enabling/disabling the display of ADS-B traffic. 1) Select the Traffic Map Page. 2) Press the ADS-B Softkey. AFCS Hazard Avoidance Testing the display of ADS-B traffic: 1) Select the Traffic Map Page. 2) If necessary, turn the Joystick to select a map range of 2 and 6 nm to ensure full test pattern display. 3) Ensure the the ADS-B Softkey is disabled. 4) If the optional TAS/TCAS I is installed, ensure the TAS STBY or TCAS STBY Softkey is enabled. 5) Press the Test Softkey. Annun/Alerts Additional Features Enabling/disabling ADS-B traffic information (MFD maps other than the Traffic Map Page): 1) Press the Map Opt Softkey. 2) Press the Traffic Softkey. Traffic is now displayed on the map. 1) Press the Map/HSI Softkey (Map Opt Softkey for TCAS II installations). 2) Press the Traffic Softkey to enable/disable the display traffic information on the Inset Map or HSI Map. Index Appendix Enabling/disabling ADS-B traffic information on the PFD Inset Map or HSI Map: 86 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance NOTE: If the installed TCAS II traffic system is not a Garmin GTS 8000, refer to the applicable documentation for system-specific information. Description Nav/Com/ XPDR/Audio Traffic Symbol EIS • If a Traffic Collision Avoidance System (TCAS II) is configured, an REL, ABS, TFC STBY, TA ONLY, TA/RA, TEST, and ALT RNG Softkey will be displayed. Flight Instruments TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS II) (OPTIONAL) Flight Management Non-Threat Traffic (intruder is beyond 5 nm and greater than 1200’ vertical separation) Proximity Advisory (PA)(TAS only, not available with TIS) (intruder is within 5 nm and less than 1200’ vertical separation) Traffic Advisory (TA) (closing rate, distance, and vertical separation meet TA criteria) Hazard Avoidance Traffic Advisory Off Scale Resolution Advisory (RA)(TCAS II only) (Potential collision area is within 15 to 35 seconds) Resolution Advisory Off Scale (TCAS II only) AFCS Traffic Symbol Description Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Turn the Joystick to set the range to 2/6 nm to allow for full traffic test pattern display. 4) Press the Test Softkey. Annun/Alerts 1) Additional Features Testing The TCAS II System Appendix Displaying Traffic On the Traffic Map Page Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Press the TA Only or TA/RA Softkey to begin displaying traffic. ‘TA ONLY’ or ‘TA/RA’ is displayed in the Traffic mode field. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 87 Index 1) Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance 4) Press the Relative or Absolute Softkey to display the relative or absolute altitude of other aircraft. When absolute altitude is displayed, the system may revert to displaying relative altitude after 30 seconds if the TCAS II system is providing altitude which is not corrected for the local barometric pressure setting. 5) Press the TFC STBY Softkey to place the system in the Standby mode. ‘STANDBY’ is displayed in the Traffic mode field. 6) Turn the Joystick clockwise to display a larger area or counter-clockwise to display a smaller area. Flight Management Switching from standby mode to TA only or TA/RA mode 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Press the TA ONLY or TA/RA Softkey AFCS Hazard Avoidance Changing the Altitude Range 1) Press the XPDR/TFC Softkey. 2) Press the TCAS Softkey. 3) Press the ALT RNG Softkey. 4) Press one of the following altitude range softkeys: Additional Features Above: Displays non-threat and proximity traffic from 9900 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. Annun/Alerts Normal: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. Appendix Below: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight. UNREST (unrestricted): All traffic is displayed. Press the BACK Softkey. Index 5) 88 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Hazard Avoidance 1) Press the Map Opt Softkey. 2) Press the Traffic Softkey. Traffic is now displayed on the map. Flight Instruments Displaying Traffic Information on MFD Navigation Maps: EIS Enabling/Disabling Traffic Information On The PFD Inset Map or HSI Map Press the Map Opt Softkey. 2) Press the Traffic Softkey to enable/disable the display traffic information on the Inset Map or HSI Map. Nav/Com/ XPDR/Audio 1) Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 89 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Hazard Avoidance Index Appendix Annun/Alerts Additional Features AFCS Blank Page 90 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B AFCS NOTE: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages. EIS ACTIVATING THE FLIGHT DIRECTOR Modes Selected Lateral Vertical ROL Pitch Hold (default) PIT AP Key Roll Hold (default) ROL Pitch Hold (default) PIT CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT GA Button Takeoff (on ground) Go Around (in air) TO GA Takeoff (on ground) Go Around (in air) TO GA ALT Key Roll Hold (default) ROL Altitude Hold ALT VS Key Roll Hold (default) ROL Vertical Speed VS Hazard Avoidance Roll Hold (default) Flight Management FD Key Nav/Com/ XPDR/Audio An initial press of a key listed in the following table (when the flight director is not active) activates the pilot-side flight director in the listed modes. Control Pressed Flight Instruments AUTOMATIC FLIGHT CONTROL SYSTEM ROL Flight Level Change FLC Roll Hold (default) ROL Vertical Path Tracking* VPTH NAV Key Navigation** GPS VOR LOC Pitch Hold (default) PIT BC Key Backcourse*** BC Pitch Hold (default) PIT APR Key Approach** GPS VOR LOC Pitch Hold (default) PIT HDG Key Heading Select HDG Pitch Hold (default) PIT Additional Features Roll Hold (default) AFCS FLC Key VNV Key Annun/Alerts *Valid VNV flight plan must be entered before VNV Key press activates flight director. ***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director. Appendix **The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 91 VERTICAL MODES Vertical Mode Description Control Annunciation Pitch Hold Holds the current aircraft pitch attitude; may be used to climb/descend to the Selected Altitude (default) PIT Selected Altitude Capture Captures the Selected Altitude * ALTS Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn ft Vertical Speed Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude VS Key VS nnnn fpm Flight Level Change, Maintains the current aircraft airspeed (in IAS Hold IAS or Mach) while the aircraft is climbing/ Flight Level Change, descending to the Selected Altitude Mach Hold FLC nnn kt FLC Key FLC M .nnn Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments AFCS * ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNV Target Altitude Index Appendix Annun/Alerts Additional Features AFCS LATERAL MODES Lateral Mode Description Control Roll Hold Holds the current aircraft roll attitude or rolls the wings level, (default) depending on the commanded bank angle Low Bank Limits the maximum commanded roll angle Heading Select Captures and tracks the Selected HDG Key Heading BANK Key Navigation, GPS Arm/ Capture/Track Navigation, VOR Enroute Arm/Capture/Track Navigation, LOC Arm/ Capture/Track (No Glideslope) Annunciation ROL * HDG GPS Captures and tracks the selected NAV Key navigation source (GPS, VOR, LOC) VOR LOC * No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator. 92 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B AFCS Lateral Mode Description Control Annunciation VPTH EIS ALTV Nav/Com/ XPDR/Audio GP GS Flight Management BC Hazard Avoidance GPS VAPP AFCS LOC Additional Features TO Annun/Alerts Captures and tracks descent VNV legs of an active vertical profile Key Captures the Vertical VNV Target Altitude Navigation (VNV) Target * Capture Altitude Captures and tracks the SBAS Glidepath glidepath on approach APR Key Captures and tracks the ILS Glideslope glideslope on approach Captures and tracks a Backcourse Arm/Capture/ localizer signal for backcourse BC Key Track approaches Approach, GPS Arm/ Capture/Track Approach, VOR Arm/ Captures and tracks the Capture/Track APR selected navigation source Key Approach, ILS Arm/ (GPS, VOR, LOC) Capture/Track (Glideslope Mode automatically armed) Commands a constant pitch angle and wings level on the GA Takeoff ground in preparation for Button takeoff Vertical Path Tracking Flight Instruments COMBINATION MODES (VNV, APR, NAV, BC, GA) Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 93 Lateral Mode Go Around** Level Control Annunciation Commands a constant pitch GA angle and wings level in the air Button Autopilot engages and commands pitch angle *** necessary to establish zero vertical fpm GA LVL **Go Around mode disengages the autopilot unless a compatible lift computer is installed. *** Level mode can only become activated as a function of Electronic Stability and Protection (ESP). Refer to the Additional Features section for a detailed discussion of the optional ESP feature. SUSPECTED AUTOPILOT MALFUNCTION NOTE: Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure. If an autopilot failure or trim failure is suspected to have occurred, perform the following steps: 1) Firmly grasp the control wheel. 2) Press and hold the AP/YD DISC Switch. The autopilot will disconnect and power is removed from the trim motor. Power is also removed from all primary servo motors and engaged solenoids. Note the visual and aural alerting indicating autopilot disconnect. 3) Retrim the aircraft as needed. Substantial trim adjustment may be needed. 4) Pull the appropriate circuit breaker(s) to electrically isolate the servo and solenoid components. 5) Release the AP/YD DISC Switch. Index Appendix Annun/Alerts Additional Features AFCS Description * ALTV is armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments AFCS 94 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B AFCS EIS Nav/Com/ XPDR/Audio Flight Management In the context of this discussion, “overpowering” refers to any pressure or force applied to the pitch controls when the autopilot is engaged. A small amount of pressure or force on the pitch controls can cause the autopilot automatic trim to run to an out-of-trim condition. Therefore, any application of pressure or force to the controls should be avoided when the autopilot is engaged. Overpowering the autopilot during flight will cause the autopilot’s automatic trim to run, resulting in an out-of-trim condition or cause the trim to hit the stop if the action is prolonged. In this case, larger than anticipated control forces are required after the autopilot is disengaged. The following steps should be added to the preflight check: 1) Check for proper autopilot operation and ensure the autopilot can be overpowered. 2) Note the forces required to overpower the autopilot servo clutches. Flight Instruments OVERPOWERING AUTOPILOT SERVOS Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 95 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments AFCS Blank Page 96 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Flight Instruments ADDITIONAL FEATURES SYNTHETIC VISION AFCS Additional Features Pathways Flight Path Marker Horizon Heading Marks Terrain and Obstacle Alerting Three-dimensional Traffic Airport Signs Runway Display Hazard Avoidance Annun/Alerts • • • • • • • Flight Management Synthetic Vision Technology (SVT) functionality is offered as an optional enhancement to the G1000 NXi system. SVT is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot’s perspective. SVT information is shown on the primary flight display (PFD). In addition to SVT enhancement to the PFD, the following features have been added to the PFD: Nav/Com/ XPDR/Audio WARNING: Do not use SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing. EIS WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVT is intended as an aid to situational awareness only and may not provide the accuracy and/or fidelity upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. Activating and deactivating SVT 2) Press the SVT Softkey. 3) Press the Terrain Softkey. The SVT display will cycle on or off with the Terrain Softkey. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index Press the PFD Opt Softkey. Appendix 1) 97 Additional Features 1) Press the PFD Opt Softkey. 2) Press the SVT Softkey. 3) Press the Pathways Softkey. The Pathway feature will cycle on or off with the Pathways Softkey. EIS Flight Instruments Activating and deactivating Pathways Flight Management Nav/Com/ XPDR/Audio Activating and deactivating Horizon Headings Press the PFD Opt Softkey. 2) Press the SVT Softkey. 3) Press the HDG LBL Softkey. The horizon heading display will cycle on or off with the HDG LBL Softkey. Activating and deactivating Airport Signs Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index 1) 1) Press the PFD Opt Softkey. 2) Press the SVT Softkey. 3) Press the APT Sign Softkey. Display of airport signs will cycle on or off with the APT Sign Softkey. TERMINAL PROCEDURE CHARTS NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may be necessary to carry another source of charts on-board the aircraft. SAFETAXI® SafeTaxi® is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport. The airport display on the map reveals runways with numbers, taxiways identifiers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. The aircraft symbol provides situational awareness while taxiing. Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and airport identification labels. Pressing the DCLTR Softkey twice removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing the DCLTR Softkey a third time removes the airport runway layout, unless the airport in view is part of an active route structure. Pressing the DCLTR Softkey again cycles 98 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Flight Instruments EIS back to the original map detail. The SafeTaxi database contains detailed airport diagrams for selected airports. These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways, ramps, runways, terminals, and services. This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground. This database is updated on a 56-day cycle. CHARTVIEW Nav/Com/ XPDR/Audio Flight Management ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams. The ChartView database is updated on a 14-day cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView will no longer function. Hazard Avoidance FLITECHARTS® AFCS Additional Features FliteCharts® resemble the paper version of AeroNav Services terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams. The FliteCharts database contains procedure charts for the United States only. This database is updated on a 28-day cycle. If not updated within 180 days of the expiration date, FliteCharts will no longer function. Selecting Terminal Procedures Charts Annun/Alerts While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press the Charts Softkey. Or: Press the MENU Key to display the Page Menu. 2) Turn the large FMS Knob to scroll through the Options Menu to Charts. 3) Press the ENT Key to display the chart. Appendix 1) Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 99 Selecting Additional Information 1) While viewing the Airport Taxi Diagram, press the WX Softkey to display the information windows (AIRPORT, INFO). 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the INFO Box. 4) Turn the small FMS Knob to select the INFO Box choices. When the INFO Box is selected the G1000NXi softkeys are blank. If multiple choices are available, scroll to the desired choice with the large FMS Knob and press the ENT Key to complete the selection. 5) Press the FMS Knob again to deactivate the cursor. Selecting full screen On or Off 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the Full Screen and Color Scheme Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. Selecting Day, Night, or Automatic View Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features 100 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move to the Color Scheme Option. 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. 5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to change the percentage value. The percentage value is the day/night crossover point based on the percentage of backlighting intensity. For example, if the value is set to 15%, the day/ night display changes when the display backlight reaches 15% of full brightness. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features 6) Flight Instruments The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. Press the FMS Knob when finished to remove the Chart Setup Menu. EIS AIRPORT DIRECTORY 2) Turn the small FMS Knob to select the Airport Information Page. Initially, information for the airport closest to the aircraft’s present position is displayed. 3) If necessary, select the Info softkey until Info 2 is displayed. AFCS Turn the large FMS Knob to select the ‘WPT’ page group. Hazard Avoidance 1) Flight Management Selecting the Airport Directory Page Nav/Com/ XPDR/Audio The Aircraft Owners and Pilots Association (AOPA) or AC-U-KWIK Airport Directory database offers detailed information regarding services, hours of operation, lodging options, and more for various airports. This information is viewed on the WPT-Airport Information Page. The Airport Directory databases are revised every 56 days. The Airport Directory is always available for use after the expiration date. Check fly.garmin.com for the current database. SATELLITE TELEPHONE AND DATA LINK SERVICES Appendix Registering with Garmin Flight Data Services Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 101 Index A subscriber account must be established prior to using the Iridium Satellite System. Before setting up an Iridium account, obtain the serial number of the Iridium Transceiver (GSR1) and the System ID by selecting the Aux- SYSTEM STATUS Page. Contact Garmin at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135. 