Garmin G1000: Beechcraft King Air 200/B200 G1000 Cockpit Reference Guide for KingAir 200/B200 Series - SSV 0985.03
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G1000 ® Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 200/B200 Series Flight Instruments Nav/Com/Transponder/Audio Panel Automatic Flight Control System GPS Navigation Flight Planning Procedures Hazard Avoidance Additional Features Annunciations & Alerts Appendix INDEx Copyright © 2008-2010 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0985.03 or later for the Beechcraft 200 and B200. 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 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836. Web Site 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®, WATCH®, FliteCharts®, and SafeTaxi® are registered trademarks of Garmin Ltd. or its subsidiaries. ESP™ is a trademark of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM Satellite Radio, Inc. October, 2010 190-00929-02 Rev. A Printed in the U.S.A. Warnings, Cautions & Notes WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. WARNING: The displayed minimum safe altitudes (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: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data Computer, or other altimeters in the aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only for weather avoidance, not penetration. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Warnings, Cautions & Notes Warning: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration. WARNING: The Garmin G1000, as installed in the Hawker Beechcraft 200/ B200 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: 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 Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft 200 and B200 King Air Airplane Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Warnings, Cautions & Notes WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp. WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. 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). 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. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings. CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Warnings, Cautions & Notes nOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. 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: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data. 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. 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: 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 G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Warnings, Cautions & Notes Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Record of Revisions Part Number 190-00929-00 190-00929-01 190-00929-02 Change Summary Initial release Added Synthetic Vision System Added TAWS-A Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Added other GDU 10.00 parameters Added GDU 11.12 changes Added GTS 820/850 Added Electronic Stabilization & Protection Iridium Telephone and Data Link Added Worldwide Weather Revision Date of Revision Affected Pages A October, 2010 All 190-00929-02 Rev. A Description Production release Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series RR-1 Record of Revisions Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A 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......................................................................................................................... 1 Change Navigation Sources.................................................................................................... 2 Enable/Disable OBS Mode While Navigating with GPS..................................................... 2 Generic Timer.............................................................................................................................. 2 Configure Vspeed Bugs Individually...................................................................................... 2 Turn Vspeed Bugs On or Off by Category............................................................................. 3 Set Barometric/Radar Altimeter Minimum Descent Altitude.......................................... 3 Testing the Radar Altimeter.................................................................................................... 3 Displaying Wind Data............................................................................................................... 3 Nav/Com/Transponder/Audio Panel......................................................................... 5 ADF Tuning (Optional)............................................................................................................... 5 DME Tuning................................................................................................................................. 5 Enter a Transponder Code....................................................................................................... 5 Activate ADS-B Transmit.......................................................................................................... 5 Selecting a COM Radio............................................................................................................. 5 Selecting a NAV Radio.............................................................................................................. 6 NAV/COM Tuning........................................................................................................................ 6 Intercom....................................................................................................................................... 6 Passenger Address (PA) System.............................................................................................. 7 Clearance Recorder and Player.............................................................................................. 7 Automatic Flight Control System............................................................................. 9 Flight Director Activation........................................................................................................ 9 Vertical Modes.......................................................................................................................... 10 Lateral Modes........................................................................................................................... 11 GPS Navigation......................................................................................................................... 13 Direct-to Navigation............................................................................................................... 13 Activate a Stored Flight Plan................................................................................................ 14 Activate a Flight Plan Leg...................................................................................................... 14 Stop Navigating a Flight Plan............................................................................................... 15 Vertical Navigation (VNAV)................................................................................................... 15 Flight Planning....................................................................................................................... 17 Weight Planning....................................................................................................................... 17 Trip Planning............................................................................................................................. 17 Create a New User Waypoint Defined by Latitude & Longitude.................................. 19 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series i Table of Contents Create a New User Waypoint Defined by Radials from Other Waypoints.................. 20 Create a New User Waypoint Defined by a Radial & Distance from Another Waypoint.............................................................................................................................. 22 Delete a User Waypoint.......................................................................................................... 23 Create a New Flight Plan....................................................................................................... 24 Import a Flight Plan from an SD Card................................................................................. 25 Insert a Waypoint in the Active Flight Plan....................................................................... 25 Enter an Airway in a Flight Plan........................................................................................... 26 Invert An Active Flight Plan................................................................................................... 27 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 27 Store a Flight Plan................................................................................................................... 27 Edit a Stored Flight Plan........................................................................................................ 28 Delete a Waypoint from the Flight Plan............................................................................. 28 Invert and Activate a Stored Flight Plan............................................................................ 28 Copy a Flight Plan.................................................................................................................... 29 Delete a Flight Plan................................................................................................................. 29 Graphical Flight Plan Creation.............................................................................................. 29 Export a Flight Plan to an SD Card...................................................................................... 30 Procedures................................................................................................................................. 31 Load and Activate a Departure Procedure........................................................................ 31 Activate A Departure Leg...................................................................................................... 31 Load An Arrival Procedure..................................................................................................... 31 Activate An Arrival Leg.......................................................................................................... 32 Load and/or Activate an Approach Procedure.................................................................. 32 Activate An Approach in the Active Flight Plan................................................................ 33 Activate a Vector to Final Approach Fix............................................................................. 33 Activate A Missed Approach in the Active Flight Plan.................................................... 33 Hazard Avoidance................................................................................................................. 35 Customizing the Hazard Displays on the Navigation Map............................................. 35 STORMSCOPE® (Optional)...................................................................................................... 35 XM Weather (Optional)........................................................................................................... 37 Worldwide Weather................................................................................................................. 38 Traffic Avoidance Systems..................................................................................................... 50 Terrain Awareness & Warning System................................................................................ 52 Airborne Color Weather Radar............................................................................................. 56 Additional Features............................................................................................................ 59 Synthetic Vision........................................................................................................................ 59 Terminal Procedure Charts.................................................................................................... 60 AOPA Airport Directory.......................................................................................................... 62 Satellite Telephone and Data Link Services...................................................................... 63 ii Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Table of Contents WI-FI Connections.................................................................................................................... 76 System Data Logging.............................................................................................................. 79 XM® Radio Entertainment..................................................................................................... 81 Electronic Stability & Protection (ESP™)............................................................................. 83 Annunciations & Alerts................................................................................................... 85 WARNING Annunciation......................................................................................................... 85 Advisory Annunciations......................................................................................................... 85 Message Advisory Alerts........................................................................................................ 85 Comparator Annunciations.................................................................................................... 86 Reversionary Sensor Annunciations.................................................................................... 86 AFCS Alerts................................................................................................................................ 87 TAWS-A Alerts........................................................................................................................... 88 TAWS-B Alerts........................................................................................................................... 91 Additional Aural Alerts........................................................................................................... 94 MFD & PFD Message Advisories........................................................................................... 95 Database Message Advisories.............................................................................................. 96 GMA 1347D Message Advisories.......................................................................................... 99 GIA 63W Message Advisories.............................................................................................. 100 GEA 71 Message Advisories................................................................................................. 103 GTX 33 Message Advisories................................................................................................. 104 GRS 77 Message Advisories................................................................................................. 104 GMU 44 Message Advisories............................................................................................... 106 GDL 59 Message Advisories................................................................................................. 106 GSR 56 Message Advisories................................................................................................. 107 GDL 69A Message Advisories.............................................................................................. 107 GWX 68 Alert Messages........................................................................................................ 107 GDC 74B Message Advisories.............................................................................................. 108 GCU 477 Message Advisories.............................................................................................. 108 GMC 710 Message Advisories............................................................................................. 109 Miscellaneous Message Advisories.................................................................................... 109 Flight Plan Import/Export Messages................................................................................. 113 Appendix...................................................................................................................................... 115 PFD Softkey Map................................................................................................................... 115 MFD Navigation Page Softkey Map.................................................................................. 120 Loading Updated Databases............................................................................................... 122 Index..........................................................................................................................................Index-1 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series iii Table of Contents Blank Page iv Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Instruments Flight Instruments Flight Instruments Selecting the Altimeter Barometric Pressure Setting Nav/Com/ XPDR/Audio Turn the BARO Knob to select the desired setting. Selecting Standard Barometric Pressure (29.92 in Hg) AFCS Push the BARO Knob to select standard pressure. Change Altimeter Barometric Pressure Setting Units 2) Press the ALT UNIT Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). Flight Planning Press the PFD Softkey to display the second-level softkeys. GPS Nav 1) Or: 4) Procedures Press the HPA Softkey to display the barometric pressure setting in hectopascals. Press the BACK Softkey to return to the top-level softkeys. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. Annun/Alerts Select the AUX-SYSTEM SETUP Page on the MFD. Additional Features 1) Hazard Avoidance Synchronizing the Altimeter Barometric Pressure Settings Synchronize CDI 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Select the AUX-SYSTEM SETUP Page on the MFD. Appendix 1) 1 Change Navigation Sources AFCS Nav/Com/ XPDR/Audio Flight Instruments Flight Instruments 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning. 3) Press the CDI Softkey a third time to return to GPS. Press the OBS Softkey to select OBS Mode. 2) Turn a CRS Knob to select the desired course to/from the waypoint. Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to disable OBS Mode. Additional Features 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. 2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted. 3) Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it will start counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window. Configure Vspeed Bugs Individually 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the desired Vspeed. 3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a Appendix Annun/Alerts 1) Generic Timer Hazard Avoidance Procedures Flight Planning GPS Nav Enable/Disable OBS Mode While Navigating with GPS Index speed has been changed from a default value, an asterisk appears next to the speed). 4) 2 Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Instruments Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or the TMR/REF Softkey. Flight Instruments 5) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired option. 4) Press the ENT Key. Press the TMR/REF Softkey to remove the window. AFCS 1) Nav/Com/ XPDR/Audio Turn Vspeed Bugs On or Off by Category GPS Nav Set Barometric/Radar Altimeter Minimum Descent Altitude 1) Press the TMR/REF Softkey. Turn the small FMS Knob clockwise to select BARO or RAD ALT. 4) Press the ENT Key. 5) Use the small FMS Knob to enter the desired altitude. 6) Press the ENT Key. 7) To remove the window, press the CLR Key or the TMR/REF Softkey. Hazard Avoidance 3) Procedures Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the right of ‘Minimums’. Flight Planning 2) Testing the Radar Altimeter 2) Select the RA TEST Softkey. ‘RA TEST’ is displayed to the left of the Radar Altitude window. The Radar Altitude window displays 50 feet, indicating a properly functioning system. 3) Selecting the RA TEST Softkey again, or exiting the System Status Page cancels the test. Annun/Alerts Select the AUX-SYSTEM STATUS Page on the MFD. Additional Features 1) Press the PFD Softkey. 2) Press the WIND Softkey to display wind data below the Selected Heading. 3) Press one of the OPTN softkeys to change how wind data is displayed. 4) To remove the Wind Data Window, press the OFF Softkey. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index 1) Appendix Displaying Wind Data 3 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Nav/Com/XPDR/Audio Panel Flight Instruments Nav/Com/Transponder/Audio Panel Nav/Com/ XPDR/Audio ADF Tuning (Optional) 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. GPS Nav Press the DME Softkey. AFCS 1) Press the XPDR Softkey to display the transponder mode selection softkeys. 2) 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. Procedures 1) Flight Planning Enter a Transponder Code Hazard Avoidance Additional Features Activate ADS-B Transmit Press the XPDR Softkey to display the transponder mode selection softkeys. 2) Press the ADS-B TX Softkey to enable transmission of three-dimensional aircraft position and aircraft heading. 3) Press the ADS-B TX Softkey again to disable transmission. Annun/Alerts 1) Appendix Selecting a COM Radio Transmit/Receive Index Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if installed) on the audio panel. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 5 Nav/Com/XPDR/Audio Panel Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the audio panel. Selecting a NAV Radio Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 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 Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Receive Only 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. 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Nav/Com/XPDR/Audio Panel Nav/Com/ XPDR/Audio 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 AFCS Flight Planning Procedures Hazard Avoidance 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. GPS Nav 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 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 7 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Nav/Com/XPDR/Audio Panel Blank Page 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A AFCS AFCS Note: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages. Nav/Com/ XPDR/Audio Note: If sensor information (other than attitude) required for a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. Flight Instruments Automatic Flight Control System Flight Director Activation Modes Selected Lateral Vertical AP Key Roll Hold (default) ROL Pitch Hold (default) PIT CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT GA Switch 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 VNV Key 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 VAPP LOC Pitch Hold (default) Glidepath Glideslope PIT GP GS HDG Key Heading Select HDG Pitch Hold (default) PIT Appendix PIT Annun/Alerts Pitch Hold (default) Additional Features ROL Hazard Avoidance Roll Hold (default) Procedures FD Key Flight Planning Control Pressed *Valid VNV flight plan must be entered before VNV Key press activates flight director. Index **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. ***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director. 190-00929-02 Rev. A GPS Nav 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 9 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments AFCS 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 Armed AFCS armed to capture the altitude displayed in the Selected Altitude window * 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 FLC nnn kt FLC M .nnn Flight Level Change, Maintains the current aircraft airspeed (in IAS or Mach) while the aircraft is climbing/ IAS Hold descending to the Selected Altitude. Press Flight Level Change, the SPD Key to switch between IAS and Mach Hold MACH. FLC Key VNAV Captures and tracks the VNAV flight path VNV Key VPTH VNAV Target Altitude Armed AFCS armed to capture the altitude displayed in the VNAV Target Altitude window ** ALTV Glidepath Captures and tracks the SBAS glidepath on approach Glideslope Captures and tracks the ILS glideslope on approach Takeoff (on ground) Disengages the autopilot and commands a constant pitch angle and wings level in the air on the ground in preparation for takeoff Go Around (in air) Level Disengages the autopilot and commands a constant pitch attitude and wings level in the air Commands 0° pitch attitude GP APR Key GS TO GA Switch GA Activated only by the ESP function LVL * ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A AFCS Lateral Mode Description Control Annunciation (default) ROL Low Bank Limits maximum commanded roll angle BANK Key * Heading Select Captures and tracks Selected Heading HDG Key HDG Navigation, GPS Arm/ Capture/Track NAV Key LOC Captures and tracks a localizer signal for backcourse approaches BC Key Approach, GPS Arm/Capture/ Track LOC Commands wings level attitude GA Switch GA LVL Index Activated only by the ESP function Appendix Disengages autopilot and commands a constant pitch angle and wings level in the air TO Annun/Alerts Disengages autopilot and commands a constant pitch angle and wings level in preparation for takeoff Additional Features Level Hazard Avoidance VAPP APR Key Track (Glideslope Mode automatically armed) Go Around (in air) BC GPS Approach, VOR Arm/Capture/ Track Captures and tracks selected Approach, ILS Arm/Capture/ navigation source (GPS, VOR, LOC) Takeoff (on ground) VOR Procedures Backcourse Arm/Capture/ Track Captures and tracks selected navigation source (GPS, VOR, LOC) Flight Planning Navigation, LOC Arm/ Capture/Track (No Glideslope) GPS GPS Nav Navigation, VOR Enroute Arm/Capture/Track AFCS Holds current aircraft roll attitude or rolls wings level, depending on commanded bank angle Nav/Com/ XPDR/Audio Roll Hold Flight Instruments Lateral Modes * 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. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 11 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments AFCS Blank Page 12 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A GPS Navigation Flight Instruments GPS Navigation Direct-to Navigation 1) 3) 5) 7) 9) 11) Direct-to Navigation from the PFD 2) 3) 5) 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 13 Index 6) ) on the PFD. Turn the large FMS Knob to place the cursor in the desired selection field. Turn the small FMS Knob to begin selecting the desired identifier, location, etc. Press the ENT Key. The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 6. Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field. Appendix 4) Press the Direct-to Key ( Annun/Alerts 1) Additional Features 12) Hazard Avoidance 10) Procedures 8) Flight Planning 6) GPS Nav 4) ) Key on the Control Unit. Enter the waypoint identifier. Press the ENT Key to confirm the identifier. The ‘Activate?’ field is highlighted. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 5. Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. Enter the desired altitude. Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9. Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. Press the ENT Key. The cursor is now flashing in the VNV offset distance field. Enter the desired offset distance before (-) or after (+) the waypoint. Press the ENT Key. The ‘Activate?’ field is highlighted. Press the ENT Key to activate. AFCS 2) Press the Direct-to ( Nav/Com/ XPDR/Audio Direct-to Navigation from the MFD Nav/Com/ XPDR/Audio Flight Instruments GPS Navigation 7) Turn the small FMS Knob to enter the desired altitude. 8) Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 10. 9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance field. AFCS 11) Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct-to. 13) Turn the small FMS Knob to enter the desired course to the waypoint. 14) Press the ENT Key to highlight ‘ACTIVATE?’. 15) Press the ENT again to activate the Direct-to. Activate a Stored Flight Plan 1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan 4) Select the ACTIVE Softkey. The confirmation window is now displayed. 5) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav 12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘CRS’ field. Appendix Annun/Alerts Activate a Flight Plan Leg 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint. 2) Select the ACT LEG Softkey. or Index Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD. 3) 14 With ‘Activate’ highlighted, press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A GPS Navigation Press the FPL Key on the Control Unit to display the Active Flight Plan Page. 2) Press the MENU Key to display the Page Menu Window. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan. AFCS Vertical Navigation (VNAV) Nav/Com/ XPDR/Audio 1) Flight Instruments Stop Navigating a Flight Plan GPS Nav The navigation database only contains altitudes for procedures that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the database. In this case the altitude may be entered manually. Flight Planning Procedures Large White Text Large Light Blue Text Hazard Avoidance Small Light Blue Text Additional Features Small Light Blue Subdued Text Small White Text with Altitude Restriction Bar Annun/Alerts Cross AT or ABOVE 5,000 ft Appendix Cross AT 2,300 ft 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Cross AT or BELOW 3,000 ft 15 Altitudes associated with arrival and approach procedures are “auto-designated”. This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF. Note that these altitudes will be displayed as small light blue text. Altitudes that have been designated for use in vertical navigation may also be made “non-designated” by placing the cursor over the desired altitude and pressing the CLR Key. The altitude is now displayed only as a reference. It will not be used to give flight path vertical guidance. Other displayed altitudes may change due to re-calculations or rendered invalid as a result of manually changing an altitude to a non-designated altitude. White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical flight path guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. The system cannot use this altitude in determining vertical flight path guidance. Small Text Altitude is not designated to be used in determining vertical flight path guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Altitude is designated for use in giving vertical flight path guidance. Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical flight path guidance. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments GPS Navigation 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning Flight Instruments Flight Planning Weight Planning Nav/Com/ XPDR/Audio All procedures apply to the MFD and the Control Unit unless otherwise stated. Entering Weight Parameters 3) Turn the small FMS Knob to enter the desired fuel quantity. 4) Press the ENT Key. The cursor is now in the ‘Fuel Reserves’ field. 5) Turn the small FMS Knob to enter the desired reserve fuel quantity. 6) Press the FMS Knob to remove the cursor. 7) Press the ENT Key. Additional Features Turn the large FMS Knob to place the cursor in the ‘Fuel On Board’ field. Annun/Alerts Trip Planning 2) Turn the small FMS Knob to select the Trip Planning Page. 3) The current ‘page mode’ is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL Softkey. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 17 Index Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page group. Appendix 1) 190-00929-02 Rev. A Hazard Avoidance 2) Procedures Press the FMS Knob to activate the cursor. Flight Planning 1) GPS Nav Entering Fuel Parameters AFCS The Weight Planning Page is displayed after system power-up. If it is necessary to return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the small FMS Knob to select the Weight Planning Pge. 1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field. 2) Enter the desired aircraft empty weight. 3) Press the ENT Key. The cursor is now over the ‘Pilot & Stores’ field. 4) Enter the desired weight of Pilot & Stores. 5) Press the ENT Key. 6) Continue repeating these steps until all desired weights have been entered. Flight Planning Flight Instruments 4) For Direct-to planning: a) Select the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). Nav/Com/ XPDR/Audio b) If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. c) Press the ENT Key and the flashing cursor moves to the ending waypoint field. AFCS d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. GPS Nav Or: For point-to-point planning: a) Enter the identifier of the starting waypoint. Flight Planning b) Once the waypoint’s identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint. c) Again, enter the identifier of the ending waypoint. Procedures d) Press the ENT Key to accept the waypoint. Or: For flight plan leg planning: Hazard Avoidance a) Select the FPL Softkey (at the bottom of the display). b) Turn the small FMS Knob to select the desired flight plan (already stored in memory), by number. Additional Features c) Turn the large FMS Knob to highlight the ‘LEG’ field. Annun/Alerts d) Turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ will display the active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan. Appendix NOTE: The page mode must be set to ‘MANUAL’ to perform the following steps. 5) Turn the large FMS Knob to highlight the departure time (DEP TIME) field. Index NOTE: The departure time on the Trip Planning Page is used for preflight planning. Refer to the Utility Page for the actual flight departure time. 18 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning 8) The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press the ENT Key when finished. Note that in ‘automatic’ page mode, fuel flow is provided by the system. 9) The flashing cursor moves to the fuel onboard field. Modify the fuel onboard. Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is provided by the entry made on the Weight Planning Page. 11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the altitude. Press the ENT Key when finished. Note that in ‘automatic’ page mode, altitude is provided by the system. Hazard Avoidance Additional Features 13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter the desired air temperature. Press the ENT Key when finished. Note that in ‘automatic’ page mode, air temperature is provided by the system outside air temperature. Procedures 12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter the desired baro setting. Press the ENT Key when finished. Note that in ‘automatic’ page mode, the baro setting is provided by the setting entered on the PFD. Flight Planning 10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field. Enter the calibrated airspeed. Press the ENT Key when finished. Note that in ‘automatic’ page mode, calibrated airspeed is provided by the system. GPS Nav The flashing cursor moves to the ground speed (GS) field. Enter the ground speed. Press the ENT Key when finished. Note that in ‘automatic’ page mode, ground speed is provided by the system. AFCS 7) Nav/Com/ XPDR/Audio Enter the departure time. Press the ENT Key when finished. Departure time may be entered in local or UTC time, depending upon system settings. Flight Instruments 6) Create a New User Waypoint Defined by Latitude & Longitude 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Select the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index 190-00929-02 Rev. A Appendix Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group. Annun/Alerts 1) 19 Flight Planning Flight Instruments a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. 7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select LAT/LON (latitude and longitude). 9) Press the ENT Key. Create a New User Waypoint Defined by Radials from Other Waypoints 1) Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Select the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. 7) Annun/Alerts With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select RAD/RAD (radial/radial). 9) Press the ENT Key. Appendix Additional Features b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: Index a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. 20 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning Flight Instruments b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Or: b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position. Nav/Com/ XPDR/Audio a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. AFCS c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. Flight Planning b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. GPS Nav Or: c) Turn the large FMS Knob to select the desired waypoint. Procedures d) Press the ENT Key. Or: b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. Hazard Avoidance a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. c) Turn the large FMS Knob to select the desired waypoint. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. Annun/Alerts 12) Press the ENT Key. Additional Features d) Press the ENT Key. 13) Repeat step 10 to enter the next waypoint name. 15) Press the ENT Key. Appendix 14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the second waypoint. Enter the desired radial from the reference waypoint. 16) Press the FMS Knob to remove the flashing cursor. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 21 Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Select the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. GPS Nav 1) Nav/Com/ XPDR/Audio Create a New User Waypoint Defined by a Radial & Distance from Another Waypoint AFCS Flight Instruments Flight Planning Flight Planning a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. Hazard Avoidance Procedures b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. 7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select RAD/DIS (radial/distance). 9) Press the ENT Key. Additional Features 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: Annun/Alerts a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Or: Appendix a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. Index b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. 22 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. Nav/Com/ XPDR/Audio b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. Flight Instruments Or: c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. AFCS Or: b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. GPS Nav a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. c) Turn the large FMS Knob to select the desired waypoint. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. Procedures 12) Press the ENT Key. 13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired distance from the reference waypoint. Hazard Avoidance 14) Press the ENT Key. 15) Press the FMS Knob to remove the flashing cursor. Additional Features Delete a User Waypoint 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’ field. 5) Turn the small FMS Knob to highlight the desired waypoint. 6) Select the DELETE Softkey. 7) The message ‘Would you like to delete the user waypoint?’ is displayed. With ‘YES’ highlighted, press the ENT Key. 23 Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix Turn the large FMS Knob to select the ‘WPT’ page group. Annun/Alerts 1) 190-00929-02 Rev. A Flight Planning d) Press the ENT Key. Create a New Flight Plan NOTE: When creating a new flight plan in the Active Flight Plan Window, the first leg is activated automatically after it is created. Nav/Com/ XPDR/Audio Flight Instruments Flight Planning Procedures Flight Planning GPS Nav AFCS Creating an active flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (only on MFD). 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. The active flight plan is modified as each waypoint is entered. 5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint. 6) When all waypoints have been entered, press the FMS Knob to remove the cursor. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Creating a stored flight plan: 1) Press the FPL Key. 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to display a blank flight plan for the first empty storage location. 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 departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. 6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint. 7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list. 24 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning 2) Press the FPL Key on the Control Unit 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) Select the IMPORT Softkey. AFCS Insert the SD card containing the flight plan in the top card slot on the MFD. Nav/Com/ XPDR/Audio 1) Flight Instruments Import a Flight Plan from an SD Card GPS Nav If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed. Or: 8) Press the ENT Key. Hazard Avoidance Turn the small FMS Knob to highlight the desired flight plan for importing. Procedures 7) Flight Planning 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 select the IMPORT Softkey. Insert a Waypoint in the Active Flight Plan Additional Features 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The new waypoint will be inserted before the highlighted waypoint. 4) Turn the small FMS Knob. The Waypoint Information Window is now displayed. 5) Enter the new flight plan waypoint by one of the following: Appendix Press the FPL Key on the Control Unit to display the active flight plan. Annun/Alerts 1) a) Enter the user waypoint identifier, facility, or city. Index b) Press the ENT Key. Or: 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 25 Flight Planning Flight Instruments a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. Nav/Com/ XPDR/Audio b) Turn the small FMS Knob to the right to display the ‘NRST’ airport waypoints to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. AFCS Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Enter an Airway in a Flight Plan 1) Press the FPL Key on the Control Unit. 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 select the LD AIRWY Softkey, or press the MENU Key and select “Load Airway”(required on the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when an acceptable 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. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. 26 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning 2) Press the MENU Key to display the Page Menu. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’. 4) Press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location. 5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan. AFCS Press the FPL Key to display the active flight plan. Nav/Com/ XPDR/Audio 1) Flight Instruments Invert An Active Flight Plan 1) Press the FPL Key on the Control Unit to display the active flight plan. Press the FMS Knob to activate the cursor. Flight Planning Or: GPS Nav Remove a Departure, Arrival, Approach, or Airway from a Flight Plan a) Turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. Procedures c) Turn the large FMS Knob to highlight the desired flight plan. d) Select the EDIT Softkey. 3) Press the CLR Key to display a confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway. After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. Appendix 1) Annun/Alerts Store a Flight Plan Additional Features Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted. Titles appear in white directly above the procedure’s waypoints. Hazard Avoidance 2) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 27 Edit a Stored Flight Plan 1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan. 4) Select the EDIT Softkey. 