190-02042-00 Rev. B Annun/Alerts Operation of these features in the cockpit is accomplished through the AuxTelephone, Aux-Text Messaging, and Aux-Maintenance WI-FI Setup Pages. For operation using the cabin handset, consult the instructions provided with the handset. Additional Features NOTE: Separate accounts must be established to access the Iridium satellite network for voice/SMS and low speed data transmission, and high speed data transmission for the maintenance reports. Activating Connext Weather Registration After a subscriber account has been established, the system must be activated for data link features such as reporting services or Connext Weather. Activation is accomplished by entering the required access code. This process is only performed when initially setting up the system for Connext services. 1) Ensure the aircraft is outside with a clear view of the sky. 2) Turn the large FMS Knob to select the MAP Page group. 3) Turn the small FMS Knob to select the MAP-WEATHER DATA LINK (CNXT) Page. 4) Press the MENU Key. If necessary, select ‘Display Connext Weather’. 5) Turn the large FMS Knob to hightlight ‘Register With Connext’. 6) Press the ENT Key. The ‘CONNEXT REGISTRATION’ Window is now displayed. 7) Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field. 8) Press the ENT Key. REGISTER will now be highlighted. 9) Press the ENT Key. System registration is complete when ‘REGISTERED’ is displayed in the STATUS field. AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features Iridium telephone and data communications may be turned on or off by performing these simple steps. Disabling/enabling telephone and low speed data services 1) Turn the large FMS Knob on the MFD to select the Aux page group. 2) Turn the small FMS Knob to select the Aux-Telephone Page. 3) Press the MENU Key. The Page Menu window is now displayed. 4) Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list. 5) Press the ENT Key. The Iridium transceiver is now disabled. 6) To enable the Iridium transceiver, repeat steps 1 through 3, then select ‘Enable Iridium Transceiver’. Index Appendix Annun/Alerts Additional Features Disable/Enable Iridium Transceiver 102 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Turn the large FMS Knob on the MFD to select the Aux page group. 2) Turn the small FMS Knob to select the Aux - Telephone or Aux - Text Messaging Page. 3) If necessary, press the TEL Softkey to display the Aux-Telephone Page. External Phone Hazard Avoidance Internal Phone Flight Management 1) Nav/Com/ XPDR/Audio Viewing the Telephone Page EIS The pilot or copilot can place and answer calls on the Iridium satellite network as well as to or from the telephone handset in the cabin. Calls can also be answered or made from the optional cabin phone, however, only actions initiated from the cockpit will be discussed here. See the cabin handset user guide for more information. Control and monitoring of telephone functions are accomplished through the Aux-Telephone Page. Flight Instruments TELEPHONE COMMUNICATION Description Phone is Idle AFCS Phone is ringing Additional Features Phone has a dial tone (off hook) or connected to another phone Annun/Alerts Phone dialed is busy Appendix Phone is dialing another phone Phone has failed Index Phone status not known 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 103 Flight Instruments Additional Features EIS Phone is disabled Nav/Com/ XPDR/Audio Phone is reserved for data transmission Flight Management Calling other phone or incoming call from other phone Other phone is on hold AFCS Hazard Avoidance Phones are connected CONTACTS The names, telephone number, and email addresses can be saved in a list of contacts for easy use when making telephone calls. 1) With the Aux - Telephone Page displayed, press the FMS Knob to display the cursor. 2) If necessary, turn either FMS Knob to place the cursor on ‘New Entry’. 3) Press the ENT Key. The cursor moves the ‘Name’ field of the ‘Contact Details’ window. 4) Enter the desired name of the new contact. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD. 5) Press the ENT Key. The cursor moves to the ‘Phone Number’ field. 6) Enter the desired telephone number. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD. 7) Press the ENT Key. The cursor moves to the ‘Email’ field. Index Appendix Annun/Alerts Additional Features Entering a new contact 104 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Enter the desired email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD. 9) Press the ENT Key. The Save button is highlighted. Flight Instruments 8) EIS 10) Press the ENT Key. The new contact entry is added to the list of saved contacts. Deleting a contact 2) Turn either FMS Knob to place the cursor on the desired contact name. 3) Press the Delete Softkey. A confirmation window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to delete the selected contact. Flight Management With the Aux - Telephone Page displayed, press the FMS Knob to display the cursor. Nav/Com/ XPDR/Audio 1) Editing a contact Hazard Avoidance 2) Turn either FMS Knob to place the cursor on the desired contact name. 3) Press the Edit Softkey. The cursor is placed in the ‘Name’ field. Enter the desired changes. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD. 4) Press the ENT Key when each field is complete. The Save Button is now highlighted. 5) Press the ENT Key to save the changes. Additional Features With the Aux - Telephone Page displayed, press the FMS Knob to display the cursor. 105 Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Appendix When viewing MFD pages other than the Aux-Telephone Page, a pop-up alert will be displayed and an aural alert “Incoming Call” will be heard. If the call is from the cabin, Cabin will be displayed. If the incoming call is an Iridium network call, Iridium will be displayed. The pop-up alert may be inhibited at times, such as during takeoff. In addition to the pop-up alert, a ringing phone symbol will be displayed to the right of the MFD page title. Also, the voice alert “Incoming Call” will be heard on the selected cockpit audio. Annun/Alerts INCOMING CALLS 190-02042-00 Rev. B AFCS 1) Flight Instruments Additional Features Answer an Incoming Call in the Cockpit 1) Press the TEL Key on the appropriate audio panel. 2) Press the Answer Softkey on the MFD. EIS Or: Additional Features Press the TEL Key on the appropriate audio panel. 2) Press the MENU Key to display the Page Menu. 3) Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’. 4) Press the ENT Key. Muting Incoming Call Alerts 1) With the Aux-Telephone Page displayed, press the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’. 3) Press the ENT Key. The voice and pop-up alert will not be displayed now when an incoming call is received. OUTGOING CALLS Voice calls can be made from the cockpit to the handset in the cabin, or to an external phone through the Iridium Satellite Network. Making a Call to the Cabin Appendix Annun/Alerts 1) Selecting the IGNORE Softkey will extinguish the pop-up window and leave the call unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page allowing additional call information to be viewed before answering. AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio While viewing the Aux-Telephone Page 1) Press the TEL Key on the appropriate audio panel. 2) Press the DIAL Softkey on the MFD. 3) Press the ENT Key. The cursor will move from ‘Cabin’ to ‘OK’. 4) Press the ENT Key again. The cabin phone will now ring. Index To exit the call, select the Hangup Softkey. 106 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Flight Instruments Make an External Call from the Cockpit Press the Dial Softkey on the MFD. 3) Turn the small FMS Knob to select ‘Iridium’. 4) Press the ENT Key. The cursor has now moved to the phone number entry field. 5) Enter the desired telephone number (country code first) by selecting the number softkeys on the MFD or by pressing the numeric keys on the MFD Control Unit. 6) Press the ENT Key. ‘OK’ is highlighted. 7) Press the ENT Key. The system will begin calling the number. Flight Management 2) Nav/Com/ XPDR/Audio Press the TEL Key on the appropriate audio panel. EIS 1) To exit the call, press the HANGUP Softkey. Hazard Avoidance Making an external call from the cockpit by using the Contact List Press the TEL Key on the appropriate audio panel. 2) Press the FMS Knob to activate the cursor. 3) Turn the small FMS Knob to select the desired contact name in the list of contacts. 4) Press the Call Softkey. The external call is initiated and the number associated with the contact name is dialed. AFCS 1) Additional Features Placing The Cockpit Phone on Hold Press the Hold Softkey on the MFD. Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’. 3) Press the ENT Key. Appendix 1) Annun/Alerts Or: Select the Hold Softkey again to resume the call. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 107 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features Transferring a Call from the Cockpit From the cockpit phone, a external call can be transferred to the cabin phone, or a call with the cabin phone can be transferred to an external phone. 1) Press the Trans Softkey on the MFD. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’. 2) Press the ENT Key. The cursor now highlights the phone number entry field. 3) Enter the phone number to which the call is being transferred, as discussed earlier for making an external call on the Iridium satellite network. 4) Press the ENT Key. ‘OK’ is now highlighted. 5) Press the ENT Key again to place the call. Making a Conference Call from the Cockpit 1) Press the CONF Softkey on the MFD. Or: AFCS a) Press the MENU Key to display the Page Menu. Annun/Alerts Additional Features b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’. 2) Press the ENT Key. The cursor now highlights the phone number entry field. 3) Enter the phone number as discussed earlier for making an external call on the Iridium satellite network. 4) Press the ENT Key. ‘OK’ is now highlighted. 5) Press the ENT Key again to place the call. Index Appendix TEXT MESSAGING (SMS) The pilot or copilot can send and receive text messages on the Iridium satellite network. Messages may be sent to an email address or text message capable cellular telephone. Message length is limited to 160 characters, including the email address. The text messaging user interface is mainly through the Aux-Text Messaging Page. 108 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Turn the large FMS Knob on the MFD to select the Aux page group. 2) Turn the small FMS Knob to select the Aux-Telephone or Aux-Text Messaging Page. 3) If necessary, press the SMS Softkey to display the Aux-Text Messaging Page. Nav/Com/ XPDR/Audio Message Symbol EIS 1) Flight Instruments Viewing the Text Messaging Page Description Received text message that has not been opened Flight Management Received text message that has been opened Saved text message, draft not sent Hazard Avoidance System is sending text message Text message has been sent AFCS System failed to send text message Additional Features Predefined text message Viewing a Text Message When Received Annun/Alerts Appendix When viewing MFD pages other than the Aux-Text Messaging Page, a pop-up alert will be displayed when a new text message is received. Select the View Softkey to view the message. Selecting the Ignore Softkey will extinguish the pop-up window and leave the text message unopened. Selecting the Ignore All Softkey will extinguish the pop-window and ignore all future incoming text messages. Selecting the SMS Softkey will display the Aux-Text Messaging Page. The pop-up alerts may be enabled or disabled through the Page Menu. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 109 Additional Features 1) With the Aux-Text Messaging Page displayed, press the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disable New Message Popups’ or ‘Enable New Message Popups’. 3) Press the ENT Key. The pop-up alert will not be displayed when an incoming text message is received. Replying to a Text Message While viewing the text message, press the Reply Softkey. Or: Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Enabling/Disabling Incoming Text Message Pop-Up Alerts 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Reply To Message’. 3) Press the ENT Key. Sending a Text Message 1) While viewing the Aux-Text Messaging Page, press the NEW Softkey. AFCS Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Draft New Message’. 2) The SMS Text Message Draft Window is now displayed with the cursor in the ‘TO’ field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to create upper and lower case alpha characters. Special characters can be accessed by pressing the Symbols Softkey. 3) Press the ENT Key. The cursor is now displayed in the ‘Message’ field. 4) Enter the desired message using any combination of entry methods as described in step 2. 5) Press the ENT Key. Index Appendix Annun/Alerts Additional Features c) Press the ENT Key. 110 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Press the Send Softkey to send the message immediately, or press the Save Softkey to save the message in Outbox for sending at a later time. Press the Cancel Softkey to delete the message. Flight Instruments 6) Sending a new text message/email to a saved contact With the Aux - Telephone Page displayed, press the FMS Knob to display the cursor. 2) Turn either FMS Knob to place the cursor on the desired contact name. 3) Press either the Text Email Softkey to send to the email address saved for the contact or Text Phone Softkey to send to the phone number saved for the contact. The cursor is placed in the ‘To’ field. Confirm the contact you wish to send a message to by pressing the ENT Key. 4) Enter the desired message, then press the ENT Key. 5) Confirm you wish to send the message by pressing the ENT Key with ‘Yes’ highlighted. Select ‘No’ to return to the message entry field and either press the Cancel Softkey to delete the message or press the Save Softkey to save the message as a draft. EIS 1) Nav/Com/ XPDR/Audio Flight Management Hazard Avoidance Predefined Text Messages While viewing the Aux-Text Messaging Page, press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to select ‘Edit Predefined Messages’. 3) Press the ENT Key. The Predefined Messages view is now displayed. 4) Press the NEW Softkey. Annun/Alerts 1) Additional Features Creating a Predefined Text Message AFCS Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message. Or: Appendix a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined Message’. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index c) Press the ENT Key. The Predefined SMS Text Message Window is now displayed. 111 5) The cursor is displayed in the ‘Title’ field. Enter the desired message title. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to create upper and lower case alpha characters. Special characters can be accessed by pressing the Symbols Softkey. 6) Press the ENT Key. The cursor is now displayed in the ‘Message’ field. 7) Enter the desired message using any combination of entry methods as described in step 5. 8) Press the ENT Key. 9) Press the Save Softkey. The new predefined message is now shown in the displayed list. Pressing the Cancel Softkey will delete the message without saving. Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features Hazard Avoidance 10) Press the MENU Key to display the Page Menu. 11) Turn either FMS Knob to place the cursor on ‘Cancel Drafting Message’. Sending a Predefined Text Message 1) While viewing the Aux-Text Messaging Page, press the NEW Softkey. 2) The Predefined SMS Text Message Window is now displayed with the cursor in the ‘TO’ field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by pressing the Numbers Softkey. Press the CapsLock Softkey to create upper and lower case alpha characters. Special characters can be accessed by pressing the Symbols Softkey. 3) Press the ENT Key. The cursor is now displayed in the ‘Message’ field. 4) Press the PREDEFD Softkey. The Predefined Message Menu Window is displayed. 5) Turn either FMS Knob to select the desired predefined message. Index Appendix Annun/Alerts Additional Features AFCS 12) Press the ENT Key. 112 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features 7) Press the ENT Key. 8) Press the Send Softkey to transmit the message. EIS Press the ENT Key. The predefined message text is inserted into the message field. If desired, the message can be edited by using the FMS Knobs. Flight Instruments 6) Text Message Boxes Flight Management Showing Inbox Messages While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Inbox Softkey. 2) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. AFCS Press the MENU Key to display the Page Menu. Hazard Avoidance Or: 1) Nav/Com/ XPDR/Audio Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to be sent later are stored as Drafts. Each text message box may be viewed separately, or together in any combination. Showing Outbox Messages Additional Features While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Outbox Softkey. Or: 2) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Appendix Press the MENU Key to display the Page Menu. Annun/Alerts 1) Showing Draft Messages Index While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Drafts Softkey. Or: 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 113 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Managing Text Messages The viewed messages may be listed according to the date/time the message was sent or received, the type of message (read, unread, sent, unsent, etc.), or by message address. Viewing Messages Sorted by Message Date/Time While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Time Softkey. Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features Or: b) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’. c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. Viewing Messages Sorted by Message Type While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Type Softkey. Additional Features AFCS Hazard Avoidance a) Press the MENU Key to display the Page Menu. Annun/Alerts Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Sort By Type’. 3) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. Appendix Viewing Messages Sorted by Address While viewing the Aux-Text Messaging Page, press the Arrange Softkey, then press the Address Softkey. Index Or: 114 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Sort By Address’. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. Viewing The Content of a Text Message 2) Press the FMS Knob to activate the cursor. 3) Turn either FMS Knob to select the desired message. 4) Press the VIEW Softkey. Nav/Com/ XPDR/Audio While viewing the Aux-Text Messaging Page, select the desired message box. EIS 1) Flight Instruments 3) Or: Flight Management Press the ENT Key. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘View Selected Message’. Hazard Avoidance c) Press the ENT Key. Message content is displayed. 5) To close the text message, press the Close Softkey. AFCS Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Close Message’. Additional Features c) Press the ENT Key. Marking Selected Message As Read While viewing the Inbox on the Aux-Text Messaging Page, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired message. 3) Press the MRK Read Softkey. Appendix Or: a) Press the MENU Key to display the Page Menu. c) Press the ENT Key. The message symbol now indicates the message has been opened. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 115 Index b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message As Read’. 190-02042-00 Rev. B Annun/Alerts 1) Mark All Messages As Read 1) While viewing the Inbox on the Aux-Text Messaging Page, press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Mark All New Messages As Read’. 3) Press the ENT Key. A confirmation window is displayed. 4) With cursor highlighting ‘YES’, press the ENT Key. The message symbols now indicate all the message have been opened. Deleting a Message 1) While viewing the Inbox on the Aux-Text Messaging Page, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired message. 3) Press the Delete Softkey. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’. AFCS c) Press the ENT Key. The system is capable of WEP64, WEP128,WPA-PSK, and WPA2-PSK encryption formats. WPA-Enterprise and WPA2-Enterprise are not supported. Connections that require web proxies, captive portals, or other elements that require user credentials, including a username and password or a redemption or access code; or require action such as accepting a user agreement, are not supported. Control and monitoring of Wi-Fi functions are accomplished through the AuxMaintenance WiFi Setup Page. Viewing the Wi-Fi Setup Page 1) Turn the large FMS Knob on the MFD to select the Aux page group. 2) Turn the small FMS Knob to select the Aux-Maintenance WiFi Setup Page. Index Appendix Annun/Alerts Additional Features WI-FI CONNECTIONS 116 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Press the Avail Softkey on the MFD. A list of available networks will be displayed in the Available Networks window. Signal strength is shown for each network, as well as security requirements and whether the network has been saved in the system’s memory. 2) If necessary, press the Rescan Softkey to have the system scan again for available networks. Nav/Com/ XPDR/Audio Or: a) Press the MENU Key to display the Page Menu. Flight Management b) Turn either FMS Knob to place the cursor on ‘Rescan Available Networks’. c) Press the ENT Key. Press the FMS Knob to place the cursor in the list of networks. 4) Turn either FMS Knob to select the desired network. 5) Press the Connect Softkey. Hazard Avoidance 3) EIS 1) Flight Instruments Setting Up a New Wi-Fi Connection Or: a) Press the MENU Key to display the Page Menu. AFCS b) Turn either FMS Knob to place the cursor on ‘Connect to Selected Network’. c) Press the ENT Key. Press the ENT Key. ‘OK’ will be highlighted. 8) Press the ENT Key again. 9) The Save Settings window is now displayed with the cursor highlighting ‘Save Connection’. Appendix 7) Annun/Alerts If the network is secured, a window will be displayed in order to enter the necessary passcode. Use the FMS Knobs to enter the desired alpha numeric characters. Press the CapsLock Softkey to enter upper case letters. If there is no security associated with the network, proceed to step 9. Additional Features 6) 10) The selected network can be saved to system memory to make reconnection easier at a later time. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 117 Additional Features Flight Instruments Connecting the selected network without saving: a) Turn the large FMS Knob to move the cursor to highlight ‘Connect’. b) Press the ENT Key. Saving and connect the selected network: EIS a) Press the ENT Key. A checkmark is placed in the checkbox and the cursor moves to the airport field. c) Press the ENT Key. The cursor moves to ‘Connect’. d) Press the ENT Key again to connect to the selected network. Editing a Saved Network 1) While viewing list of saved networks, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to highlight the network to be edited. 3) Pressing the ENT Key at this point will check or uncheck the Auto Connect checkbox. When a checkmark is present, the system will automatically connect to the network when within range. 4) Press the Edit Softkey. The cursor now appears in the Connection Settings window. 5) Turn the large FMS Knob to select the network attribute to be edited. 6) Turn the small FMS Knob to begin editing the field. 7) When the entry is complete, press the ENT Key. 8) Turn the large FMS Knob or press the ENT Key until ‘Save’ is highlighted. 9) Press the ENT Key. Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio b) Using the FMS Knobs, enter an airport identifier to be associated with the saved network. This aids in identifying the network later in the event of duplicate network names. Appendix Disconnecting a Wi-Fi Network Press the DISCNCT Softkey. Or: a) Press the MENU Key to display the Page Menu. Index b) Turn either FMS Knob to place the cursor on ‘Disconnect From Network’. c) Press the ENT Key. 118 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features While viewing the list of saved networks, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to highlight the network to be deleted. 3) Press the DELETE Softkey. The selected network is removed from the list. EIS 1) Flight Instruments Deleting a Saved Wi-Fi Network SIRIUSXM™ RADIO ENTERTAINMENT Turn the large FMS Knob to select the Auxiliary Page Group. 2) Turn the small FMS Knob to select the displayed Aux - XM Information Page. 3) Press the Radio Softkey to show the XM Radio Page where audio entertainment is controlled. Hazard Avoidance 1) ACTIVE CHANNEL AND CHANNEL LIST 2) Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey. Annun/Alerts While on the XM Radio Page, press the Channel Softkey. Additional Features Selecting a channel from the channel list Or: Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels. 2) Press the ENT Key to activate the selected channel. Appendix 1) AFCS The Active Channel Box on the XM Radio Page displays the currently selected channel. The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category. 1) Flight Management Selecting the XM Radio Page Nav/Com/ XPDR/Audio The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM™ Satellite Radio. Selecting a channel directly While on the XM Radio Page, press the Channel Softkey. 2) Press the Direct CH Softkey. The channel number in the Active Channel Box is highlighted. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index 1) 119 Flight Instruments Additional Features 3) Press the numbered softkeys located on the bottom of the display to directly select the desired channel number. 4) Press the ENT Key to activate the selected channel. Flight Management Nav/Com/ XPDR/Audio EIS Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio. 1) Press the Category Softkey on the XM Radio Page. 2) Press the CAT + and CAT - Softkeys to cycle through the categories. Or: Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob and press the ENT Key. Selecting All Categories places all channels in the list. 1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, press the Presets Softkey to access the first five preset channels (Preset 1 - Preset 5). 2) Press the More Softkey to access the next five channels (Preset 6 – Preset 10), and again to access the last five channels (Preset 11 – Preset 15). Pressing the More Softkey repeatedly cycles through the preset channels. 3) Press any one of the (Preset 1 - Preset 15) softkeys to assign a number to the active channel. 4) Press the Set Softkey on the desired channel number to save the channel as a preset. Adjusting Volume Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Setting a preset channel number 1) With the XM Radio Page displayed, press the Volume Softkey. 2) Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL Softkey is pressed, the volume can also be adjusted using the small FMS Knob.) Index SiriusXM Radio volume may also be adjusted on each passenger headset. 120 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Flight Instruments Muting SiriusXM audio 1) Select the XM Radio Page or XM Information Page. 2) Press the Mute Softkey to mute the audio. Press the Mute Softkey again to unmute the audio. EIS SCHEDULER Hazard Avoidance 1) Select the Aux - Utility Page. Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key. 5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type. 6) Turn the small FMS Knob to select the message type: • Event—Message issued at the specified date/time • One time—Message issued when the message timer reaches zero (default setting) • Periodic—Message issued each time the message timer reaches zero 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. 8) For periodic and one-time messages, use the FMS Knob to enter the timer value (HHH:MM:SS) from which to countdown and press the ENT Key. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 121 Index 4) Appendix Turn the large FMS Knob to highlight the first empty scheduler message naming field. Annun/Alerts 3) Additional Features Press the FMS Knob momentarily to activate the flashing cursor. AFCS 2) 190-02042-00 Rev. B Flight Management Entering a scheduler message Nav/Com/ XPDR/Audio The Scheduler feature can be used to enter and display reminder messages (e.g., Change oil, Switch fuel tanks, or Altimeter-Transponder Check) in the Alerts Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed. When power is cycled, all messages are retained until deleted, and message timer countdown is resumed Additional Features Flight Instruments 9) a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. EIS b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message Flight Management Nav/Com/ XPDR/Audio For event-based messages: 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted. 4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored. 5) Press the ENT Key while the message line is cleared to clear the message time. AFCS Hazard Avoidance 1) Select the Aux - Utility Page. The SurfaceWatch™ feature provides aural and visual annunciations to help the flight crew maintain situational awareness and avoid potential runway incursions and excursions during ground and air operations in the airport environment. Inhibiting/Uninhibiting SurfaceWatch Appendix Annun/Alerts Additional Features SURFACEWATCH (OPTIONAL) 1) Select the Aux - System Setup 1 Page. 2) Press the FMS Knob momentarily to activate the flashing cursor.. 3) Turn the large FMS Knob to highlight the SurfaceWatch field. 4) Turn the small FMS Knob to toggle the SurfaceWatch alerts on or off. Index Entering origin/destination airport 122 1) Select the FPL - SurfaceWatch Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Turn the large FMS Knob if necessary to highlight the Origin or Destination Airport field. 4) Use the FMS Knobs to input the desired Origin or Destination Airport. Flight Instruments 3) Selecting origin/destination runway EIS 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob if necessary to highlight the Runway or Landing Runway field. 4) Turn the small FMS Knob to select the desired available Runway or Landing Runway. As the small FMS Knob is turned, the preview of the selected runway or landing runway is also displayed. Selecting required takeoff/landing distance Select the FPL - SurfaceWatch Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob if necessary to highlight the REQD Takeoff DIS or REQD Landing DIS field. 4) Use the FMS Knobs to enter the required takeoff or landing distance. Upon pressing the FMS Knob and committing the required takeoff or landing distance, the Runway Length field will turn amber if an insufficient runway length exists. Hazard Avoidance 1) Additional Features Annun/Alerts Creating a profile 1) Select the AUX - System Setup Page. Appendix Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘Create’ in the Crew Profile Box. 4) AFCS PILOT PROFILES 2) Flight Management Select the FPL - SurfaceWatch Setup Page. Nav/Com/ XPDR/Audio 1) Press the ENT Key. A ‘Create Profile’ window is displayed. 5) Use the FMS Knob to enter a profile name up to 16 characters long and 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 123 Index press the ENT Key. Crew profile names cannot begin with a blank as the first letter. EIS Flight Instruments Additional Features 6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or other previously created profile settings. 7) Press the ENT Key. 8) With ‘Create’ highlighted, press the ENT Key to create the profile Use the large FMS Knob to select ‘Create & Activate’ and press the ENT Key to activate the new profile. 9) To cancel the process, select ‘Cancel’ with the large FMS Knob and press the ENT Key. Selecting an active profile 1) Select the AUX - System Setup Page. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio Or: 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the active profile field in the Crew Profile Box. AFCS 4) Turn the small FMS Knob to display the crew profile list and highlight the desired profile. the selected profile. Renaming a profile 1) Select the AUX - System Setup Page. Annun/Alerts Additional Features 5) Press the ENT Key. The system loads and displays the system settings for 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘Rename’ in the Crew Profile Box. Appendix 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. 6) Press the ENT Key. Index 7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key. 124 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features 9) To cancel the process, use the large FMS Knob to select ‘Cancel’ and press the ENT Key. Flight Instruments 8) With ‘Rename’ highlighted, press the ENT Key. Deleting a profile EIS 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 4) Nav/Com/ XPDR/Audio 3) Turn the large FMS Knob to highlight ‘Delete’ in the Crew Profile Box. Press the ENT Key. 5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to 6) Flight Management delete. Press the ENT Key. 7) With ‘Delete’ highlighted, press the ENT Key. To cancel the process, use the large FMS Knob to select ‘Cancel’ and press the ENT Key. Hazard Avoidance 8) Importing a profile from an SD card 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) Press the Import Softkey. Additional Features Insert an SD card containing the crew profile(s) into the top card slot on the MFD. AFCS 1) Or: a) Press the MENU Key. 5) If the imported profile name is the same as an existing profile on the system, the system displays an ‘Overwrite existing profile? OK or CANCEL’ prompt. Press the ENT Key to replace profile on the system with the profile imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Crew Profile Importing window. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 125 Index The system displays the Crew Profile Importing window with ‘Import’ highlighted. Turn the large FMS Knob to highlight the ‘Profile Name’ field, then scroll to the desired profile name with the large and small FMS Knobs, then press the ENT Key. Then press the ENT Key with ‘Import’ highlighted. Appendix 4) Annun/Alerts b) Turn the FMS Knob to highlight ‘Import Crew Profile’ and press the ENT Key. Additional Features 1) Insert the SD card for storing the Crew Profile into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) Press the Export Softkey. The system displays the Crew Profile Exporting window. Flight Management Or: a) Press the MENU Key. 4) To export the crew profile using the current selected profile, press the ENT Key with ‘Export’ highlighted. To change the selected profile, turn the large FMS Knob to highlight the ‘Profile Name’ field, then scroll to the desired profile name with the large and small FMS Knobs, then press the ENT Key. Then press the ENT Key with ‘Export’ highlighted. 