5) Turn the large FMS Knob to place the cursor in the desired location. 6) Enter the changes, then press the ENT Key. 7) Press the FMS Knob to return to the Flight Plan Catalog Page. Delete a Waypoint from the Flight Plan 1) Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Flight Planning Or: Procedures a) Turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. c) Turn the large FMS Knob to highlight the desired flight plan. Annun/Alerts Additional Features Hazard Avoidance d) Select the EDIT Softkey. 2) Turn the large FMS Knob to highlight the waypoint to be deleted. 3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 5) Once all changes have been made, press the FMS Knob to remove the cursor. Invert and Activate a Stored Flight Plan Index Appendix Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor. 28 1) Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Flight Planning 5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be displayed. 6) With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now inverted and activated. The original flight plan remains intact in its flight plan catalog storage location. AFCS Copy a Flight Plan Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the flight plan to be copied. 5) Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. GPS Nav 1) 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the flight plan to be deleted. 5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. Hazard Avoidance Press the FPL Key on the Control Unit. Press the Joystick to activate the map pointer. Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan. 29 Index 2) Appendix Press the FPL Key on the Control Unit to display the Active Flight Plan Page. Annun/Alerts 1) Additional Features Graphical Flight Plan Creation Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Procedures 1) Flight Planning Delete a Flight Plan 190-00929-02 Rev. A Nav/Com/ XPDR/Audio Turn the large FMS Knob to highlight the desired flight plan. Flight Instruments 4) AFCS Nav/Com/ XPDR/Audio Flight Instruments Flight Planning 3) The default insertion point is at the end of the flight plan. If the selected waypoint is to be placed anywhere other than the end of the flight plan, press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE the cursor. Turn the large FMS Knob to select the desired insertion point. 4) Select the LD WPT Softkey. The selected waypoint will be inserted at the selected point. The default user waypoint naming is USR000, USR001, USR002, and so on. 5) To change the user waypoint name, follow the procedure for modifying a user waypoint. 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key on the Contol Unit 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) Select the EXPORT Softkey. 7) Press the ENT Key to confirm the export. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav Export a Flight Plan to an SD Card 30 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Procedures Flight Instruments Procedures Load and Activate a Departure Procedure Nav/Com/ XPDR/Audio Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a list of available departures. 4) Turn the large FMS Knob to highlight the desired departure. 5) Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway. 6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a list of available transitions. 7) Turn the large FMS Knob to highlight the desired transition. 8) Press the ENT Key. 9) With ‘LOAD?’ highlighted, press the ENT Key. The departure will be active when the flight plan is active. Flight Planning 2) GPS Nav Press the PROC Key. AFCS 1) Procedures Activate A Departure Leg Hazard Avoidance 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure. 4) Select the ACT LEG Softkey. A confirmation window showing the selected leg will be displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. Annun/Alerts Press the FPL Key to display the active flight plan. Additional Features 1) Load An Arrival Procedure Appendix Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’. 3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list of available arrivals. 4) Turn the large FMS Knob to highlight the desired arrival. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 31 Index 1) Nav/Com/ XPDR/Audio Flight Instruments Procedures 5) Press the ENT Key. A list of transitions is displayed for the selected arrival. 6) Turn either FMS Knob to select the desired transition. 7) Press the ENT Key. A list of runways is displayed for the selected arrival. 8) Turn the large FMS Knob to highlight the desired runway. 9) Press the ENT Key. 10) With ‘LOAD?’ highlighted, press the ENT Key. AFCS 11) The arrival will become part of the active flight plan. 1) Press the FPL Key on the Control Unit to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival. 4) Select the ACT LEG Softkey. A confirmation window showing the selected leg is displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. Load and/or Activate an Approach Procedure Hazard Avoidance Procedures Flight Planning GPS Nav Activate An Arrival Leg Index Appendix Annun/Alerts Additional Features NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. 32 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. A list of available approaches for the destination airport is displayed. 4) Turn either FMS Knob to highlight the desired approach. 5) Press the ENT Key. A list of available transitions for the selected approach procedure is now displayed. 6) Turn either FMS Knob to select the desired transition. The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Procedures 8) If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO. 9) Press the ENT Key. The cursor moves to the altitude field. Turn the small FMS Knob to enter the published DA/MDA for the selected approach procedure. Nav/Com/ XPDR/Audio Press the ENT Key. The cursor moves to the MINIMUMS field. Flight Instruments 7) AFCS 10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’ highlighted. 11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’. Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’. 3) Press the ENT Key. Hazard Avoidance 1) Procedures Activate An Approach in the Active Flight Plan Activate a Vector to Final Approach Fix 2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’. 3) Press the ENT Key. 4) The final approach course becomes the active leg. Annun/Alerts Press the PROC Key. Additional Features 1) Activate A Missed Approach in the Active Flight Plan Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A confirmation window will be displayed. Appendix 1) Flight Planning 12) Press the ENT Key. GPS Nav Selecting ‘LOAD?’ enters the selected approach procedure into the active flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the selected approach procedure into the active flight plan and is immediately activated. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 33 Procedures Flight Instruments 4) With ‘ACTIVATE’ highlighted, press the ENT Key. Or: Press the go-around button. After activating the missed approach procedure, and the CDI has changed to TERM mode sensitivity, another approach procedure may be loaded. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio 5) 34 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Flight Instruments Hazard Avoidance Customizing the Hazard Displays on the Navigation Map 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. Nav/Com/ XPDR/Audio 1) GPS Nav Procedures Displaying Stormscope Lightning Data on the Navigation Map Page Select the MAP Softkey. 2) Select the STRMSCP Softkey. Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page. Hazard Avoidance 1) Symbol Additional Features Strike is between 6 and 60 seconds old Annun/Alerts Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Press the MENU Key (with the Navigation Map Page displayed). 2) Turn either FMS Knob to highlight ‘Map Setup’. 3) Press the ENT Key. 4) Turn the small FMS Knob to highlight ‘Weather’. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index 1) Appendix Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode 190-00929-02 Rev. A Flight Planning WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation. Lightning Age Strike is less than 6 seconds old AFCS STORMSCOPE® (Optional) 35 Nav/Com/ XPDR/Audio Flight Instruments Hazard Avoidance 5) Press the ENT Key. 6) Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field. 7) Turn the small FMS Knob to display the ‘Cell/Strike’ window. 8) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key. 9) Push the FMS Knob to return to the Navigation Map Page. 1) Press the MENU Key (with the Navigation Map Page displayed). 2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field and press the ENT Key. GPS Nav AFCS Clear Stormscope Lightning Data from the Navigation Map Page NOTE: If heading input is lost, strikes and/or cells must be cleared manually Flight Planning after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. Procedures Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob select the Stormscope Page. 1) Select the Stormscope Page. 2) Select the MODE Softkey. The CELL and STRIKE Softkeys are displayed. Select the CELL Softkey to display ‘CELL’ data or select 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. Additional Features Hazard Avoidance Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’ Annun/Alerts NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells. Index Appendix Change the Viewing Mode Between 360˚ and 120˚ 1) Select the Stormscope Page. 2) Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to display a 120˚ viewing area. Select the CLEAR Softkey to remove all Stormscope lightning data from the display. 36 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Displaying XM Weather on the Navigation Map Page 2) Select the NEXRAD or XM LTNG Softkey to display the desired weather. Select the applicable softkey again to remove weather data from the Navigation Map Page. GPS Nav Select the MAP Softkey. AFCS 1) Display METAR and TAF information on the Airport Information Page Turn the large FMS Knob to select the WPT Page Group. 2) Turn the small FMS Knob to select the Airport Information Page. 3) Select the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). Flight Planning 1) Procedures Displaying Weather on the Weather Data Link Page 2) Turn the small FMS Knob to select the Weather Data Link Page. 3) Select the available softkeys to select the desired XM weather product. 4) Select the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Key to return to the map. Map Panning Information – Weather Data Link Page 2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs. 3) Press the ENT Key to display pertinent information for the selected product. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report. Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport’s Information Page to display the text of the report. Pressing the ENT Key when panning over a TFR displays TFR specific information. Appendix Push in the Joystick to display the panning arrow. Annun/Alerts 1) Additional Features Turn the large FMS Knob to select the Map Page Group. Hazard Avoidance 1) 190-00929-02 Rev. A Nav/Com/ XPDR/Audio WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. Flight Instruments XM Weather (Optional) 37 Hazard Avoidance Flight Instruments Weather Products and Symbols Nav/Com/ XPDR/Audio Echo Top (Cloud Top and Echo Top Mutually Exclusive) Cyclone Warnings City Forecast AIREPs Cell Movement Icing Potential Freezing Levels Procedures PIREPs NEXRAD XM Lightning Cloud Top METARs Surface Analysis SIGMETs/AIRMETs County Warnings Winds Aloft Worldwide Weather Note: Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather. Do not utilize Worldwide Weather information to penetrate hazardous weather. Flight Planning GPS Nav AFCS Turbulence Weather data are provided when the pilot initiates either a manual or automatic GFDS data request on the GFDS Weather Data Link Page on the MFD. No weather data is displayed until the first GFDS Weather Data Request is made. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Accessing GFDS Worldwide Weather Products 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the GFDS Weather Data Link Page. When a weather product is selected for display on the GFDS Weather Data Link 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 Refresh 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 GFDS 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. 38 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Symbol U.S./Canada: 3* Europe: 15 60 30 30 Continuous 60 Continuous 90 Continuous 60 Continuous 90 Continuous 60 Continuous 60 Continuous AFCS 30 Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Radar Precipitation (PRECIP) Infrared Satellite (IR SAT) Datalink Lightning (DL LTNG) SIGMETs/AIRMETs (SIG/AIR) Meteorological Aerodrome Report (METARs) Winds Aloft (WIND) Pilot Weather Report (PIREPs) Temporary Flight Restrictions no product image (TFRs) Terminal Aerodrome Reports no product image (TAFs) Refresh Rate (Minutes) Flight Instruments Weather Product Expiration Time (Minutes) Additional Features * The composite precipitation image is updated every 3 minutes, but individual radar sites may take between 3 and 10 minutes to provide new data. Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 39 Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Setting Up and Customizing the GFDS Weather Data Link Page 1) Select the GFDS Weather Data Link 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, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the GFDS Weather Data Link Page with the changed settings. On aircraft equipped with both GFDS and XM weather services, customizing the display settings for the corresponding weather products shown in following table will result in identical settings for both services. GFDS Worldwide Weather Product Precipitation Next-generation Radar (NEXRAD) (PRECIP) Cloud Top Infrared Satellite (CLD TOP) (IR SAT) XM Lightning GFDS Lightning (DL LTNG) (XM LTNG) SIGMETs/AIRMETs SIGMETs/AIRMETs (SIG/AIR) (SIG/AIR) Meteorological Aerodrome Report Meteorological Aerodrome Report (METARs) (METARs) Winds Aloft Winds Aloft (WIND) (WIND) Pilot Weather Report Pilot Weather Report (PIREPs) (PIREPs) Index Appendix Annun/Alerts Additional Features Hazard Avoidance XM Weather Product 40 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance 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. AFCS Select the GFDS Weather Data Link Page. Nav/Com/ XPDR/Audio 1) Flight Instruments Restoring Default GFDS Weather Data Link Page Settings Switching Between GFDS and XM Weather Sources Turn the large FMS Knob on the MFD to select the MAP page group. 2) Turn the small FMS Knob to select the GFDS (or XM) Weather Data Link Page. 3) Press the MENU Key. 4) Turn the large FMS Knob to select ‘Display GFDS Weather’ or ‘Display XM’ Weather’ (choice dependent on current weather source) and press the ENT Key. GPS Nav 1) 2) Select the LEGEND Softkey to display the legends for the displayed weather products. Hazard Avoidance Select the GFDS Weather Data Link Page. Additional Features Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT 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, select the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. Appendix Setting Up and Customizing Weather Data for the Navigation Map Page 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Select the Navigation Map Page. Annun/Alerts 3) 1) Procedures 1) Flight Planning Viewing Legends for Displayed GFDS Weather Products 41 Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Hazard Avoidance 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. GFDS Weather Data Requests The GFDS 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 GFDS data request process. Hazard Avoidance Procedures Requesting GFDS Weather Data Manually 1) Select the GFDS Weather Data Link Page. 2) Press the MENU Key. 3) With ‘GFDS Weather 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 check or uncheck one of more of the following coverage selections: Additional Features • PRESENT POSITION – Requests data based on current location. Annun/Alerts • DESTINATION – Requests data based on active flight plan destination (if the flight plan contains no destination, dashes ‘------” are displayed.) Appendix • FPL – Requests data based on active flight plan. Turn the small FMS Knob to select the desired flight plan look-ahead distance option (or choose ‘REMAINING FPL’ to request the remainder of the flight plan). • WAYPOINT – Requests data based on any valid waypoint. Index 5) 42 Turn the large FMS Knob highlight to the ‘DIAMETER / RTE 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted. Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the GFDS Data Link Page without requesting data. Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning During a GFDS Data Request, the Request Status box displays “Processing...” and the ‘CANCEL REQ’ button is highlighted. If desired, the GFDS Data Request window may be closed while the data request is processing by pressing the FMS Knob; the data request will continue in the background. GFDS Data Requests typically take between 1 to 3 minutes to complete depending on the size of the selected weather coverage area. The G1000 retrieves all available Worldwide Weather products within the selected coverage area during an initial GFDS Data Request, regardless of which products (if any) are currently enabled for display. On subsequent requests, previously retrieved textual data (such as METARs and TAFS) is retained if it has not expired, while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request. Flight Instruments 6) Cancelling a GFDS Weather Data Request in Progress 2) Press the MENU Key. 3) With ‘GFDS Data Request’ highlighted, press the ENT Key. 4) Turn the large FMS Knob to select ‘CANCEL REQ’ and press the ENT Key. The request status box indicates ‘Request Cancelled’. 5) Press the FMS Knob to return to the GFDS Weather Datalink Page. Hazard Avoidance Select the GFDS Weather Data Link Page. Procedures 1) Additional Features Enabling Automatic GFDS Data Requests Select the GFDS Weather Data Link Page. 2) Press the MENU Key. 3) With ‘GFDS Weather Request’ highlighted, press the ENT Key. 4) Choose the desired weather coverage options. 5) Turn the large FMS Knob to select the ‘UPDATE RATE’ setting. Then turn the small FMS Knob to highlight the desired automatic update frequency (OFF, 5 Min, 10 Min, 15 Min, 20 Min, 25 Min, 30 Min, 45 Min, or 60 Min), then press the ENT Key. 43 Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix 190-00929-02 Rev. A Annun/Alerts 1) Hazard Avoidance Flight Instruments 6) The ‘SEND REQ” button is highlighted and a countdown timer is displayed in the ‘REQUEST STATUS’ based on the currently selected update rate. Press the ENT Key to immediately send an immediate GFDS Data Request. Nav/Com/ XPDR/Audio Or: Press the FMS Knob to return to the GFDS Weather Data Link Page. Worldwide Weather Products AFCS Precipitation Precipitation data is not real-time. The lapsed time between collection, processing, and dissemination of radar images can be significant and may not reflect the current radar synopsis. Due to the inherent delays and the relative age of the data, it should be used for long-range planning purposes only. Displaying Precipitation Weather Information 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the GFDS Weather Data Link Page. 2) Select the PRECIP Softkey. Radar data shown represents lowest level, base reflectivity, of radar returns. The display of the information is color-coded to indicate the weather severity level. All weather product legends can be viewed on the GFDS Weather Data Link Page. For the Precipitation legend, select the LEGEND Softkey when Precipitation is selected for display. Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav NOTE: Precipitation data cannot be displayed at the same time as terrain. No Radar Coverage Index Boundary of weather data request Precipitation Data Legend 44 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Displaying Cloud Tops information 1) Select the GFDS Weather Data Link Page. 2) Select the IR SAT Softkey. Nav/Com/ XPDR/Audio Infrared Satellite Infrared Satellite (IR SAT) data depicts cloud top temperatures from satellite imagery. Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes. Flight Instruments Precipitation Limitations Radar images may have certain limitations: • Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet hail, and rain. • Radar base reflectivity is sampled at the minimum antenna elevation angle. An individual radar site cannot depict high altitude storms at close ranges. It has no information about storms directly over the site. • When zoomed in to a range of 30 nm, each square block on the display represents an area of four square kilometers. The following may cause abnormalities in displayed radar images: • Ground clutter • Strobes and spurious radar data • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows • Metallic dust from military aircraft, which can cause alterations in radar scans Annun/Alerts Appendix Datalink Lightning Lightning data shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. Neither cloud-to-cloud nor the exact location of the lightning strike is displayed. If the aircraft is also equipped with the L-3 WX-500 Stormscope®, only one lightning product may be enabled for display at a time. Additional Features To display the Infrared Satellite legend, select the LEGEND Softkey when Infrared Satellite data is selected for display. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 45 Hazard Avoidance To display the Datalink Lightning legend on the Weather Data Link Page, select the LEGEND Softkey when Datalink Lightning is selected for display. SIGMETs and AIRMETs SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information) are issued for potentially hazardous weather. A Convective SIGMET is issued for hazardous convective weather such as severe or widespread thunderstorms. A localized SIGMET can be displayed when significant weather conditions are not widespread. The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the GFDS data request. Displaying SIGMETs and AIRMETs 1) Select the GFDS Weather Data Link Page. 2) Select the SIG/AIR Softkey. 3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon. 4) Press the ENT key. To display the SIGMET and AIRMET legend, select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Displaying Datalink Lightning information 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the GFDS Weather Data Link Page. 2) Select the DL LTNG Softkey. Index SIGMET/AIRMET Legend 46 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note that the METAR text must be completely scrolled through before scrolling through the TAF text. 47 Index Use the FMS Knob to enter the desired airport and press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Flight Planning 3) 190-00929-02 Rev. A GPS Nav Displaying METAR and TAF text 1) On the GFDS Weather Data Link Page, select the METAR Softkey. 2) Press the RANGE Knob and pan to the desired airport. 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text. 5) Press the FMS Knob or the CLR Key to return to the GFDS Weather Data Link Page. Or: 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Select the WX Softkey to select the Weather Information Page. 2) Press the FMS Knob to display the cursor. AFCS METARs (METeorological Aerodrome Reports) typically contain information about the temperature, dewpoint, wind, precipitation, cloud cover, cloud heights, visibility, and barometric pressure at an airport or observation station. They can also contain information on precipitation amounts, lightning, and other critical data. METARs reflect hourly observations; non-routine updates include the code “SPECI” in the report. METARs are shown as colored flags at airports that provide them. TAFs (Terminal Aerodrome Forecasts) are weather predictions for specific airports within a 24- hour period, and may span up to 36 hours. TAFs typically include forecast wind, visibility, weather phenomena, and sky conditions using METAR codes. METAR and TAF text are displayed on the Weather Information Page. TAF information is displayed in its raw form when it is available. Nav/Com/ XPDR/Audio Note: METAR information is only displayed within the installed aviation database service area. Flight Instruments METARs and TAFs To display the METAR legend on the GFDS Weather Data Link Page, select the LEGEND Softkey when METARs are selected for display. Nav/Com/ XPDR/Audio Flight Instruments Hazard Avoidance Winds Aloft Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000 feet MSL. Displaying Winds Aloft data 1) Select the GFDS Weather Data Link Page. 2) Select the MORE WX Softkey. 3) Select the WIND Softkey. 4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected. To display the Winds Aloft legend, select the LEGEND Softkey when Winds Aloft is selected for display. Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS METAR Legend Index Winds Aloft Data with Legend 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Nav/Com/ XPDR/Audio AFCS Displaying PIREP text 1) Select the GFDS Weather Data Link Page. 2) Select the MORE WX Softkey. 3) Select the PIREPS Softkey. 4) Press the RANGE Knob and pan to the desired weather report. A gray circle will appear around the weather report when it is selected. 5) Press the ENT Key. The PIREP tex is first displayed in a decoded fashion, then as raw text. 6) Use the FMS Knob or the ENT Key to scroll through the PIREP text. 7) Press the FMS Knob or the CLR Key to close the PIREP text window and return to the GFDS Weather Data Link Page. Flight Instruments PIREPs Pilot Weather Reports (PIREPs) describe in-flight weather encountered by pilots. A PIREP may contain unforecast adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, turbulence, and type of aircraft flown. PIREPs are issued as either Routine (UA) or Urgent (UUA). GPS Nav Flight Planning Hazard Avoidance The PIREP color is determined by the type (routine or urgent). Procedures To display the PIREP or AIREP legend, select the LEGEND Softkey when PIREPs or AIREPs are selected for display. Additional Features AIREPs & PIREPs Legend Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 49 Traffic Avoidance Systems • If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and TNA MUTE Softkey will be displayed. • If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE or NORMAL, TEST, and ALT MODE Softkey will be displayed. Nav/Com/ XPDR/Audio Flight Instruments Hazard Avoidance Traffic Symbol Description AFCS Non-Threat Traffic (intruder is beyond 5 nm and greater than 1200’ vertical separation) GPS Nav Proximity Advisory (PA)(TAS only, not available with TIS) (intruder is within 5 nm and less than 1200’ vertical separation) Flight Planning Traffic Advisory (TA) (closing rate, distance, and vertical separation meet TA criteria) Traffic Advisory Off Scale Procedures Traffic Symbol Description Traffic Information Service (TIS) Hazard Avoidance NOTE: If the G1000 is configured to use an optional Traffic Advisory System (TAS), TIS is not available for use. Additional Features NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. Index Appendix Annun/Alerts Displaying Traffic on the Traffic Map Page 50 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) Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic Mode field. 4) Select the STANDBY Softkey to place the system in the Standby Mode. ‘STANDBY’ will be displayed in the Traffic Mode field. 5) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area. 6) Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural alert. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Ensure TIS is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map. Nav/Com/ XPDR/Audio 1) Flight Instruments Displaying Traffic on the Navigation Map Traffic Advisory System (TAS) (Optional) AFCS System Self Test Select the STANDBY Softkey. 3) Select the TEST Softkey. 4) Self test will take approximately eight seconds to complete. When completed successfully, traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed (see Annuciations & Alerts section). If the self test fails, the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed. 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 second rectangular page icon. 3) Select the OPERATE or NORMAL Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic Mode field. 4) Select the ALT MODE Softkey to change the altitude display volume. Select the desired altitude volume by selecting the BELOW, NORMAL, ABOVE, or UNREST (unrestricted) Softkey. The selection is displayed in the Altitude Mode field. 5) Select the STANDBY Softkey to place the system in the Standby Mode. ‘STANDBY’ will be displayed in the Traffic Mode field. 6) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area. 7) Select the FLT ID Softkey (GTS 820/850 only) to enable or disable Flight ID displayed with the intruder information. Hazard Avoidance 1) Procedures 2) Flight Planning Set the range to 2/6 nm. GPS Nav 1) Additional Features Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 51 Hazard Avoidance Nav/Com/ XPDR/Audio Flight Instruments Displaying Traffic on the Navigation Map 1) With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map. Terrain Awareness & Warning System AFCS TAWS-A (Optional) GPS Nav WARNING: The TAWS display shows supplemental information only. It should not be used for navigation. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Flight Planning NOTE: TAWS operation is only available when the system is configured for a TAWS-A installation. Hazard Avoidance Procedures Manual System Test 1) While the TAWS-A Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS System’. 3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS-A Page. Additional Features When all is in working order, “TAWS System Test, OK” is heard. 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS-A Page. 3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Select the 360 Softkey to return to the 360° default display. 4) Rotate the Joystick clockwise to increase the display range or rotate counter-clockwise to decrease the display range. Index Appendix Annun/Alerts Displaying the TAWS-A Page 52 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Red Terrain/Obstacle above or within 100’ below current aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. Nav/Com/ XPDR/Audio Terrain/Obstacle Location Flight Instruments Color While the TAWS-A Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. GPS Nav 1) AFCS Enable/Disable Aviation Data Inhibiting/Enabling FLTA and PDA Alerting 2) Select the TAWS INH Softkey to inhibit or enable TAWS-A (choice dependent on current state). Procedures Select the TAWS-A Page. Flight Planning 1) Overriding Flaps-based FIT Alerting Select the TAWS-A Page. 2) Select the FLAP OVR Softkey. Hazard Avoidance 1) Inhibiting/Enabling GPWS Alerting Select the TAWS-A Page. 2) Select the GPWS INH Softkey to inhibit or enable GPWS alerts (choice dependent on current state). Additional Features 1) Annun/Alerts Inhibiting/Enabling GSD Alerting NOTE: Only available during a GSD alert. Select the TAWS-A Page. 2) Select the GS INH or GP INH Softkey to inhibit or enable GSD alerts (softkey choice dependent on present GSD alert type). Appendix 1) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 53 Hazard Avoidance Flight Instruments TAWS-B Nav/Com/ XPDR/Audio WARNING: The TAWS display shows supplemental information only. It should not be used for navigation. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. AFCS NOTE: TAWS operation is only available when the system is configured for a TAWS-B installation. Flight Planning GPS Nav Manual System Test 1) While the TAWS-B Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS System’. 3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS-B Page. Procedures When all is in working order, “TAWS System Test, OK” is heard. Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS-B Page. 3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Select the 360 Softkey to return to the 360° default display. 4) Rotate the Joystick clockwise to increase the display range or rotate counter-clockwise to decrease the display range. Color Terrain/Obstacle Location Red Terrain/Obstacle above or within 100’ below current aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. Index Annun/Alerts 1) Appendix Additional Features Hazard Avoidance Display Terrain and Obstacles on the TAWS-B Page 54 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance While the TAWS-B Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. Nav/Com/ XPDR/Audio 1) Flight Instruments Enable/Disable Aviation Data TAWS Inhibit GPS Nav Inhibit TAWS Flight Planning While the TAWS-B Page is displayed, select the INHIBIT Softkey. Or: Press the MENU Key. 2) Turn the small FMS Knob to select ‘Inhibit TAWS’. 3) Press the ENT Key. Procedures 1) AFCS NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. Hazard Avoidance Enable TAWS While the TAWS-B Page is displayed, select the INHIBIT Softkey. Or: While the TAWS-B Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Enable TAWS’. 3) Press the ENT Key. Additional Features 1) Annun/Alerts Displaying Terrain and Obstacles on the Navigation Map With the Navigation Map displayed, select the MAP Softkey. 2) Select the TERRAIN Softkey. Terrain and obstacles will now be displayed on the map. Appendix 1) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 55 Airborne Color Weather Radar 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 11 feet of the antenna. Nav/Com/ XPDR/Audio Flight Instruments Hazard Avoidance AFCS 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. 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Radar Page. 3) Select the MODE Softkey. 4) If the aircraft is on the ground, select the STANDBY Softkey to initiate the one minute warm-up period. After the warm-up is complete, the radar will enter the Standby Mode. After the aircraft is airborne, select the WEATHER Softkey. Procedures Flight Planning GPS Nav Displaying Weather on the Weather Radar Page Hazard Avoidance Or: Index Appendix Annun/Alerts Additional Features If the aircraft is already airborne, select the WEATHER or GROUND Softkey. The one-minute warm-up period will be initiated, after which the radar will begin transmitting. The horizontal scan is initially displayed. 5) Turn the Joystick to select the desired range. 6) If desired, select the VERTICAL Softkey for vertical scanning. Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field. When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt of the antenna. If the Tilt Line is not displayed, perform the following steps: 1) Press the MENU Key 2) Turn the large FMS Knob to select ‘Show Tilt Line’. 3) Press the ENT Key. 56 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Hazard Avoidance Move the Joystick right or left to move the scanned “slice” a few degrees right or left. 4) Turn the Joystick to adjust the range. 5) To select a new area to be vertically scanned, select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps. Adjusting Gain 2) 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. 4) Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be displayed in the ‘GAIN’ field. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 57 Index 190-00929-02 Rev. A Appendix Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field. Annun/Alerts 1) Additional Features WARNING: Changing the gain in Weather Mode will cause 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. Hazard Avoidance 3) Procedures Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now be displayed. Flight Planning 2) GPS Nav 1) While in the Horizontal Scan view, move the Joystick to place the Bearing Line on the desired storm cell, or other area, to be vertically scanned. AFCS Vertically Scan a Storm Cell Nav/Com/ XPDR/Audio Move the Joystick right or left to adjust the azimuth position of the antenna right or left. Monitor the displayed bearing value in the BEARING field. When scanning horizontally, a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan. If the Bearing Line is not displayed, perform the following steps: 1) Press the MENU Key 2) Turn the large FMS Knob to select ‘Show Bearing Line’. 3) Press the ENT Key. Flight Instruments Adjusting Antenna Bearing Hazard Avoidance Nav/Com/ XPDR/Audio Flight Instruments Ground Mapping 1) Select the MODE Softkey. 2) Select the GROUND Softkey to place the radar in Ground Map Mode. 3) Select the BACK Softkey. Sector Scan While in the Horizontal Scan Mode, move the Joystick right or left to place the Bearing Line in the desired position. The location of the Bearing Line will become the center point of the Sector Scan. 2) Press the FMS Knob to display the cursor. 3) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field. 4) Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan. 5) If desired, readjust the Bearing Line with the Joystick to change the center of the Sector Scan. 6) Press the FMS Knob to remove the cursor. Flight Planning GPS Nav AFCS 1) Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Antenna Stabilization 1) To activate or deactivate the antenna stabilization, select the MODE Softkey. 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. Weather Attenuated Color Highlight (WATCH®) To activate or deactivate the Watch® feature, select the WATCH Softkey. This feature is only available in the Horizontal Scan Mode. Weather Alert To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating and deactivating will also enable or inhibit the alert on the PFD. Automatic Standby When the weather radar system is in the Weather or Ground Map Mode, upon landing the system will automatically switch to Standby Mode. 58 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Flight Instruments Additional Features Synthetic Vision Hazard Avoidance Additional Features Annun/Alerts Displaying SVS Terrain 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. 4) Press the BACK Softkey to return to the previous page. Appendix Press the PFD Softkey. Procedures Pathways Flight Path Marker Horizon Heading Marks Terrain and Obstacle Alerting Three-dimensional Traffic Airport Signs Runway Display 1) Flight Planning • • • • • • • GPS Nav Synthetic Vision System (SVS) functionality is offered as an optional enhancement to the G1000 system. SVS 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. SVS information is shown on the primary flight display (PFD). In addition to SVS enhancement to the PFD, the following features have been added to the PFD: AFCS WARNING: Do not use SVS 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. Nav/Com/ XPDR/Audio WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS 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. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 59 Additional Features Nav/Com/ XPDR/Audio Flight Instruments Displaying Pathways Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the PATHWAY Softkey. 5) Press the BACK Softkey to return to the previous page. Flight Planning GPS Nav AFCS Displaying Heading on the Horizon 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the HRZN HDG Softkey. 5) Press the BACK Softkey to return to the previous page. Procedures Displaying Airport Signs Hazard Avoidance Additional Features Annun/Alerts Appendix Index 1) 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the APTSIGNS Softkey. 5) Press the BACK Softkey to return to the previous page. 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 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey. 3) Select the GO BACK Softkey to return to the previous page. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS are only available with ChartView. Appendix 2) Annun/Alerts Or: Additional Features Select the SHW CHRT Softkey when displayed. Hazard Avoidance 1) Procedures View Charts from the Navigation Map Page Flight Planning FliteCharts® resemble the paper version of AeroNav Services terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. Current aircraft position is not displayed on FliteCharts. 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. GPS Nav FliteCharts® AFCS 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. Nav/Com/ XPDR/Audio ChartView Flight Instruments 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 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. 61 Additional Features AFCS Nav/Com/ XPDR/Audio Flight Instruments View Charts from the Active Flight Plan Page 1) While viewing the Active Flight Plan Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to select the departure airport, destination airport, departure, arrival, or approach. 3) Select the SHW CHRT Softkey. The appropriate chart will be displayed, if available for the item selected. 4) Select the GO BACK Softkey to return to the previous page. While viewing a 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. 5) Hazard Avoidance Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’ Options. 6) In Auto Mode, turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob. The percentage of change is the day/night crossover point based on backlighting intensity. 7) Press the FMS Knob when finished to remove the Chart Setup Menu. Procedures Flight Planning GPS Nav 1) Additional Features Change Day/Night View AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT-Airport Information Page. This database is updated four times per year. Check fly.garmin.com for the current database. View Airport Directory Information While viewing the WPT-Airport Information Page, if necessary, select the INFO-1 Softkey to change the softkey label to display INFO-2. AOPA airport information is displayed on the right half of the display. Index Appendix Annun/Alerts AOPA Airport Directory 62 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Procedures Register the System for Telephone and Low Speed Data Services Flight Planning A subscriber account must be established prior to using the Iridium Satellite System for telephone, text messaging and low speed data services. Contact Garmin Flight Data Services at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135. After an account has been established, the system must be registered. GPS Nav Registering the Iridium Satellite System AFCS Operation of these features in the cockpit is accomplished through the AUXTELEPHONE, AUX-TEXT MESSAGING, AUX-REPORT STATUS, and AUX-WI-FI SETUP Pages. For operation using the cabin handset, consult the instructions provided with the handset. Nav/Com/ XPDR/Audio 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. Flight Instruments Satellite Telephone and Data Link Services 3) Turn the small FMS Knob to select the AUX-REPORTS STATUS or AUX-WI-FI SETUP Page. 4) If necessary, select the REPORTS Softkey. The AUX-Report Status Page is now displayed. 5) Press the MENU Key. The Page Menu window is now displayed. 6) If the system is connected to Wi-Fi proceed to step 10. If there is no Wi-Fi connection, turn the FMS Knob to select ‘Iridium Internet’ in the menu list. 7) Press the ENT Key. 8) Select CONNECT Softkey. Momentarily, IRIDIUM 1 will display ‘CONNECTED’ in the Connection Status Window. 9) Press the MENU Key to again display the Page Menu window. Appendix Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the System ID number in the AIRFRAME field. Annun/Alerts 2) Additional Features Turn the large FMS Knob on the MFD to select the AUX page group. Hazard Avoidance 1) 10) Select ‘Register With GFDS’ in the menu list. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 63 Index 11) Press the ENT Key. The Garmin Flight Data Service Registration window is now displayed. Additional Features Flight Instruments 12) Enter the last four digits of the System ID number in the Access Code field. 