5) If the selected profile to be exported is the same as an existing profile file name on the SD card, the system displays an ‘Overwrite existing profile? OK or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD card with the profile to be exported, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting window without exporting the profile. 6) If successful, the window displays ‘Crew profile export succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the FMS Knob to return to the AUX - System Setup Page. Additional Features AFCS Hazard Avoidance b) Turn the FMS Knob to highlight ‘Export Crew Profile’ and press the ENT Key. Annun/Alerts Appendix Index If successful, the system displays ‘Crew profile import succeeded.’ in the window below. With ‘OK’ highlighted, press the ENT or CLR Keys or press the FMS Knob to return to the AUX - System Setup Page. The imported profile becomes the active profile. Exporting a profile to an SD card Nav/Com/ XPDR/Audio EIS Flight Instruments 6) ELECTRONIC STABILITY & PROTECTION (ESP™) (OPTIONAL) ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo, Mmo, and/or angle of attack) beyond the normal flight parameters. Enhanced stability for each condition is provided by applying a force to the appropriate control surface to return the 126 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Additional Features Flight Instruments EIS Nav/Com/ XPDR/Audio Flight Management Hazard Avoidance AFCS aircraft to the desired flight envelope. This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep attitude, high airspeed, or when a stall is imminent. As the aircraft deviates further from the desired attitude, angle of attack, or airspeed continues to increase, the force increases (up to an established maximum) to encourage control movement in the direction necessary to return to the desired attitude and/or airspeed range. Except in the case of high airspeed, when maximum force is reached, force remains constant up to the maximum engagement limit. Above the maximum engagement limit, forces are no longer applied. There is no maximum engagement related to a high airspeed condition. When ESP has been engaged for more than ten seconds (cumulative; not necessarily consecutive seconds) of a 20-second interval, the autopilot is automatically engaged with the flight director in Level Mode in the pitch and/or roll axis, bringing the aircraft into level flight. An aural “Engaging Autopilot” alert is played and the flight director mode annunciation will indicate ‘LVL’ for vertical and lateral modes. The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering (CWS) or Autopilot Disconnect (AP/YD DISC TRIM INTRPT) switch. Upon releasing the CWS or AP/YD DISC TRIM INTRPT switch, ESP force will again be applied, provided aircraft attitude, angle of attack and/or airspeed are within their respective engagement limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit. ESP can be enabled or disabled on the Aux-System Setup 2 Page on the MFD. Enabling or disabling ESP Turn the small FMS Knob to select the System Setup Page. 3) If necessary, press the SETUP 2 Softkey to display the Aux-System Setup 2 Page. If the Aux-System Setup 2 is already displayed, proceed to step 4. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to place the cursor in the Stability & Protection field. 6) Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’. 7) Press the FMS Knob to remove the cursor. Appendix 2) Annun/Alerts Turn the large FMS Knob to select the Aux Page Group. Additional Features 1) Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 127 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Additional Features ROLL ENGAGEMENT Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the on-side Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases to within the desirable roll attitude range. Once engaged, ESP force will be applied between 30° and 75°. The force increases as roll attitude increases and decreases as roll attitude decreases. The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude. As roll attitude decreases, ESP will disengage at 30°. ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75°. PITCH ENGAGEMENT ESP engages at 20° nose-up and 17° nose-down. Once ESP is engaged, it will apply opposing force between 15° and 50° nose-up and between 12° and 50° nose-down. Maximum opposing force is applied between 25° and 50° nose-up and between 22° and 50° nose-down. The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel. This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft. There are no indications marking the pitch ESP engage and disengage limits in these nose-up/nose-down conditions. ANGLE OF ATTACK PROTECTION When a compatible lift computer is installed, angle of attack protection is provided as part of the ESP feature. ESP force may be applied if the lift computer determines a stall warning condition is imminent. In this condition, the Pitch Limit Indicator will be initially displayed 4° below this computed pitch attitude. When pitch attitude equals that indicated by the Pitch Limit Indicator, ESP will engage, applying a force in the direction necessary to lower the nose of the aircraft. HIGH AIRSPEED PROTECTION Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of the aircraft. When the high airspeed condition is remedied, ESP force is no longer applied. 128 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Flight Instruments ANNUNCIATIONS & ALERTS WARNING ANNUNCIATION Alerts Window Text Aural Alert None None EIS Annunciation Window Text UNDERSPEED PROTECT ACTIVE Nav/Com/ XPDR/Audio ADVISORY ANNUNCIATIONS Alerts Window Text Avionics cooling fan #1 is inoperative. AVN FAN 2 FAIL Avionics cooling fan #2 is inoperative. MFD cooling fan is inoperative. PFD 1 FAN FAIL PFD #1 cooling fan is inoperative. PFD 2 FAN FAIL PFD #2 cooling fan is inoperative. Hazard Avoidance MFD FAN FAIL Flight Management Annunciation Window Text AVN FAN 1 FAIL AFCS MESSAGE ADVISORY ALERTS Alerts Window Message Additional Features TAWS GEAR FAULT – Landing Gear detected in the DOWN position. TAWS FLAP FAULT – Flaps detected in the LDG position. WOW FAULT – Miscompare between weight on wheels inputs. Annun/Alerts WOW INVALID – Weight on wheels inputs invalid. ESP OFF – ESP selected off. ESP FAIL – ESP is inoperative. ESP DEGRADE – ESP AOA mode is inoperative*. Appendix ESP DEGRADE – ESP IAS mode is inoperative. ESP CONFIG – ESP config error. Config service req’d. YD OFF – AP engaged without Yaw Damper *only available when compatible lift computer is installed. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 129 COMPARATOR ANNUNCIATIONS Comparator Comparator Condition Annunciation Type MISCOMPARE Difference in altitude sensors is > 200 ft. ALT If both airspeed sensors detect < 35 knots, this is inhibited. EIS Flight Instruments Annunciations & Alerts IAS If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 knots. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 knots. AFCS Additional Features Annun/Alerts Appendix Index MISCOMPARE HDG PIT ROL VDI MISCOMPARE Difference in heading sensors is > 6 degrees. MISCOMPARE Difference in pitch sensors is > 5 degrees. MISCOMPARE Difference in roll sensors is > 6 degrees. MISCOMPARE Difference in temp compensated altitudes is > 50 ft. ALT NO COMP No data from one or both altitude sensors. IAS HDG PIT ROL VDI NO COMP No data from one or both airspeed sensors. NO COMP No data from one or both heading sensors. NO COMP No data from one or both pitch sensors. NO COMP No data from one or both roll sensors. NO COMP No temp compensated altitude data available. REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Window Text BOTH ON ADC1 BOTH ON ADC2 BOTH ON AHRS1 BOTH ON AHRS2 BOTH ON GPS1 BOTH ON GPS2 USING ADC1 USING ADC2 USING AHRS1 130 Condition Both PFDs are displaying data from the #1 Air Data Computer. Both PFDs are displaying data from the #2 Air Data Computer. Both PFDs are displaying data from the #1 AHRS. Both PFDs are displaying data from the #2 AHRS. Both PFDs are displaying data from the #1 GPS receiver. Both PFDs are displaying data from the #2 GPS receiver. PFD2 is displaying data from the #1 Air Data Computer. PFD1 is displaying data from the #2 Air Data Computer. PFD2 is displaying data from the #1 AHRS. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Flight Instruments Condition PFD1 is displaying data from the #2 AHRS. PFD2 is displaying data from the #1 GPS. PFD1 is displaying data from the #2 GPS. EIS Reversionary Sensor Window Text USING AHRS2 USING GPS1 USING GPS2 AFCS ALERTS Annunciation Nav/Com/ XPDR/Audio Condition Description Roll Failure Roll axis control failure. AP is inoperative. MET Switch Stuck, or Pitch Trim Axis Control Failure If annunciated when AP is engaged, take control of the aircraft and disengage the autopilot. If annunciated when AP is not engaged, move each half of the MET switch separately to check if a stuck switch is causing the annunciation. YD control failure. System Failure AP and MET are unavailable. FD may still be available. Elevator Mistrim Up A condition has developed causing the pitch servo to provide a sustained force. Be prepared to apply nose up control wheel force upon autopilot disconnect. Elevator Mistrim Down A condition has developed causing the pitch servo to provide a sustained force. Be prepared to apply nose down control wheel force upon autopilot disconnect. Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. Rudder Mistrim Left A condition has developed causing the yaw servo to provide a sustained force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. Appendix Index 131 Annun/Alerts Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Additional Features 190-02042-00 Rev. B AFCS Yaw Damper Failure Hazard Avoidance Pitch axis control failure. AP is inoperative. Flight Management Pitch Failure EIS Flight Instruments Annunciations & Alerts Condition Annunciation Description Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. Preflight Test Performing preflight system test. Upon completion of the test, the aural alert will be heard. TAWS ALERTS Alert Type AFCS PFD/MFD TAWS Page Annunciation Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) or TERRAIN AHEADPULL-UP TERRAIN AHEADPULL-UP or TERRAIN-PULL-UP Reduced Required Obstacle Clearance Warning (ROC) OBSTACLE-PULL-UP PULL UP Annun/Alerts Additional Features PULL UP or OBSTACLE AHEADPULL-UP Voice Message “Terrain, Terrain; Pull Up, Pull Up” † or “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” or “Terrain, Terrain; Pull Up, Pull Up” † “Obstacle, Obstacle; Pull Up, Pull Up” † or “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” * TAWS-A Only † Default Selection ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled Index Appendix MFD Map Page Pop-Up Alert TERRAIN-PULL-UP PULL UP Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio Preflight system test has failed. 132 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Imminent Obstacle Impact Warning (IOI) or or “Obstacle, Obstacle; Pull Up, Pull Up” † PULL-UP PULL UP PULL-UP [Whoop, Whoop]“Pull Up” Reduced Required Terrain Clearance Caution (RTC) TERRAIN TERRAIN AHEAD TERRAIN AHEAD or CAUTION-TERRAIN Annun/Alerts * TAWS-A Only † Default Selection ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled Additional Features “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain” † AFCS Imminent Terrain Impact Caution (ITI) or “Caution, Terrain; Caution, Terrain” † or “Terrain Ahead; Terrain Ahead” Hazard Avoidance TERRAIN CAUTION-TERRAIN Flight Management PULL UP “Pull Up” or “ [Whoop, Whoop]“Pull Up” Nav/Com/ XPDR/Audio OBSTACLE-PULLUP EIS *Excessive Closure Rate Warning (ECR) Voice Message OBSTACLE AHEAD- “Obstacle Ahead, Pull Up; PULL-UP Obstacle Ahead, Pull Up” PULL UP Excessive Descent Rate Warning (EDR) MFD Map Page Pop-Up Alert Flight Instruments PFD/MFD TAWS Page Annunciation Alert Type Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 133 Flight Instruments Annunciations & Alerts Alert Type PFD/MFD TAWS Page Annunciation TERRAIN Imminent Obstacle Impact Caution (IOI) TERRAIN Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Reduced Required Obstacle Clearance Caution (ROC) MFD Map Page Pop-Up Alert Voice Message CAUTION-OBSTACLE “Caution, Obstacle; Caution, Obstacle” † or or OBSTACLE AHEAD “Obstacle Ahead; Obstacle Ahead” OBSTACLE AHEAD “Obstacle Ahead; Obstacle Ahead” or or CAUTION-OBSTACLE “Caution, Obstacle; Caution, Obstacle” † Premature Descent Alert Caution (PDA) TERRAIN TOO LOW-TERRAIN “Too Low, Terrain” Excessive Descent Rate Caution (EDR) TERRAIN SINK RATE “Sink Rate” *Excessive Closure Rate Caution (ECR) TERRAIN TERRAIN “Terrain, Terrain” DON’T SINK “Don’t Sink” † or or TOO LOW-TERRAIN “Too Low, Terrain” Negative Climb Rate Caution (NCR) TERRAIN *Flight Into Terrain High Speed Caution (FIT) TERRAIN TOO LOW-TERRAIN “Too Low, Terrain” *Flight Into Terrain Gear Caution (FIT) TERRAIN TOO LOW-GEAR “Too Low, Gear” *Flight Into Terrain Flaps Caution (FIT) TERRAIN TOO LOW-FLAPS “Too Low, Flaps” *Flight Into Terrain Takeoff Caution (FIT) TERRAIN TOO LOW-TERRAIN “Too Low, Terrain” * TAWS-A Only † Default Selection ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled 134 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Voice Message GLIDESLOPE GLIDESLOPE “Glide Slope” or or or GLIDEPATH GLIDEPATH “Glide Path” None “Five-Hundred” or *“Four-Hundred” or *“Three-Hundred” or *“Two-Hundred” or *“One-Hundred” None Hazard Avoidance TAWS System Status Annunciations TAWS System Test Fail; Terrain, m or Obstacle database unavailable or invalid on all GDUs; software mismatch among GDUs; TAWS audio fault Voice Message TAWS TEST TAWS TEST None None None “TAWS System Test OK” TAWS FAIL TAWS FAIL “TAWS System Failure” Annun/Alerts System Test pass TAWS Page Center Banner Annunciation Additional Features System Test in progress PFD/MFD‡ Alert Annunciation † AFCS Alert Type Flight Management * TAWS-A Only † Default Selection ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled Nav/Com/ XPDR/Audio Altitude Voice Callout (VCO) (all except “Five-Hundred” are configurable) MFD Map Page Pop-Up Alert EIS *Glide Slope Deviation Caution (GSD) (depends on approach type) PFD/MFD TAWS Page Annunciation Flight Instruments Alert Type Appendix * TAWS-A Only † VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available. ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 135 Annunciations & Alerts TAWS Page Center Banner Annunciation Voice Message None TERRAIN DATABASE FAILURE None TAWS N/A NO GPS POSITION “TAWS Not Available” TAWS N/A None “TAWS Not Available” None None “TAWS Available” (aural message only in flight) TAWS Alerting is disabled TAWS INH None None *Radar Altimeter invalid, Vertical Speed Invalid, GPS and Baro Altitude invalid, Software mismatch among GDUs, TAWS configuration mismatch among GDUs, TAWS audio fault GPWS FAIL None “GPWS System Failure” *GPWS Alerting is disabled GPWS INH None None *Flap Override is enabled FLAP OVR None None None None Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments PFD/MFD‡ Alert Annunciation Alert Type MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases No GPS position Excessively degraded GPS signal, or out of database coverage area Sufficient GPS signal reception restored *Glideslope/Glidepath Alerting is disabled † GS INH or GP INH * TAWS-A Only † VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available. ‡ Annunciation is shown on the TAWS Page and the Navigation Map Page when Terrain is enabled. 136 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts SurfaceWatch Alert Annunciation Associated Voice Alert Description Issued when the aircraft is taking off from a nonrunway (e.g. a taxiway) EIS “Taxiway” Flight Instruments SURFACEWATCH ALERTS Issued when the aircraft is taking off from, or landing on, a runway different than that entered by the crew. “Taxiway” Issued when the aircraft is landing on a nonrunway (e.g. a taxiway). Flight Management “Check runway” Nav/Com/ XPDR/Audio Issued when the aircraft is taking off from, or “Runway too landing on, a runway with a length less than short” needed as entered by the crew. GDL 69/69A SXM DATA LINK RECEIVER MESSAGES CHECK ANTENNA XM Information Page (MFD) Data Link Receiver antenna error; service required UPDATING XM Information Page (MFD)) Data Link Receiver updating encryption code NO SIGNAL XM Information Page Weather Datalink Page (MFD) Loss of signal; signal strength too low for receiver LOADING XM Radio Page (MFD) Acquiring channel audio or information OFF AIR XM Radio Page (MFD) Channel not in service -------WEATHER DATA LINK FAILED ACTIVATION REQUIRED DETECTING ACTIVATION XM Radio Page (MFD) Missing channel information XM Information Page (MFD) SiriusXM subscription is not activated Weather Datalink Page (MFD) SiriusXM subscription is activating. Weather Datalink Page (MFD) SiriusXM subscription confirmed downloading weather data. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index No communication from Data Link Receiver within last 5 minutes Appendix Weather Datalink Page (MFD) Annun/Alerts 190-02042-00 Rev. B Additional Features WAITING FOR DATA... Description AFCS Message Location Hazard Avoidance Message 137 FLIGHT PLAN IMPORT/EXPORT MESSAGES Flight Plan Import/Export Results A flight plan file stored on the SD card was successfully imported as a stored flight plan. ‘File contained user waypoints only. User waypoints imported successfully. No stored flight plan data was modified.’ The file stored on the SD card did not contain a flight plan, only user waypoints. These waypoints have been saved to the system user waypoints. No flight plans stored in the system have been modified. ‘No flight plan files found to import.’ The SD card contains no flight plan data. ‘Flight plan import failed.’ Flight plan data was not successfully imported from the SD card. ‘Flight plan partially imported.’ Some flight plan waypoints were successfully imported from the SD card, however others had errors and were not imported. A partial stored flight plan now exists in the system. ‘File contained user waypoints only.’ The file stored on the SD card did not contain a flight plan, only user waypoints. One or more of these waypoints did not import successfully. ‘Too many points. Flight plan truncated.’ The flight plan on the SD card contains more waypoints than the system can support. The flight plan was imported with as many waypoints as possible. ‘Some waypoints not loaded. Waypoints locked.’ The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database. The flight plan has been imported, but must be edited within the system before it can be activated for use. ‘User waypoint database full. Not all loaded.’ The flight plan file on the SD card contains user waypoints. The quantity of stored user waypoints has exceeded system capacity, therefore not all the user waypoints on the SD card have been imported. Any flight plan user waypoints that were not imported are locked in the flight plan. The flight plan must be edited within the system before it can be activated for use. ‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system. ‘Flight plan successfully exported.’ The stored flight plan was successfully exported to the SD card. ‘Flight plan export failed.’ The stored flight plan was not successfully exported to the SD card. The SD card may not have sufficient available memory or the card may have been removed prematurely. Additional Features Annun/Alerts Appendix Index Description ‘Flight plan successfully imported.’ AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts 138 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Pilot Profile Import/Export Results Flight Instruments PILOT PROFILE IMPORT/EXPORT MESSAGES Description ‘Overwrite existing profile?’ Displayed if the profile name matches the name of existing profile. ‘Profile name invalid. Enter a different profile name.’ Displayed if the profile name is invalid. ‘All available pilot profiles in use. Delete a profile before importing another.’ Displayed if the maximum number for pilot profiles has been reached. ‘Pilot profile import failed.’ Displayed if the importing operation fails for any other reason. ‘Pilot profile import succeeded.’ Displayed if the importing operation succeeds. ‘Overwrite existing file?’ Displayed if the filename matches the name of an existing file on the SD card. ‘Pilot profile export failed.’ Displayed if the export operation fails. ‘Pilot profile export succeeded.’ Displayed if the export operation succeeds. Nav/Com/ XPDR/Audio Displayed if the SD card does not have one or more valid pilot profile filenames. Flight Management Hazard Avoidance AFCS VOICE ALERTS Description “Minimums” The aircraft has descended below the preset minimum descent altitude or decision altitude. “Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. The aircraft is in an underspeed condition. See the AFCS section for more details. “Traffic” Played when a Traffic Advisory (TA) is issued with the TIS system, the optional GTS 820/825 TAS system, or the optional GTS 850/855 TCAS I system. See the Hazard Avoidance section for additional details on GTS 820/825/850/855 voice alerts. “TIS Not Available” The aircraft is outside the Traffic Information Service (TIS) coverage area. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 139 Index The ESP system is engaging the autopilot. See the AFCS section for more details. Appendix “Engaging autopilot” Annun/Alerts “Airspeed” Additional Features Voice Alert 190-02042-00 Rev. B EIS ‘No pilot profile plan files found to import.’ Voice Alert Description “Traffic, Traffic” Played when a Traffic Advisory (TA) is issued with the optional SKY 497/SKY899 TAS system, or the optional KTA 870 TAS system. See the Skywatch PG or KTA 870 PG for additional details on voice alerts. Played for each subsequent TA (KTA 870 only). EIS Flight Instruments Annunciations & Alerts Played when the optional traffic system passes a pilotinitiated self test. “Traffic Advisory System Test Passed” - SKY 497 TAS “SKYWATCH System Test Passed” - SKY 899 TAS “TAS System Test OK” - KTA 870 TAS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio “Traffic” “TAS System Test Passed” - GTS 820/825 TAS “TCAS System Test Passed” - GTS 850 TCAS I “TCAS One System Test Passed” - GTS 855 TCAS I “TCAS Two System Test Passed” - GTS 8000 TCAS II Annun/Alerts Additional Features AFCS Played when the optional traffic system fails a pilotinitiated self test. “Traffic Advisory System Test Failed” - SKY 497 TAS “SKYWATCH System Test Failed” - SKY 899 TAS “TAS System Test Fail” - KTA 870 TAS “TAS System Test Failed” - GTS 820/825 TAS “TCAS System Test Failed” - GTS 850 TCAS I “TCAS One System Test Failed” - GTS 855 TCAS I “TCAS Two System Test Failed” - GTS 8000 TCAS II Index Appendix “One o’clock” through “Twelve o’clock”or “No Bearing” 140 Intruder bearing (GTS 820/825/850/855 only) “High”, “Low”, “Same Altitude” (if within 200 feet of own altitude), or “Altitude not available” Intruder relative altitude (GTS 820/825/850/855 only) “Less than one mile”, “One Mile” through “Ten Miles”, or “More than ten miles” Intruder distance (GTS 820/825/850/855 only) Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Message Flight Instruments SYSTEM MESSAGE ADVISORIES Comments ABORT APR – Loss of GPS navigation. Abort approach due to loss of GPS navigation. Abort approach. ADC1 SERVICE – ADC1 needs service. Return unit for repair. The GDC1 should be serviced. ADC2 ALT EC – ADC2 altitude error correction is unavailable. GDC2 is reporting that the altitude error correction is unavailable. The system should be serviced. ADC2 AS EC – ADC2 airspeed error correction is unavailable. GDC2 is reporting that the airspeed error correction is unavailable. The system should be serviced. ADC2 SERVICE – ADC2 needs service. Return unit for repair. The GDC2 should be serviced. AHRS MAG DB – AHRS magnetic model database version mismatch. The #1 AHRS and #2 AHRS magnetic model database versions do not match. Hazard Avoidance GDC1 is reporting that the airspeed error correction is unavailable. The system should be serviced. Flight Management ADC1 AS EC – ADC1 airspeed error correction is unavailable. Nav/Com/ XPDR/Audio GDC1 is reporting that the altitude error correction is unavailable. The system should be serviced. EIS ADC1 ALT EC – ADC1 altitude error correction is unavailable. Additional Features AHRS configuration settings do not match those of AHRS1 CONFIG – AHRS1 config error. backup configuration memory. The system should be Config service req’d. serviced. The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced. AHRS1 GPS – AHRS1 not receiving backup GPS information. The #1 AHRS is not receiving backup GPS information. The system should be serviced. AHRS1 GPS – AHRS1 using backup GPS source. The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible. AHRS1 SERVICE – AHRS1 needs service. Return unit for repair. A failure has been detected in the #1 AHRS or #2 AHRS. The system should be serviced. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index AHRS1 GPS – AHRS1 not receiving any GPS information. Appendix The #1 AHRS is operating exclusively in no-GPS mode. The system should be serviced. Annun/Alerts AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. 190-02042-00 Rev. B AFCS AHRS1 CAL – AHRS1 calibration version The #1 AHRS calibration version error. The system should error. Srvc req’d. be serviced. 141 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts Message Comments AHRS1 SRVC – AHRS1 Magnetic-field model needs update. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. AHRS1 TAS – AHRS1 not receiving valid airspeed. The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The system should be serviced. AHRS2 CAL – AHRS2 calibration version The #1 AHRS calibration version error. The system should error. Srvc req’d. be serviced. AHRS configuration settings do not match those of AHRS2 CONFIG – AHRS2 config error. backup configuration memory. The system should be Config service req’d. serviced. AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode. The #1 AHRS is operating exclusively in no-GPS mode. The system should be serviced. AHRS2 GPS – AHRS2 not receiving any GPS information. The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced. AHRS2 GPS – AHRS2 not receiving backup GPS information. The #1 AHRS is not receiving backup GPS information. The system should be serviced. AHRS2 GPS – AHRS2 using backup GPS source. The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible. AHRS2 SERVICE – AHRS2 needs service. Return unit for repair. A failure has been detected in the #1 AHRS or #2 AHRS. The system should be serviced. AHRS2 SRVC – AHRS2 Magnetic-field model needs update. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. AHRS2 TAS – AHRS2 not receiving valid airspeed. The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The system should be serviced. APR ADVISORY – SBAS VNAV not available. Using Baro VNAV. SBAS VNAN not available. Check GPS sensor. APR DWNGRADE – Approach downgraded. Vertical guidance generated by SBAS is unavailable, use LNAV only minimums.. APPR INACTV – Approach is not active. The system notifies the pilot that the loaded approach is not active. Activate approach when required. 142 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts ARSPC AHEAD – Airspace ahead less than 10 minutes. Special use airspace is ahead of aircraft. The aircraft will penetrate the special use airspace within 10 minutes. ARSPC NEAR – Airspace near and ahead. Special use airspace is near and ahead of the aircraft position. ARSPC NEAR – Airspace near – less than 2 nm. Special use airspace is within 2 nm of the aircraft position. CHECK CRS – Database course for LOC1 / [LOC ID] is [CRS]°. Selected course for LOC1 differs from published localizer course by more than 10 degrees. CHECK CRS – Database course for LOC2 / [LOC ID] is [CRS]°. Selected course for LOC2 differs from published localizer course by more than 10 degrees. CNFG MODULE – PFD1 configuration module is inoperative. The PFD1 configuration module backup memory has failed. The system should be serviced. COM1 CONFIG – COM1 config error. Config service req’d. COM1 configuration settings do not match backup configuration memory. The system should be serviced. COM1 MANIFEST – COM1 software mismatch, communication halted. COM1 software mismatch. The system should be serviced. COM1 PTT – COM1 push-to-talk key is stuck. The COM1 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced. COM1 RMT XFR – COM1 remote transfer key is stuck. The COM1 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. COM1 SERVICE – COM1 needs service. Return unit for repair. The system has detected a failure in COM1. COM1 may still be usable. The system should be serviced when possible. COM1 TEMP – COM1 over temp. Reducing transmitter power. The system has detected an over temperature condition in COM1. The transmitter operates at reduced power. If the problem persists, the system should be serviced. COM2 CONFIG – COM2 config error. Config service req’d. COM2 configuration settings do not match backup configuration memory. The system should be serviced. COM2 MANIFEST – COM2 software mismatch, communication halted. COM2 software mismatch. The system should be serviced. Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Nav/Com/ XPDR/Audio 190-02042-00 Rev. B EIS Comments Flight Instruments Message 143 Message Comments COM2 PTT – COM2 push-to-talk key is stuck. The COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced. COM2 RMT XFR – COM2 remote transfer key is stuck. The COM2 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. COM2 SERVICE – COM2 needs service. Return unit for repair. The system has detected a failure in COM2. COM2 may still be usable. The system should be serviced when possible. COM2 TEMP – COM2 over temp. Reducing transmitter power. The system has detected an over temperature condition in COM2. The transmitter operates at reduced power. If the problem persists, the system should be serviced. DATA LOST – Pilot stored data was lost. Recheck settings. The pilot profile data was lost. system reverts to default pilot profile and settings. The pilot may reconfigure the MFD & PFD with preferred settings, if desired. DB CHANGE – Database changed. Verify stored airways. This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database. This alert is issued only after an navigation database update. Verify use of airways in stored flight plans and reload airways as needed. DB CHANGE – Database changed. Verify user modified procedures. This occurs when a stored flight plan contains a procedure that is no longer consistent with the navigation database. This alert is issued only after an navigation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date. DB MISMATCH – Navigation database mismatch. Xtalk is off. The PFDs and MFD have different navigation database versions or regions installed. Crossfill is off. Check the Aux-System Status Page to determine versions or regions. Also, check the Aux-System Status Page for a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts 144 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Comments DB MISMATCH – Obstacle database mismatch. The PFDs and MFD have different obstacle database versions or regions installed. Check the Aux-System Status Page to determine versions or regions. Also, check the Aux-System Status Page for a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. DB MISMATCH – Standby Navigation database mismatch. The PFDs and MFD have different standby navigation database versions or regions installed. Check the Aux-System Status Page to determine versions or regions. Also, check the Aux-System Status Page for a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. DB MISMATCH – Terrain database mismatch. The PFDs and MFD have different terrain database versions or regions installed. Check the Aux-System Status Page to determine versions or regions. Also, check the Aux-System Status Page for a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. DME CHECK RANGE – DME range disagreement. Check position sensors. A failure or disagreement has been detected in a DME receiver. Check position sensors. FAILED PATH – A data path has failed. A data path connected to the GDU or the GIA 63/W has failed. FPL TRUNC – Flight plan has been truncated. This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan. The obsolete procedure is removed from the flight plan. Update flight plan with current arrival or approach. Flight Instruments Message EIS Nav/Com/ XPDR/Audio Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 145 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts Message Comments Upon power-up, the system detects that a stored flight plan waypoint is locked. This occurs when an navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags FPL WPT LOCK – Flight plan waypoint this message. This can also occur with user waypoints in a flight plan that is deleted. is locked. Remove the waypoint from the flight plan if it no longer exists in any database, Or - update the waypoint name/identifier to reflect the new information. G/S1 FAIL – G/S1 is inoperative. A failure has been detected in glideslope receiver 1. The system should be serviced. G/S1 SERVICE – G/S1 needs service. Return unit for repair. A failure has been detected in glideslope receiver 1. The receiver may still be available. The system should be serviced when possible. G/S2 FAIL – G/S2 is inoperative. A failure has been detected in glideslope receiver 2. The system should be serviced. G/S2 SERVICE – G/S2 needs service. Return unit for repair A failure has been detected in glideslope receiver 2. The receiver may still be available. The system should be serviced when possible. GCU CNFG – GCU Config error. Config service req’d. GCU 477 configuration settings do not match those of backup configuration memory. The system should be serviced. GCU FAIL – GCU is inoperative. A failure has been detected in the GCU 477. The GCU 477 is unavailable. GCU KEYSTK – GCU [keyname] Key is stuck A key is stuck on the GCU 477 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. GCU1 MANIFEST– GCU software mismatch, communication halted. The GCU 477 has incorrect software installed. The system should be serviced. GDC1 MANIFEST – GDC1 software mismatch, communication halted. The GDC1 has incorrect software installed. The system should be serviced. GDC2 MANIFEST – GDC2 software mismatch, communication halted. The GDC2 has incorrect software installed. The system should be serviced 146 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Comments GDL59 CONFIG – GDL 59 config error. Config service req’d. GDL 59 configuration settings do not match those of backup configuration memory. The system should be serviced. GDL59 FAIL – GDL 59 has failed. A failure has been detected in the GDL 59. The receiver is unavailable. The system should be serviced. GDL59 MANIFEST – GDL59 software mismatch, communication halted. The GDL 59 has incorrect software installed. The system should be serviced. GDL59 RTR FAIL – The GDL 59 router has failed. A failure has been detected in the GDL 59 router. The system should be serviced. GDL59 SERVICE – GDL 59 needs service. Return unit for repair. A failure has been detected in the GDL 59. The system should be serviced. GDL69 CONFIG – GDL 69 config error. Config service req’d. GDL 69A/GDL 69A SXM configuration settings do not match those of backup configuration memory. The system should be serviced. GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL 69A/GDL 69A SXM. The receiver is unavailable. The system should be serviced GDL69 MANIFEST – GDL software mismatch, communication halted. The GDL 69A/GDL 69A SXM has incorrect software installed. The system should be serviced. GEA1 CONFIG – GEA1 config error. Config service req’d. The GEA1 configuration settings do not match those of backup configuration memory. The system should be serviced. GEA2 CONFIG – GEA2 config error. Config service req’d. The GEA2 configuration settings do not match those of backup configuration memory. The system should be serviced. GEA1 MANIFEST – GEA1 software mismatch, communication halted. The #1 GEA 71 has incorrect software installed. The system should be serviced. GEA2 MANIFEST – GEA2 software mismatch, communication halted. The #2 GEA 71 has incorrect software installed. The system should be serviced. AFCS Additional Features Annun/Alerts Appendix The GIA1 configuration settings do not match backup configuration memory. The system should be serviced. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index GIA1 CONFIG – GIA1 config error. Config service req’d. 190-02042-00 Rev. B Hazard Avoidance The GIA1 has an error in the audio configuration. The system should be serviced. Flight Management The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged as invalid. GIA1 CONFIG – GIA1 audio config error. Config service req’d. Nav/Com/ XPDR/Audio GEO LIMITS – AHRS2 too far North/ South, no magnetic compass. EIS GEO LIMITS – AHRS1 too far North/ South, no magnetic compass. Flight Instruments Message 147 Comments GIA1 COOLING – GIA1 over temperature. The GIA1 temperature is too high. If problem persists, the system should be serviced. GIA1 COOLING – GIA1 temperature too low. The GIA1 temperature is too low to operate correctly. Allow units to warm up to operating temperature. GIA1 MANIFEST – GIA1 software mismatch, communication halted. The GIA1 has incorrect software installed. The system should be serviced. GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 self-test has detected a problem in the unit. The system should be serviced. GIA2 CONFIG – GIA2 audio config error. Config service req’d. The GIA2 an error in the audio configuration. The system should be serviced. Flight Management GIA2 CONFIG – GIA2 config error. Config service req’d. The GIA2 configuration settings do not match backup configuration memory. The system should be serviced. GIA2 COOLING – GIA2 over temperature. The GIA2 temperature is too high. If problem persists, the system should be serviced. GIA2 COOLING – GIA2 temperature too low. The GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. GIA2 MANIFEST – GIA2 software mismatch, communication halted. The GIA 2 has incorrect software installed. The system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. The GIA2 self-test has detected a problem in the unit. The system should be serviced. GMA XTALK – GMA crosstalk error has occurred. An error has occurred in transferring data between the two GMAs. The system should be serviced. Index Appendix Annun/Alerts Additional Features AFCS Nav/Com/ XPDR/Audio EIS Flight Instruments Message Hazard Avoidance Annunciations & Alerts The audio panel configuration settings do not match GMA1 CONFIG – GMA1 configuration backup configuration memory. The system should be error. Config service req’d. serviced. GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced. GMA1 MANIFEST – GMA1 software mismatch. Communication halted. The audio panel has incorrect software installed. The system should be serviced. The audio panel self-test has detected a problem in the GMA1 SERVICE – GMA1 needs service. unit. Certain audio functions may still be available, and Return unit for repair. the audio panel may still be usable. The system should be serviced when possible. 148 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Message Flight Instruments Comments The audio panel configuration settings do not match GMA2 CONFIG – GMA2 configuration backup configuration memory. The system should be error. Config service req’d. serviced. GMA2 MANIFEST – GMA2 software mismatch. Communication halted. The audio panel has incorrect software installed. The system should be serviced. GMC MANIFEST – GMC software mismatch, communication halted. The GMC 710 has incorrect software installed. The system should be serviced. GPS NAV LOST – Loss of GPS navigation. GPS fail. Loss of GPS navigation due to GPS failure. GPS NAV LOST – Loss of GPS navigation. Insufficient satellites. Loss of GPS navigation due to insufficient satellites. GPS NAV LOST – Loss of GPS navigation. Position error. Loss of GPS navigation due to position error. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in GPS receiver #1. The system should be serviced. GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 receiver. The receiver may still be available. The system should be serviced. GPS2 FAIL – GPS2 is inoperative. A failure has been detected in GPS receiver #2. The system should be serviced. GPS2 SERVICE – GPS2 needs service. Return unit for repair. A failure has been detected in the GPS2 receiver. The receiver may still be available. The system should be serviced. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index A key is stuck on the GCMC 710 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. Appendix GMC KEYSTK – GMC [keyname] Key is stuck Annun/Alerts A failure has been detected in the GMC 710. The GMC 710 is unavailable. Additional Features GMC FAIL – GMC is inoperative. AFCS Error in the configuration of the GMC 710. Hazard Avoidance GMC CNFG – GMC Config error. Config service req’d. Flight Management The audio panel self-test has detected a problem in the GMA2 SERVICE – GMA2 needs service. unit. Certain audio functions may still be available, and Return unit for repair. the audio panel may still be usable. The system should be serviced when possible. Nav/Com/ XPDR/Audio The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced. EIS GMA2 FAIL – GMA2 is inoperative. 149 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts Message Comments GRA1 CAL – GRA1 calibration error. Service req’d. A calibration error has been detected in the GRA. The system should be serviced. GRA1 CONFIG – GRA1 config error. Config service req’d. The GRA configuration settings do not match those of backup configuration memory. The system should be serviced. GRA1 MANIFEST – GRA1 software mismatch, communication halted. The GRA has incorrect software installed. The system should be serviced. GRA1 SERVICE – GRA1 needs service. A failure has been detected in the GRA. The system Return unit for repair. should be serviced. GRA1 TEMP – GRA1 over temperature. The GRA temperature is too high. If the problem persists, the system should be serviced. GRS1 MANIFEST – GRS1 software mismatch, communication halted. The #1 AHRS has incorrect software installed. The system should be serviced. GRS2 MANIFEST – GRS2 software mismatch, communication halted. The #2 AHRS has incorrect software installed. The system should be serviced. GSD1 CONFIG – GSD1 config error. Config service req’d. GSD1 and the CDU have different copies of the GSD1 configuration. GSD1 COOLING – GSD1 temperature too low. GSD1 is reporting a low temperature condition. GSD1 MANIFEST – GSD1 software mismatch. Communication halted. GSD1 has incorrect software installed. The system should be serviced. GSD1 SERVICE – GSD1 needs service. GSD1 is reporting an internal error condition. The GSD Return unit for repair. may still be usable. GSR1 FAIL – GSR1 has failed. A failure has been detected in the #1 GSR 56. The system should be serviced. GTS CONFIG – GTS Config error. Config service req'd. The GTS and GDU have different copies of the GTS configuration, or the Mode S address is invalid. The system should be serviced. GTS MANIFEST – GTS software mismatch, communication halted. The GTS has incorrect software installed. The system should be serviced. GTX1 MANIFEST – GTX1 software mismatch, communication halted. The transponder has incorrect software installed. The system should be serviced. GTX2 MANIFEST – GTX2 software mismatch, communication halted. The transponder has incorrect software installed. The system should be serviced. 150 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Comments GWX CONFIG – GWX config error. Config service req’d. GWX 68/70 configuration settings do not match those of the GDU configuration. The system should be serviced. GWX FAIL – GWX is inoperative. The GDU is not recieving status packet from the GWX 68/70 or the GWX 68/70 is reporting a fault. The GWX 68/70 radar system should be serviced. GWX MANIFEST – GWX software mismatch, communication halted. The GWX 68/70 has incorrect software installed. The system should be serviced. GWX SERVICE – Needs service. Return unit for repair. A failure has been detected in the GWX 68/70. The GWX 68/70 may still be usable. Nav/Com/ XPDR/Audio HDG FAULT – AHRS1 magnetometer fault has occurred. A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced. Flight Management HDG FAULT – AHRS2 magnetometer fault has occurred. A fault has occurred in the #2 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced. HOLD EXPIRED – Holding EFC time expired. Expect Further Clearance (EFC) time has expired for the User Defined Hold. AFCS A GIA mismatch has been detected, where only one is SBAS capable. The system should be serviced. Additional Features The aircraft is inside the special use airspace. INVALID ADM – Invalid ADM: ATN communication halted. Data link avionics were not configured correctly and therefore will not be able to communicate with the ground network. LOCKED FPL – Cannot navigate locked flight plan. This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. LOI – GPS integrity lost. Crosscheck with other NAVS. GPS integrity is insufficient for the current phase of flight. Index 151 Appendix Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Annun/Alerts INSIDE ARSPC – Inside airspace. 190-02042-00 Rev. B Hazard Avoidance HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. EIS HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. Flight Instruments Message Message Comments LRG MAG VAR – Verify all course angles. The GDU’s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles. Displayed magnetic course angles may differ from the actual magnetic heading by more than 2°. MANIFEST – GFC software mismatch, communication halted. Incorrect servo software is installed, or gain settings are incorrect. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts MANIFEST – GMU1 software mismatch, communication halted. MANIFEST – GMU2 software mismatch, communication halted. MANIFEST – MFD1 software mismatch. Communication halted. MANIFEST – PFD1 software mismatch. Communication halted. MANIFEST – PFD2 software mismatch. Communication halted. The GMU 44 has incorrect software installed. The system should be serviced. The MFD has incorrect software installed. The system should be serviced. The PFD has incorrect software installed. The system should be serviced. MFD1 CONFIG – MFD1 configuration error. Config service req’d. The MFD configuration settings do not match backup configuration memory. The system should be serviced. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. The MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 Airport Directory database error exists. The MFD detected a failure in the Airport Directory database. Ensure the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 basemap database error exists. The MFD detected a failure in the basemap database. The system should be serviced. MFD1 DB ERR – MFD1 Chartview database error exists. The MFD detected a failure in the Chartview database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 FliteCharts database error exists. The MFD detected a failure in the FliteCharts database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. 152 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Comments MFD1 DB ERR – MFD1 navigation database error exists. The MFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 obstacle database error exists. The MFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 obstacle database missing. The obstacle database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 Safe Taxi database error exists. The MFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 terrain database error exists. The MFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the system should be serviced. MFD1 DB ERR – MFD1 terrain database missing. The terrain database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. MFD1 KEYSTK – MFD1 [key name] Key is stuck A key is stuck on the MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. MFD1 SERVICE – MFD1 needs service. Return unit for repair. The MFD self-test has detected a problem. The system should be serviced. Flight Instruments Message EIS Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix NAV DB UPDATED – Active navigation database updated. System has updated the active navigation database from the standby navigation database. 153 Index The MFD voltage is low. The system should be serviced. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Flight Management MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage. 190-02042-00 Rev. B Nav/Com/ XPDR/Audio MFD1 SOFTWARE – MFD1 mismatch, The specified GDU has different software versions communication halted. installed. The system should be serviced. Message Comments NAV1 MANIFEST – NAV1 software mismatch, communication halted. NAV1 software mismatch. The system should be serviced. NAV1 RMT XFR – NAV1 remote transfer key is stuck. The remote NAV1 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. A failure has been detected in the NAV1 receiver. The NAV1 SERVICE – NAV1 needs service. receiver may still be available. The system should be Return unit for repair. serviced. NAV2 MANIFEST – NAV2 software mismatch, communication halted. NAV2 software mismatch. The system should be serviced. NAV2 RMT XFR – NAV2 remote transfer key is stuck. The remote NAV2 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. A failure has been detected in the NAV2 receiver. The NAV2 SERVICE – NAV2 needs service. receiver may still be available. The system should be Return unit for repair. serviced. NO WGS84 WPT – Non WGS 84 waypoint for navigation -[xxxx] The position of the selected waypoint [xxxx] is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed. Do not use GPS to navigate to the selected non-WGS84 waypoint. NON-MAG UNITS– Non-magnetic NAV ANGLE display units are active. Navigation angle is not set to MAGNETIC at power-up. PFD1 CONFIG – PFD1 configuration error. Config service req’d. The PFD configuration settings do not match backup configuration memory. The system should be serviced. PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. The PFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced. PFD1 DB ERR – PFD1 basemap database error exists. The PFD detected a failure in the basemap database. The system should be serviced. PFD1 DB ERR – PFD1 navigation database error exists. The PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts 154 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Comments PFD1 DB ERR – PFD1 obstacle database error exists. The PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. PFD1 DB ERR – PFD1 obstacle database missing. The obstacle database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. PFD1 DB ERR – PFD1 Safe Taxi database error exists. The PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. PFD1 DB ERR – PFD1 terrain database error exists. The PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the system should be serviced. PFD1 DB ERR – PFD1 terrain database missing. The terrain database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. PFD1 KEYSTK – PFD1 [key name] Key is stuck. A key is stuck on the PFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. [PFD1, PFD2, or MFD1] BKLT CAL INV – calibration lost or mismatch. Return for repair. The PFD1, PFD2 and/or MFD backlight calibration cannot be found or is invalid. The system should be serviced. [PFD1, PFD2, or MFD1] CARD 1 ERR – Card 1 is invalid. The SD card in the top card slot of the specified PFD or MFD contains invalid data. [PFD1, PFD2, or MFD1] CARD 2 ERR – Card 2 is invalid. The SD card in the bottom card slot of the specified PFD or MFD contains invalid data. Flight Instruments Message Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Nav/Com/ XPDR/Audio The SD card was removed from the bottom card slot [PFD1, PFD2, or MFD1] CARD 2 REM of the specified PFD or MFD. The SD card needs to be – Card 2 was removed. Reinsert card. reinserted. 190-02042-00 Rev. B EIS The SD card was removed from the top card slot of [PFD1, PFD2, or MFD1] CARD 1 REM the specified PFD or MFD. The SD card needs to be – Card 1 was removed. Reinsert card. reinserted. 155 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts Message Comments PFD1 SERVICE – PFD1 needs service. Return unit for repair. The PFD1 self-test has detected a problem. The system should be serviced. PFD1 SOFTWARE – PFD1 mismatch, communication halted. The specified GDU has different software versions installed. The system should be serviced. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage. The PFD1 voltage is low. The system should be serviced. PFD2 CONFIG – PFD2 configuration error. Config service req’d. The PFD configuration settings do not match backup configuration memory. The system should be serviced. PFD2 COOLING – PFD2 has poor cooling. Reducing power usage. The PFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 basemap database error exists. The PFD detected a failure in the basemap database. The system should be serviced. PFD2 DB ERR – PFD2 navigation database error exists. The PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 obstacle database error exists. The PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 obstacle database missing. The obstacle database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 Safe Taxi database error exists. The PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 terrain database error exists. The PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the system should be serviced. PFD2 DB ERR – PFD2 terrain database missing. The terrain database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the system should be serviced. 156 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts PFD2 KEYSTK – PFD2 [key name] Key is stuck A key is stuck on the PFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. PFD2 SERVICE – PFD2 needs service. Return unit for repair. The PFD2 self-test has detected a problem. The system should be serviced. PFD2 SOFTWARE – PFD2 mismatch, communication halted. The specified GDU has different software versions installed. The system should be serviced. PFD2 VOLTAGE – PFD2 has low voltage. Reducing power usage. The PFD2 voltage is low. The system should be serviced. PTK FAIL – Parallel track unavailable: bad geometry. Bad parallel track geometry. PTK FAIL – Parallel track unavailable: invalid leg type. Invalid leg type for parallel offset. PTK FAIL – Parallel track unavailable: past IAF. IAF waypoint for parallel offset has been passed. REGISTER CONNEXT – Data services are inoperative, register w/CONNEXT. The GDL 59 is not registered with Garmin Flight Data Services, or its current registration data has failed authentication. SCHEDULER [#] – <message>. Message criteria entered by the user. SLCT FREQ – Select appropriate frequency for approach. The system notifies the pilot to load the approach frequency for the appropriate NAV receiver. Select the correct frequency for the approach. SLCT MAG – Select MAGNETIC NAV ANGLE display units. The Navigation angle is non-magnetic. Select the MAGNETIC NAV ANGLE display units. SLCT NAV – Select NAV on CDI for approach. The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to the correct NAV receiver. SLCT NON-MAG – Select alternate NAV ANGLE display units. The Navigation angle is magnetic. Select the alternate NAV ANGLE display units. STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. STRMSCP FAIL – Stormscope has failed. Stormscope has failed. The system should be serviced. SURFACEWATCH DISABLED - Too far north/south. The SurfaceWatch system has been disabled. Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Nav/Com/ XPDR/Audio 190-02042-00 Rev. B EIS Comments Flight Instruments Message 157 Message Comments SURFACEWATCH FAIL - Invalid audio configuration. The SurfaceWatch system has failed due to an invalid audio configuration. SURFACEWATCH FAIL - Invalid configurable alerts. The SurfaceWatch system has failed due to invalid configurable alerts. The SurfaceWatch system has been inhibited. SVT – DISABLED: Out of available terrain region. Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database. SVT – DISABLED: Terrain DB resolution too low. Synthetic Vision is disabled because a terrain database of sufficient resolution (4.9 arc-second or better) is not currently installed. TERRAIN AUD CFG – Trn Awareness audio config error. Service req’d. Terrain audio alerts are not configured properly. The system should be serviced TERRAIN DISABLED – Terrain Awareness DB resolution too low. TAWS is disabled because a terrain database of sufficient resolution (4.9 arc-second or better) is not currently installed. TERRAIN DSP – [PFD1, PFD2 or MFD1] Terrain awareness display unavailable. One of the terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid. TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has expired. TRAFFIC FAIL – Traffic device has failed. The system is no longer receiving data from the traffic system. The traffic device should be serviced. TRN AUD FAIL – Trn Awareness audio source unavailable. The audio source for terrain awareness is offline. Check GIA1 or GIA 2. UNABLE RNP – Estimated position error exceeds RNP. The estimated GPS position error exceeds the RNP limits. Check GPS sensors. UNABLE RNP APR – GPS integrity lost. Check GPS sensors. The estimated GPS position error exceeds the requirements for the current approach. Check GPS sensor UNABLE V WPT – Can’t reach current vertical waypoint. The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. Index Appendix Annun/Alerts Additional Features AFCS Nav/Com/ XPDR/Audio SURFACEWATCH INHIBITED Surfacewatch inhibited. Flight Management SURFACEWATCH FAIL - One or more The SurfaceWatch system has failed due to one or more inputs invalid. invalid inputs. Hazard Avoidance EIS Flight Instruments Annunciations & Alerts 158 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts User magnetic variation mode was selected during previous operation and is still active (checked at powerup.) VNV UNAVAILABLE. – Excessive crosstrack error. The current crosstrack exceeds the limit, causing vertical deviation to go invalid. VNV UNAVAILABLE. – Excessive track angle error. The current track angle error exceeds the limit, causing the vertical deviation to go invalid. Nav/Com/ XPDR/Audio USER MAG VAR – User magnetic variation is active. EIS Comments Flight Instruments Message VNV UNAVAILABLE. – Parallel course A parallel course has been selected, causing the vertical selected. deviation to go invalid. Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. WX ALERT – Possible severe weather ahead. The GWX 68/70 indicates severe weather within ±10 degrees of the aircraft heading at a range of 80 to 320 nm. XPDR1 ADS-B 1090 – Datalinik: ADS-B 1090 receiver has failed. A failure has been detected in the 1090 receiver. XPDR1 ADS-B FAIL – Transponder: XPDR1 is unable to transmit ADS-B messages. ADS-B is inoperative. The transponder may not be receiving a valid GPS position. Other transponder functions may be available. Service when possible. AFCS WPT ARRIVAL – Arriving at waypoint -[xxxx] Additional Features XPDR1 ADS-B TRFC – Transponder: ADS-B traffic has failed The Transponder is incapable of processing traffic information. Appendix The transponder is not able to receive position information. Annun/Alerts XPDR1 ADS-B NO POS – The transponder is not able to receive position Transponder: ADS-B is not transmitting information. position. XPDR1 ADS-B NO TX – Transponder: ADS-B out failed. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index XPDR1 ADS-B UAT – Datalink: ADS-B A failure has been detected in the UAT receiver. in UAT receiver has failed. 190-02042-00 Rev. B Hazard Avoidance The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint. Flight Management VNV UNAVAILABLE. - Unsupported leg type in flight plan. 159 Message Comments The transponder configuration settings do not match XPDR1 CONFIG – XPDR1 config error. those of backup configuration memory. The system Config service req’d. should be serviced. XPDR1 CSA FAIL - Traffic: ADS-B In traffic alerting has failed. ADS-B Conflict Situational Awareness (CSA) is unavailable. XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1 or #2 transponder. XPDR1 FAULT – Datalink: ADSB-B in has failed. The transponder is unable to receive ADS-B information. XPDR1 FIS-B WX – Datalink: FIS-B Weather has failed. The transponder is unable to receive FIS-B weather information. XPDR1 OVER TEMP - Transponder: Transponder over temp. The system has detected an over temperature condition in XPDR1. The transmitter operates at reduced power. If the problem persists, the system should be serviced. XPDR1 PRES ALT –Transponder: ADS-B no pressure altitude. Unable to provide pressure altitude information. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. The #1 transponder should be serviced when possible. XPDR1 UNDER TEMP - Transponder: Transponder under temp. The system has detected an under temperature condition in XPDR1. The transmitter operates at reduced power. If the problem persists, the system should be serviced. XPDR2 ADS-B 1090 – Datalinik: ADS-B 1090 receiver has failed. A failure has been detected in the 1090 receiver. XPDR2 ADS-B FAIL – XPDR2 is unable to transmit ADS-B messages. ADS-B is inoperative. The transponder may not be receiving a valid GPS position. Other transponder functions may be available. Service when possible. XPDR2 FIS-B WX – Datalink: FIS-B Weather has failed. The transponder is unable to receive FIS-B weather information. XPDR2 ADS-B NO POS – The transponder is not able to receive position Transponder: ADS-B is not transmitting information. position. XPDR2 ADS-B NO TX – Transponder: ADS-B out failed. The transponder is not able to receive position information. XPDR2 ADS-B TRFC – Transponder: ADS-B traffic has failed The Transponder is incapable of processing traffic information. Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts 160 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Annunciations & Alerts Message Flight Instruments Comments XPDR2 ADS-B UAT – Datalink: ADS-B A failure has been detected in the UAT receiver. in UAT receiver has failed. EIS The transponder configuration settings do not match XPDR2 CONFIG – XPDR2 config error. those of backup configuration memory. The system Config service req’d. should be serviced. XPDR2 FAIL – XPDR2 is inoperative. There is no communication with the #2 transponder. XPDR2 FAULT – Datalink: ADSB-B in has failed. The transponder is unable to receive ADS-B information. XPDR2 PRES ALT –Transponder: ADS-B no pressure altitude. Unable to provide pressure altitude information. XPDR2 SRVC – XPDR2 needs service. Return unit for repair. The #2 transponder should be serviced when possible. XPDR2 UNDER TEMP - Transponder: Transponder under temp. The system has detected an under temperature condition in XPDR2. The transmitter operates at reduced power. If the problem persists, the system should be serviced. XTALK ERROR – A flight display crosstalk error has occurred. The MFD and PFD are not communicating with each other. The system should be serviced. Flight Management ADS-B Conflict Situational Awareness (CSA) is unavailable. Nav/Com/ XPDR/Audio XPDR2 CSA FAIL - Traffic: ADS-B In traffic alerting has failed. Hazard Avoidance AFCS Additional Features Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 161 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Annunciations & Alerts Index Appendix Annun/Alerts Additional Features AFCS Blank Page 162 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Flight Instruments APPENDIX PFD SOFTKEY MAPS (With TCAS II ) OR EIS OR Nav/Com/ XPDR/Audio (Only available with GWX70) Flight Management Hazard Avoidance AFCS Additional Features Annun/Alerts PFD Map/HSI Softkeys Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 163 Appendix Flight Instruments (With TCAS II ) OR EIS OR Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio (See Sensor Softkeys Figures) Annun/Alerts Additional Features AFCS PFD Opt Softkey Index Appendix Sensor Softkeys with GSU 75B (ADAHRS) or GRS 77 (Legacy AHRS) 164 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Flight Instruments EIS Nav/Com/ XPDR/Audio Flight Management Sensor Softkeys with GRS 7800 (AHRS) Hazard Avoidance AFCS Additional Features XPDR Softkeys without TCAS II Annun/Alerts Appendix Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 165 XPDR Softkeys with TCAS II Level 1 Map/HSI Or Map Opt Level 2 Level 3 Appendix Index Description Displays the PFD Map selection softkeys. Map Off 166 Level 4 Displays the PFD Map display settings softkeys. Layout Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Appendix Removes the PFD map from display (Inset, HSI, or Traffic) Inset Map Displays the Inset Map HSI Map Displays the HSI Map TFC Map Replaces the PFD Map with a dedicated traffic display. Wx LGND Displays/removes the name of the selected data link weather provider (SiriusXM, Connext) and the weather product icon and age box (for enabled weather products). Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Level 2 Detail Level 3 Level 4 Description Rel Ter Displays relative terrain information on the PFD Map NEXRAD Displays XM NEXRAD weather and coverage on PFD Map (subscription optional) METAR Displays METAR information on Inset Map (subscription optional) Lightning Adds/removes the display of SiriusXM or Connext lightning information (based on data link weather source selection) on the PFD Map. Datalink Selects the data link weather source for the PFD Map STRMSCP Adds or removes the display of Stormscope information on the PFD Map. The softkey annunciator is green when the function is on. When the function is off, the annunciator is gray. RDR Opt Displays softkeys for airborne weather radar options (WX 70 only). 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 167 Index When enabled, displays the airborne weather radar overlay on HSI Map (WX 70 only). Appendix Wx Radar Annun/Alerts Disables lightning function on PFD Map. The softkey annunciator is green when the lightning function is off. Additional Features LTNG Off AFCS Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on PFD Map Hazard Avoidance Topo Flight Management Displays traffic information on PFD Map. Nav/Com/ XPDR/Audio Traffic EIS Selects desired amount of map detail: All (No Declutter): All map features visible Detail 1: Declutters land data Detail 2: Declutters land and SUA data Detail 3: Removes everything except for the active flight plan Flight Instruments Level 1 Flight Instruments Appendix Level 1 Level 2 Level 3 Mode SEL Level 4 Displays softkeys for weather radar mode selection (WX 70 only). EIS Off Disables weather radar mode (WX 70 only). Standby Selects Standby weather radar mode (WX 70 only). Weather Activates Weather radar mode (WX 70 only). Ground Activates Ground Map weather radar mode (WX 70 only). Decreases weather radar gain setting (WX 70 only). Increases weather radar gain setting (WX 70 only). Gain + Stab Activates antenna stabilization feature (WX 70 only). ACT Activates Altitude Compensated Tilt feature (WX 70 only). AFCS Flight Management Gain - Hazard Avoidance Nav/Com/ XPDR/Audio Description TFC Map Replaces the PFD Map with a dedicated traffic display. PFD Opt Displays second-level softkeys for additional PFD options. SVT Displays additional SVT overlay softkeys Additional Features Pathways Displays compass heading along the ZeroPitch line. APT Sign Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm. Index Wind 168 Enables synthetic terrain depiction. HDG LBL Appendix Annun/Alerts Terrain Displays Pathway Boxes on the Synthetic Vision Display. Displays the wind option softkeys Option 1 Headwind/Tailwind and crosswind components. Option 2 Wind direction arrow and speed. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Level 2 Level 3 Option 3 Level 4 Description Flight Instruments Level 1 Wind direction arrow with direction and speed. Off Wind information not displayed. DME Bearing 1 EIS Displays DME Information Window Sensors Displays the sensor selection softkeys. ADC ADC 1 Selects the #1 ADC. ADC 1 Selects the #2 ADC. AHRS Flight Management Displays ADC selection softkeys. Displays the AHRS selection softkeys. Selects the #1 AHRS. AHRS 2 Selects the #2 AHRS. Hazard Avoidance AHRS 1 HDG Selects desired DG Mode: (GRS 7800 only). Slave: Slaves the DG to the AHRS. Free: Allows the DG to enter FREE mode. HDG - Slews heading counterclockwise (GRS 7800 only). HDG + Slews heading clockwise (GRS 7800 only). Synchronizes heading to the selected heading (GRS 7800 only). TRK Sync Synchronizes heading to the current track (GRS 7800 only). Displays softkeys to select altitude unit parameters. 190-02042-00 Rev. B Index ALT Units When enabled, displays altimeter in meters. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Appendix Cycles the Bearing 2 Information Window through NAV1, NAV2, GPS/waypoint identifier and GPS-derived distance information, ADF/ frequency, and Off. Annun/Alerts HDG Sync Additional Features DG AFCS Displays the softkeys for selecting one of the two DG modes (GRS 7800 only). Bearing 2 Meters Nav/Com/ XPDR/Audio Cycles the Bearing 1 Information Window through NAV1, NAV2, GPS/waypoint identifier and GPS-derived distance information, ADF/frequency, and Off. 169 Flight Instruments Appendix Level 1 Level 2 Level 3 IN STD Baro Description Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals. Sets barometric pressure to 29.92 in Hg (1013 hPa if metric units are selected) OBS Selects OBS mode on the CDI when navigating by GPS (only available with active leg). When OBS is on, the softkey annunciator is green. CDI Cycles through FMS, NAV1, and NAV2 navigation modes on the CDI. DME Displays the DME Tuning Window, allowing tuning and selection of the DME (optional). Transponder Softkeys without TCAS II XPDR Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS HPA Level 4 170 Displays the transponder selection softkeys. XPDR 1 Selects the #1 transponder as active. XPDR 2 Selects the #2 transponder as active. Standby Selects transponder Standby Mode (transponder does not reply to any interrogations). On Activates transponder (transponder replies to identification interrogations). ALT Altitude Reporting Mode (transponder replies to identification and altitude interrogations). VFR Automatically enters the VFR code (1200 in the U.S.A. only) Code Displays transponder code selection softkeys 0-7. 