13) Press the ENT Key. REGISTER will now be highlighted. AFCS Nav/Com/ XPDR/Audio 14) Press the ENT Key. System registration is complete when ‘REGISTERED’ is displayed in the STATUS field. Disable/Enable Iridium Transceiver Iridium telephone and data communications may be turn on of off by performing these simple steps. 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-REPORTS STATUS or AUX-WI-FI SETUP Page. 3) If necessary, select the REPORTS Softkey. The AUX-Report Status Page is now displayed. 4) Press the MENU Key. The Page Menu window is now displayed. 5) Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list. 6) Press the ENT Key. The Iridium transceiver is now disabled. 7) To enable the Iridium transceiver, repeat steps 1 through 4, then select ‘Enable Iridium Transceiver’. Telephone Communication 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 cabin phone, however, only actions initiated from the cockpit phone will be discussed here. See the cabin handset user guide for more information. Control and monitoring of telephone functions are accomplished through the AUXTELEPHONE Page. Appendix Viewing the Telephone 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 - TELEPHONE or AUX - TEXT MESSAGING Page. Index Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav Disable/Enable Telephone and Low Speed Data Services: 3) If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page. 64 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features External Phone Flight Instruments Internal Phone Description Nav/Com/ XPDR/Audio Phone is Idle Phone is ringing AFCS Phone has a dial tone (off hook) or connected to another phone GPS Nav Phone dialed is busy Flight Planning Phone is dialing another phone Procedures Phone has failed Hazard Avoidance Phone status not known Phone is disabled Additional Features Phone is reserved for data transmission Annun/Alerts Calling other phone or incoming call from other phone Appendix Other phone is on hold Index Phones are connected 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 65 Incoming Calls When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up alert will be displayed. 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. AFCS Nav/Com/ XPDR/Audio Flight Instruments Additional Features GPS Nav Answer an Incoming Call in the Cockpit 1) Press the TEL Key on the appropriate audio panel. 2) Select the ANSWER Softkey on the MFD. Or: 1) 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. 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. Mute 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 ‘Mute 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. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning While viewing the AUX-TELEPHONE Page 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Voice calls can be made from the cockpit to the handset in the cabin, or to an external phone through the Iridium Satellite Network. Nav/Com/ XPDR/Audio Make a Call to the Cabin: Press the TEL Key on the appropriate audio panel. 2) Select 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. AFCS 1) GPS Nav To exit the call, select the HANGUP Softkey. Make an External Call from the Cockpit Press the TEL Key on the appropriate audio panel. 2) Select 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 Planning 1) Hazard Avoidance Additional Features Annun/Alerts Placing The Cockpit Phone on Hold Select the HOLD Softkey on the MFD. Or: 2) Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’. 3) Press the ENT Key. Appendix Press the MENU Key to display the Page Menu. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Select the HOLD Softkey again to resume the call. 190-00929-02 Rev. A Procedures To exit the call, select the HANGUP Softkey. 1) Flight Instruments Outgoing Calls 67 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, or (when two Iridium Transceivers are installed) an external call can be transferred to another external phone. To transfer a call: 1) AFCS Nav/Com/ XPDR/Audio Flight Instruments Additional Features Select the TRANS Softkey on the MFD. Or: GPS Nav a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’. Procedures Flight Planning c) Press the ENT Key. 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. Hazard Avoidance Making a Conference Call from the Cockpit 1) Select the CONF Softkey on the MFD. Additional Features Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’. Index Appendix Annun/Alerts c) Press the ENT Key. 68 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Viewing the Text Messaging Page 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, select the SMS Softkey to display the AUX-TEXT MESSAGING Page. Flight Planning Description GPS Nav Message Symbol AFCS 1) Nav/Com/ XPDR/Audio 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. Flight Instruments Text Messaging (SMS) Received text message that has not been opened Procedures Received text message that has been opened Hazard Avoidance Saved text message, draft not sent Additional Features System is sending text message Annun/Alerts Text message has been sent System failed to send text message Appendix Predefined text message Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 69 AFCS Nav/Com/ XPDR/Audio Flight Instruments Additional Features Viewing a Text Message When Received 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 IGNR 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. Procedures Flight Planning GPS Nav Enable/Disable Incoming Text Message Pop-Up Alerts 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. Reply to a Text Message Hazard Avoidance While viewing the text message, select the REPLY Softkey. Or: a) Press the MENU Key to display the Page Menu. Additional Features b) Turn either FMS Knob to place the cursor on ‘Reply To Message’. c) Press the ENT Key. Annun/Alerts Sending a Text Message 1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey. Or: Appendix a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Draft New Message’. Index c) Press the ENT Key. 70 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features 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. 6) Select the SEND Softkey to send the message immediately, or select the SAVE Softkey to save the message in Outbox for sending at a later time. Select the CANCEL Softkey to delete the message. AFCS 3) Nav/Com/ XPDR/Audio The 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 selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. Flight Instruments 2) GPS Nav Flight Planning Predefined Text Messages Procedures Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message. Create a Predefined Text Message 2) Turn either FMS Knob to select ‘Edit Predefined Messages’. 3) Press the ENT Key. The Predefined Messsages view is now displayed. 4) Select the NEW Softkey. Additional Features While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to display the Page Menu. Hazard Avoidance 1) Annun/Alerts Or: a) Press the MENU Key to display the Page Menu. Appendix b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined Message’. c) Press the ENT Key. The Predefined SMS Text Message Window is now displayed. 5) 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 71 Index 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 Additional Features 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) Select the SAVE Softkey. The new predefined message is now shown in the displayed list. Selecting the CANCEL Softkey will delete the message without saving. GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. 10) Press the MENU Key to display the Page Menu. Flight Planning 11) Turn either FMS Knob to place the cursor on ‘Stop Editing Predefined Message’. Procedures 12) Press the ENT Key. While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey. 2) The 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 selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. 3) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field. 4) Appendix Select the PREDEFD Softkey. The Predefined Message Menu Window is displayed. 6) 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. 7) Press the ENT Key. 8) Select the SEND Softkey to transmit the message. Annun/Alerts Additional Features Hazard Avoidance 1) Index Send a Predefined Text Message 72 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Show Inbox Messages AFCS While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the INBOX Softkey. 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. Flight Instruments Text Message Boxes Or: GPS Nav a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’. Flight Planning c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Show Outbox Messages Procedures While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the OUTBOX Softkey. Or: b) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’. Additional Features c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Hazard Avoidance a) Press the MENU Key to display the Page Menu. Show Draft Messages Annun/Alerts While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the DRAFTS Softkey. Or: Appendix a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’. c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 73 Arranging 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. View Messages Sorted by Message Date/Time: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TIME Softkey. AFCS Nav/Com/ XPDR/Audio Flight Instruments Additional Features Or: GPS Nav a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’. Flight Planning c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. View Messages Sorted by Message Type Procedures While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TYPE Softkey. Or: a) Press the MENU Key to display the Page Menu. Hazard Avoidance b) Turn either FMS Knob to place the cursor on ‘Sort By Type’. Additional Features c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. View Messages Sorted by Address: Annun/Alerts While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the ADDRESS Softkey. Or: a) Press the MENU Key to display the Page Menu. Appendix b) Turn either FMS Knob to place the cursor on ‘Sort By Address’. Index c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. 74 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features While viewing the AUX-TEXT MESSAGING Page, select the desired message box. 2) Press the FMS Knob to activate the cursor. 3) Turn either FMS Knob to select the desired message. 4) Select the VIEW Softkey. Nav/Com/ XPDR/Audio 1) Flight Instruments Viewing The Content of a Text Message Or: AFCS Press the ENT Key. Or: b) Turn either FMS Knob to place the cursor on ‘View Selected Message’. GPS Nav a) Press the MENU Key to display the Page Menu. c) Press the ENT Key. To close the text message, select the CLOSE Softkey. Flight Planning 5) Or: a) Press the MENU Key to display the Page Menu. Procedures b) Turn either FMS Knob to place the cursor on ‘Close Message’. c) Press the ENT Key. 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) Select the MRK READ Softkey. Additional Features 1) Hazard Avoidance Mark Selected Message As Read Or: Annun/Alerts a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message As Read’. Appendix c) Press the ENT Key. The message symbol now indicates the message has been opened. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 75 Additional Features AFCS Nav/Com/ XPDR/Audio Flight Instruments 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. Flight Planning GPS Nav Delete 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) Select the DELETE Softkey. Or: b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’. c) Press the ENT Key. WI-FI Connections The system can connect to a IEEE 802.11g compatible network provided the aircraft is on the ground and located within range of the network. The system is capable of WEP64, WEP128,WPA-PSK, and WPA2-PSK encryption formats. WPAEnterprise 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 AUXWI-FI SETUP Page. View the Wi-Fi Setup Page Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures a) Press the MENU Key to display the Page Menu. 76 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 - WI-FI SETUP or AUX - REPORT STATUS Page. 3) If necessary, select the WI-FI Softkey to display the AUX-WI-FI SETUP Page. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Select 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, select the RESCAN Softkey to have the system scan again for available networks. Nav/Com/ XPDR/Audio 1) Flight Instruments Set Up a New Wi-Fi Connection AFCS Or: a) Press the MENU Key to display the Page Menu. GPS Nav 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) Select the CONNECT Softkey. Flight Planning 3) Procedures Or: a) Press the MENU Key to display the Page Menu. Hazard Avoidance 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’. 10) The selected network can be saved to system memory to make reconnection easier at a later time. 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. Select the CAP LOCK Softkey to enter upper case letters. If there is no security associated with the network, proceed to step 9. Additional Features 6) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 77 Additional Features Flight Instruments To connect the selected network without saving: a) Turn the large FMS Knob to move the cursor to highlight ‘CONNECT’. b) Press the ENT Key. Nav/Com/ XPDR/Audio To save and connect the selected network: a) Press the ENT Key. A checkmark is placed in the checkbox and the cursor moves to the airport field. AFCS 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. GPS Nav c) Press the ENT Key. The cursor moves to ‘CONNECT’. d) Press the ENT Key again to connect to the selected network. Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning Edit 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) Select 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. Disconnect a Wi-Fi Network Appendix Select 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. 