0-7 Use numbers to enter code. Ident Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen. BKSP Removes numbers entered, one at a time. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Level 2 Ident Level 3 Level 4 Description Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen. EIS Transponder Softkeys with TCAS II XPDR/ TFC XPDR2 Selects the #2 transponder as active Mode Displays transponder mode selection softkeys Activates transponder (transponder replies to identification interrogations). When the transponder is set to ON, the TCAS II system is set to standby. ALT Altitude Reporting Mode (transponder replies to identification and altitude interrogations). When the transponder is set to ALT, the TCAS II system is set to standby. TA Only Activates the TCAS II system in TA Only Mode and sets the transponder to ALT. TCAS Activates the TCAS II system in TA/RA Mode and sets the transponder to ALT. Displays the TCAS control softkeys. Displays intruder altitude as altitude relative to own aircraft altitude. Absolute Displays intruder MSL altitude. ALT RNG Displays the altitude display range softkeys. Appendix Relative Annun/Alerts TA/RA Additional Features On AFCS Selects transponder Standby Mode (transponder does not reply to any interrogations). When the transponder is set to standby, the TCAS II system is also set to standby. Hazard Avoidance Standby Flight Management Selects the #1 transponder as active Nav/Com/ XPDR/Audio XPDR1 Flight Instruments Level 1 Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 171 Level 1 Level 2 Level 3 Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Appendix Hazard Avoidance AFCS Code Annun/Alerts Additional Features Ident Ident Displays non-threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. Normal Displays non-threat traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. Below Displays non-threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight. UNREST Test Description All traffic is displayed. Activates Test Mode and displays test intruder symbols. Displays transponder code selection softkeys 0-7. 0-7 Use numbers to enter code. Ident Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen. BKSP Removes numbers entered, one at a time. Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen. Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen. Tmr/Ref Displays Timer/References Window. Nearest Displays Nearest Airports Window. Index Appendix Level 4 Above 172 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Flight Instruments EIS Nav/Com/ XPDR/Audio Flight Management Hazard Avoidance AFCS MFD Navigation Map Page Softkeys Level 1 Level 2 Level 3 Description Additional Features Map Opt Displays traffic information on Navigation Map Page. Inset Displays inset window second level softkeys. VSD Displays VSD profile information of terrain/obstacles along the current track, vertical track vector, and selected altitude. Auto: Automatically displays either VSD profile information for active flight plan information or along current track with no active flight plan. FPL: Displays VSD profile information for active flight plan. TRK: Displays VSD profile information along current track. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 173 Index Removes VSD inset from Navigation Map Page. Appendix 190-02042-00 Rev. B Off Annun/Alerts Traffic Level 1 Level 2 AWY Displays airways on the map; cycles through the following: Off: No airways are displayed. On: All airways are displayed. Low: Only low altitude airways are displayed. High: Only high altitude airways are displayed. STRMSCP Displays Stormscope information on Navigation Map Page (optional). NEXRAD Displays XM NEXRAD weather and coverage on Navigation Map Page (optional). XM LTNG Displays XM lightning information on Navigation Map Page (optional). Nav/Com/ XPDR/Audio Flight Management Hazard Avoidance AFCS METAR Displays METAR information on Inset Map (subscription optional). Legend Displays legends for the displayed XM Weather products (optional). Displays XM weather radar information on Navigation Map Page (optional). Selects desired amount of map detail; cycles through the following levels: Detail All: All map features visible. Annun/Alerts Additional Features Description Displays terrain on the map; cycles through the following: Off: No terrain information shown on MFD Map. Topo: Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on MFD Map. REL: Displays relative terrain information on the MFD Map. WX Radar Detail Level 3 TER EIS Flight Instruments Appendix Detail-1: Declutters land data. Detail-2: Declutters land and SUA data. Index Appendix Detail-3: Removes everything except for the active flight plan. 174 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix Level 2 Level 3 Charts Description Flight Instruments Level 1 When available, displays optional airport and terminal procedure charts. CHRT Opt Displays chart display settings softkeys. Profile Displays the header view (approach chart briefing strip) on the screen. Nav/Com/ XPDR/Audio Plan Displays the entire chart on the screen. EIS All Header Displays the approach chart two dimensional plan view. Displays the approach chart descent profile strip. bottom of the approach chart. Full SCN Removes data window to display chart on screen. Displays the WPT–Airport Information page. Displays airport information: Info 1: Displays Airport Information Page Info 2: Displays Airport Directory Page AFCS DP Changes the chart size to fit the available screen width. Hazard Avoidance Show Map Info Fit WDTH Flight Management Minimums Displays the minimum descent altitude/visibility strip at the Displays departure procedure chart. APR Displays approach procedure chart. WX Displays airport weather information chart. Appendix NOTAM Annun/Alerts Displays standard terminal arrival procedure chart. Additional Features STAR Displays NOTAM information for selected airport, when available. Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 175 LOADING UPDATED DATABASES Database information is obtained from third party sources. Inaccuracies in the data may be discovered from time to time. Garmin communicates this information by issuing a Database Alert. These notifications are available on http://fly.garmin.com. Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to http:// fly.garmin.com and select Aviation Data Error Report. CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system. Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Appendix In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional. It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features. Updating Databases: With the system OFF, remove an SD Card from the bottom SD card slot of the MFD. 2) Download and install the databases on an SD card. 1) Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance NOTE: When loading database updates, the ‘DB Mismatch’ message will be displayed until database synchronization is complete, followed by turning system power off, then on. Synchronization can be monitored on the AuxDatabase Page. 176 3) Put the SD Card in the bottom SD card slot of the MFD. 4) Turn the system ON. 5) Press the ENT Key or the right most softkey on MFD display to acknowledge the startup screen. 6) Turn the large FMS Knob to select the Aux page group on the MFD. 7) Turn the small FMS Knob to select the Database page group on the MFD. Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix ITT temperature is less than 200° F. 10) Press the Restart Softkey. A 10 second restart countdown will appear. Flight Management 11) Press the Restart Button in the display window to continue with the restart of the system, or remove power from the system if the Restart Softkey is diminished. 12) Remove the SD card from the bottom slot of the MFD. Nav/Com/ XPDR/Audio NOTE: The Restart Softkey is enabled only when the engines are off and EIS 9) Monitor the Sync Status on the Database page. Wait for all databases to complete syncing, indicated by ‘Sync Complete’ being displayed. A cyan double arrow will appear between the Standby and Active colums to show which Standby databases will be transferred to Active at the next power cycle. Verify the correct database cycle information is shown in the Standby Database column. Flight Instruments 8) Hazard Avoidance 13) After restarting the system, turn the large FMS Knob and select the Aux page group on the MFD. 14) Turn the small FMS Knob and select the Databases page. AFCS 15) Verify that the standby databases transferred and are now in the active database column. Annun/Alerts a) Press the FMS Knob. The first database title on the screen will be selected. Additional Features 16) To view database information for an individual display, press and then turn the FMS Knob to select the database, and then press the Details Softkey. Press the ENT Key or the FMS Knob to exit. 17) To manually activate any databases that did not transfer to the active column: b) Turn the small FMS Knob as necessary to select the database title. d) Remove and reapply power to the system. Appendix c) Press the ENT Key. A cyan double-sided arrow will appear indicating that the standby database will become active. e) Verify that the standby databases transferred and are now in the active database column. Index 18) Remove power from the system. 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 177 LOADING UPDATED DATABASES USING FLIGHT STREAM 510 Updating Databases from any MFD page (except the Aux - Databases page): 1) Insert the Flight Stream 510 SD Card in the bottom slot of the MFD. 2) 3) 4) Press the Update softkey when the Database Update screen appears. The Flight Stream 510 will enter Wifi mode. Put the mobile device in Wifi mode. 5) Connect the mobile device to the Flight Stream 510 Wifi (refer to the Additional Features section). The Wifi Not Connected screen will close when the Wifi connection is established. 6) 7) When the transfer is complete, press the Close softkey. When an existing database is expired and a new one is ready to become active, a Database Expired window will appear. Continue to the next step to restart the system. Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Appendix NOTE: The Restart Softkey is enabled only when the engines are off and Additional Features AFCS ITT temperature is less than 200° F. 8) Press the Restart softkey to restart the system and load the updated database(s), or remove power from the system if the Restart Softkey is diminished . 9) After restarting the system, turn the large FMS Knob and select the Aux page group on the MFD. 10) Turn the small FMS Knob and select the Databases page. Annun/Alerts 11) Verify that the standby databases transferred and are now in the active database column. Appendix 12) To view database information for an individual display, press and then turn the FMS Knob to select the database, and then press the Details Softkey. Press the ENT Key or the FMS Knob to exit. 13) To manually activate any databases that did not transfer to the active column: Index a) Press the FMS Knob. The first database title on the screen will be selected. b) Turn the small FMS Knob as necessary to select the database title. 178 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Appendix d) Remove and reapply power to the system. 14) Remove power from the system. Flight Management At startup, the system compares this version of the MV DB with that presently being used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs to be updated, a prompt is displayed on the MFD. Note, in the following example, GRS1 is the first AHRS to indicate an update is available. In actuality, this is dependent on which AHRS is the first to report status to the system. GRS2 may be displayed before GRS1. The order is not important, only that both AHRS be updated. Nav/Com/ XPDR/Audio Magnetic Field Variation Database Update EIS e) Verify that the standby databases transferred and are now in the active database column. Flight Instruments c) Press the ENT Key. A cyan double-sided arrow will appear indicating that the standby database will become active. Hazard Avoidance AFCS GRS1 Magnetic Field Variation Database Update Prompt Additional Features Loading the magnetic field variation database update: 1) With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key on the MFD. A progress monitor is displayed as shown in the following figure. Annun/Alerts Appendix Uploading Database to GRS1 Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 179 Appendix When the upload is complete, the prompt for the next GRS upload is displayed, as seen in the following figure. EIS Flight Instruments 2) Nav/Com/ XPDR/Audio GRS2 Magnetic Field Variation Database Update Prompt With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor is displayed as shown in the following figure. When the upload is complete, the system is ready for use. AFCS Hazard Avoidance Flight Management 3) Index Appendix Annun/Alerts Additional Features Uploading Database to GRS2 180 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Index Cargo 51 CDI 2, 10, 157 Cell 56 Cell mode 56 ChartView 98, 99 Closest Point 35 Code selection softkeys 9 COM 9, 10 Data Link Receiver 137 Day/Night views 100 DB Mismatch 176 DCLTR Softkey 98 Deleting An entire airway 32 An entire procedure 33 An individual waypoint 32, 33 Departure Procedure 43, 44 Select 43, 45, 46 DG Mode 2 Direct-to 13, 23, 24, 25 DME 9, 10 Hazard Avoidance AFCS Additional Features E Electronic Stability and Protection (ESP) 126, 127, 128 Export a Flight Plan 30 Appendix F Annun/Alerts Barometric Altitude Minimums 4 Basic Empty Weight 50 Bearing Line 72, 74 Bluetooth 30 D Flight Management B Nav/Com/ XPDR/Audio Access code 60, 102 Active Channel 119 ADF 9, 10 Advisory alerts 129 AHRS 141, 142, 146, 147, 149, 151 Air Data Computer 130 Airport Directory 101 AC-U-KWIK 101 AOPA 101 Airport Information 19 Airport Signs 97 Along Track Offset 33 Altitude Constraints 39 AP 131 Approach Activating 48 Channel 46 Loading 46, 48 Removing 48 APR softkey 49 Arrival procedure 45 Attitude & Heading Reference System (AHRS) 130 Audio panel controls NAV1, NAV2 10 Autopilot 131 EIS C Flight Instruments A Flight Director (FD) 91, 131 Flight path marker 97 Index 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index-1 Index Appendix Annun/Alerts Additional Features AFCS Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Index Flight Plan, Active Creating 26 Flight Stream 30 FliteCharts 98, 99 FPA 42 Frequency Transfer 10 Fuel Flow (FFLOW PPH) 8 Fuel on Board 51, 52 Mistrim 131, 132 Mode selection softkeys 9 N Ground Mapping, Weather Radar 75 NAV1/NAV2 10 Navigation Database 39 Nearest Airport 18, 19 Airports Page 18, 19 NO COMP 130 H O HF 9 Horizon Heading 97 Horizontal Scan 72, 73 Horizontal Situation Indicator (HSI) 46 OBS 3 Obstacles 145, 151 Oil Pressure (OIL PSI) 8 Oil Temperature (OIL °C) 8 Overspeed Protection 92 G I Import a Flight Plan 29 Interstage Turbine Temperature (ITT) 8 Inverting a flight plan 29 IOI 133, 134 Iridium satellite network 101, 103, 108 P Jeppesen 99 Parallel Track 34 Passenger(s) 51 Pathways 97 Pending flight plan 30, 31 Pilot and Stores Weight 51 Predefined message 111, 112 Propeller Sync 8 L R Level Mode 127 Lightning 56 Low speed data 101, 102 RAIM 52, 53 Register 60, 102 Resolution Advisory 87 ROC 132, 134 J M MET 131 Minimums 139 MISCOMP 130 Missed Approach 48 Index-2 S SafeTaxi 98 SBAS 53 Scheduler 121 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Index Hazard Avoidance WAAS 151 Waypoint Selection Submenu 24, 26, 27, 52 Weather Attenuated Color Highlight 75 Weather Radar 71 Wi-Fi 116, 117, 118, 119 Flight Management W Nav/Com/ XPDR/Audio AFCS X XPDR Softkey 9 Additional Features Annun/Alerts Appendix Tachometer (PROP RPM) 8 TAS 142 TAWS 132, 134 TCAS II 87 TCAS System Test Fail 140 Pass 140 Telephone 103 Terminal procedures charts 99 Terrain 77, 132, 133, 134, 135, 145 Text messaging 108, 109, 111, 113 Tilt, Antenna 73 Tilt Line 73 Torque (FT-LB) 8 Traffic 55 Traffic Advisory System (TAS) 83, 85 Traffic Advisory (TA) 139, 140 Traffic map page 83, 84, 85 Transponder 9, 170, 171 Turbine Speed (% RPM) 8 Vertical Navigation (VNAV) 25, 39 Direct-to 42 Guidance 40 Vertical track 139 VNAV 159 VNV Guidance Disabling 38 Enabling 38 VRP 20 Vspeed 3 VS TGT 42 EIS T V Flight Instruments Sector Scan 74 Sensor 130 Stabilization, Antenna 74 Standby Navigation Database 177 Stormscope lightning data 56 Strike Mode 56 SurfaceWatch RR-1, 122, 123, 137, 157, 158 Synthetic vision (SVS) 158 Synthetic Vision Technology (SVT) 97 System ID 60 System message advisories 141 U 190-02042-00 Rev. B Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series Index User-Defined Holding Pattern 37 Index-3 Hazard Avoidance Flight Management Nav/Com/ XPDR/Audio EIS Flight Instruments Index Index Appendix Annun/Alerts Additional Features AFCS Blank Page Index-4 Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 300/B300 Series 190-02042-00 Rev. B Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Aircraft On Ground (AOG) Hotline: 913.397.0836 Aviation Dealer Technical Support: 888.606.5482 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.581.8101 f: 503.364.2138 Garmin (Europe) Ltd. Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.K. Tel: +44 (0) 238 052 4000 Fax: +44 (0) 238 052 4004 Aviation Support: +44 (0) 370 850 1243 Garmin Corporation No. 68, Zhangshu 2nd Road Xizhi District, New Taipei City, Taiwan p: 34-93-357-2608 f: 34-93-429-4484 www.garmin.com © 2017 Garmin Ltd. or its subsidiaries 190-02042-00 Rev. B
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