78 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features Flight Instruments Delete a Saved Wi-Fi Network: 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) Select the DELETE Softkey. The selected network is removed from the list. AFCS System Data Logging Nav/Com/ XPDR/Audio 1) 2) Turn the small FMS Knob to select AUX-WI-FI SETUP or aux-REPORT STATUS Page. 3) If necessary, select the REPORT Softkey to display the AUX-REPORT STATUS Page. Additional Features Turn the large FMS Knob on the MFD to select the AUX page group. Hazard Avoidance 1) Procedures View the Report Status Page Flight Planning The system selects the appropriate transmission method based on communication network availability. Data transmission is manually when the airplane is on the ground. If report transmission is interrupted for some reason (e.g. networks unavailable, hardware failure, loss of power), the system will attempt to resume sending the reports at the next opportunity. The system ensures the complete data set is transmitted. Transmitted reports remain in the system’s memory until they are overwritten by newer data. Control and monitoring of report transmissions is accomplished through the AUXREPORT STATUS Page. GPS Nav NOTE: An account must be established with Garmin Flight Data Services to make full use of the System Data Logging feature. Annun/Alerts Changing Transmission Method 2) Turn the large FMS Knob to move the cursor to the 1st or 2nd transmit method for the desired data report. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index While viewing the Report Status Page, press the FMS Knob to activate the cursor. Appendix 1) 79 Nav/Com/ XPDR/Audio Flight Instruments Additional Features 3) Turn the small FMS Knob to select the desired option (SAT SHORT BURST, SAT RUDICS, WI-FI, or NONE). Sat Short Burst is generally used for transmission of data packets less than 300 bytes. Wi-Fi is used only when the aircraft on the ground. 4) Press the ENT Key. Flight Planning GPS Nav AFCS Send All Unsent Data 1) While viewing the Report Status Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to move the cursor to the SEND button on the desired data report. 3) Press the ENT Key. The Send Report window is displayed. 4) Turn the large FMS Knob to highlight the ‘select data to send’ field. 5) Turn the small FMS Knob to select ‘all unsent data’. 6) Press the ENT Key. Procedures Resend Data or Send Data Recorded in a Specific Time Frame NOTE: Transmission of data can only be performed while the aircraft is Index Appendix Annun/Alerts Additional Features Hazard Avoidance on the ground. 1) While viewing the Report Status Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to move the cursor to the SEND button on the desired data report. 3) Press the ENT Key. The Send Report window is displayed. 4) Turn the large FMS Knob to highlight the ‘select data to send’ field. 5) Turn the small FMS Knob to select ‘data within time frame’. 6) Press the ENT Key. The time frame selection fields are now displayed. 7) Turn the large FMS Knob to select the starting time or date field. 8) Turn the small FMS Knob to select the desired starting time or date. 9) Press the ENT Key. The cursor will move to the next field. 10) When the last field is addressed, ‘OK’ will be highlighted. Press the ENT Key to send the selected data. 80 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features 2) Turn the FMS Knob to select ‘Restore Defaults’ in the menu list. 3) Press the ENT Key. 4) A confirmation window is now displayed. 5) Turn the large FMS Knob to select ‘YES’ or ‘NO’. 6) With ‘YES’ highlighted, press the ENT Key. AFCS While viewing the Report Status Page, press the MENU Key. Nav/Com/ XPDR/Audio 1) Flight Instruments Restore Reports Page Options to Default Settings: XM® 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) Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. Procedures 1) Flight Planning Selecting the XM Radio Page Selecting a Category Index 81 Appendix Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Annun/Alerts The Category Box of the XM Radio Page displays the currently selected category of audio. 1) Select the CATGRY Softkey on the XM Radio Page. 2) Select 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. 3) Press the ENT Key. Additional Features 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. Hazard Avoidance Active Channel and Channel List 190-00929-02 Rev. A GPS Nav The XM® Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. Additional Features Nav/Com/ XPDR/Audio Flight Instruments Select an Available Channel within the Selected Category 1) While on the XM Radio Page, select the CHNL Softkey. 2) Select the CH + Softkey to move down through the list in the Channel Box, or move up the list with the CH – Softkey. Or: AFCS Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels. 3) With the desired channel highlighted, press the ENT Key. Procedures Flight Planning GPS Nav Entering a Channel Directly 1) While on the XM Radio Page, select the CHNL Softkey. 2) Select the DIR CH Softkey. The channel number in the Active Channel Box is highlighted. 3) Select 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. Assigning Channel Presets Annun/Alerts Additional Features Hazard Avoidance Up to 15 channels from any category can be assigned a preset number. 1) On the XM Radio Page, with the desired channel active, select the PRESETS Softkey to access the first five preset channels (PS1 - PS5). 2) Select the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five channels (PS11 – PS15). Selecting the MORE Softkey repeatedly cycles through the preset channels. 3) Select the SET Softkey. 4) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel. Appendix Adjusting Volume Index Radio volume is controlled at each passenger station. 82 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Additional Features 5) Turn the large FMS Knob to place the cursor in the STABILITY & PROTECTION field. 6) Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’. 7) Press the FMS Knob to remove the cursor. 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index Press the FMS Knob to activate the cursor. Appendix 4) Annun/Alerts If necessary, select 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. Additional Features 3) Hazard Avoidance Turn the small FMS Knob to select the System Setup Page. Procedures 2) Flight Planning Turn the large FMS Knob to select the AUX Page Group. GPS Nav 1) AFCS To enable or disable ESP: Nav/Com/ XPDR/Audio 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 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. Flight Instruments Electronic Stability & Protection (ESP™) 83 GPS Nav AFCS Nav/Com/ XPDR/Audio 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 onside 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°. 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 ESP force may be applied if the Angle of Attack 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. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning Pitch Engagement 84 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Flight Instruments Annunciations & Alerts WARNING Annunciation Alerts Window Text Nav/Com/ XPDR/Audio Aural Alert “Airspeed” is heard once when an altitude-notUNDERSPEED critcal flight director mode is active. “Airspeed” PROTECT ACTIVE - repeats every five seconds when an altitudecritical flight director mode is active. AFCS Annunciation Window Text UNDERSPEED PROTECT ACTIVE GPS Nav Advisory Annunciations Alerts Window Text AVN FAN 2 FAIL AVN FAN 2 FAIL - Avionics cooling fan #2 is inoperative. PFD 1 FAN FAIL PFD 2 FAN FAIL PFD 1 FAN FAIL - PFD #1 cooling fan is inoperative. MFD FAN FAIL MFD FAN FAIL - MFD cooling fan is inoperative. Procedures AVN FAN 1 FAIL - Avionics cooling fan #1 is inoperative. Flight Planning Annunciation Window Text AVN FAN 1 FAIL PFD FAN FAIL - PFD #2 cooling fan is inoperative. Hazard Avoidance Message Advisory Alerts Alerts Window Message Additional Features Annun/Alerts ESP DEGRADE – ESP AOA mode is inoperative. ESP DEGRADE – ESP IAS mode is inoperative. ESP FAIL – ESP is inoperative. ESP OFF – ESP selected off. 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. WOW INVALID – Weight on wheels inputs invalid. YD OFF – AP engaged without Yaw Damper. Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 85 Comparator Annunciations Comparator Window Text ALT MISCOMP Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts Difference in altitude sensors is > 200 ft. If both airspeed sensors detect < 35 knots, this is inhibited. IAS MISCOMP If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts. Procedures Flight Planning GPS Nav AFCS If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts. HDG MISCOMP Difference in heading sensors is > 6 degrees. PIT MISCOMP Difference in pitch sensors is > 5 degrees. ROL MISCOMP Difference in roll sensors is > 6 degrees. ALT NO COMP No data from one or both altitude sensors. IAS NO COMP No data from one or both airspeed sensors. HDG NO COMP No data from one or both heading sensors. PIT NO COMP No data from one or both pitch sensors. ROL NO COMP No data from one or both roll sensors.. Condition BOTH ON ADC1 BOTH ON ADC2 BOTH ON AHRS1 Both PFDs are displaying data from the number one Air Data Computer. BOTH ON AHRS2 Both PFDs are displaying data from the number two Attitude & Heading Reference System. BOTH ON GPS1 BOTH ON GPS2 USING ADC1 USING ADC2 USING AHRS1 Both PFDs are displaying data from the number one GPS receiver. Index Appendix Reversionary Sensor Window Text Additional Features Reversionary Sensor Annunciations Annun/Alerts Hazard Avoidance Condition 86 Both PFDs are displaying data from the number two Air Data Computer. Both PFDs are displaying data from the number one Attitude & Heading Reference System. Both PFDs are displaying data from the number two 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 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts PFD1 is displaying data from the #2 AHRS. PFD2 is displaying data from the #1 GPS. Nav/Com/ XPDR/Audio USING AHRS2 USING GPS1 USING GPS2 Condition Flight Instruments Reversionary Sensor Window Text PFD1 is displaying data from the #2 GPS. Condition Annunciation Description Roll Failure Roll axis control failure. Pitch Trim Axis Control Failure If annunciated when AP is engaged, a failure has occurred in the pitch trim system. System Failure AP and MET are unavailable. FD may still be available. Flight Planning Pitch axis control failure. GPS Nav Pitch Failure Procedures YD control failure. A condition has developed causing the pitch servo to provide a sustained force in the nose up direction. Hazard Avoidance Yaw Damper Failure Elevator Mistrim Up AFCS AFCS Alerts Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left force. Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force. Rudder Mistrim Left A condition has developed causing the yaw servo to provide a sustained force. Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force. Preflight Test Performing preflight system test. Upon completion of the test, the aural alert will be heard. Annun/Alerts A condition has developed causing the pitch servo to provide a sustained force in the nose down direction. Additional Features Elevator Mistrim Down Appendix Preflight system test has failed. Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 87 TAWS-A Alerts Alert Type PFD/MFD TAWS Page Annunciation MFD Map Page Pop-Up Alert Reduced Required Terrain Clearance Warning (RTC) or Imminent Terrain Impact Warning (ITI) or Reduced Required Obstacle Clearance Warning (ROC) or Imminent Obstacle Impact Warning (IOI) or “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” “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” or “Obstacle, Obstacle; Pull Up, Pull Up” Excessive Closure Rate Warning (ECR) “<whoop><whoop> Pull Up” or Annun/Alerts “<whoop><whoop> Pull Up” Reduced Required Terrain Clearance Caution (RTC) Imminent Terrain Impact Caution (ITI) or Reduced Required Obstacle Clearance Caution (ROC) or Index Additional Features Aural Message Excessive Descent Rate Warning (EDR) Appendix Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 88 “Caution, Terrain; Caution, Terrain” or “Terrain Ahead; Terrain Ahead” “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain” “Caution, Obstacle; Caution, Obstacle” or “Obstacle Ahead; Obstacle Ahead” Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts or Aural Message “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle” Excessive Descent Rate Caution (EDR) “Sink Rate” Excessive Closure Rate Caution (ECR) “Terrain, Terrain” Negative Climb Rate Caution (NCR) “Don’t Sink” or “Too Low, Terrain” Flight Into Terrain Gear Caution (FIT) “Too Low, Gear” Flight Into Terrain Flaps Caution (FIT) “Too Low, Flaps” Flight Into Terrain Takeoff Caution (FIT) “Too Low, Terrain” or or None None (depends on approach type) (all are configurable, except “Five-Hundred”) “Five-Hundred” “Four-Hundred” “Three-Hundred” “Two-Hundred” “One-Hundred” Annun/Alerts Altitude Voice Callout (VCO) “Glide Slope” or “Glide Path” Additional Features Glide Slope Deviation Caution (GSD) Hazard Avoidance “Too Low, Terrain” Procedures Flight Into Terrain High Speed Caution (FIT) Flight Planning or GPS Nav “Too Low, Terrain” AFCS Premature Descent Alert Caution (PDA) Nav/Com/ XPDR/Audio Imminent Obstacle Impact Caution (IOI) MFD Map Page Pop-Up Alert Flight Instruments PFD/MFD TAWS Page Annunciation Alert Type Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 89 Annunciations & Alerts Flight Instruments TAWS-A System Status Annunciations Nav/Com/ XPDR/Audio Alert Type PFD/MFD Additional TAWS-A Page TAWS-A Page Annunciation Annunciation TAWS FAIL “TAWS System Failure” System Test in progress TAWS TEST None Flight Planning GPS Nav AFCS TAWS System Fail System Test pass None None “TAWS System Test OK” MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases None TERRAIN DATABASE FAILURE None GPWS System Fail, Radar Altimeter invalid, Altitude or Vertical Speed unavailable None “GPWS System Failure” No GPS position, excessively degraded GPS signal NO GPS POSITION “TAWS Not Available” “TAWS Available” when sufficient GPS signal is received. Out of database coverage area None “TAWS Not Available” “TAWS Available” when aircraft enters database coverage area. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Aural Message 90 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Flight Instruments TAWS-A Alert Type Availability Under Various Conditions TAWS-A Alert Type Available FIT GSD VCO No No No No No No No No No No No No No No No Yes Yes Yes Yes *No **Yes No No No No No Yes Yes Yes Yes Yes **Yes No No No No No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No No No No No **Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes Yes Yes Yes Yes Yes Yes #Yes Yes Yes AFCS No Flight Planning VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available. # Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is displayed. Hazard Avoidance ** Additional Features TAWS-B Alerts Imminent Terrain Impact Warning (ITI) or “Terrain, Terrain; Pull Up, Pull Up” or “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 91 Index Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” or “Terrain, Terrain; Pull Up, Pull Up” Appendix or Aural Message Annun/Alerts MFD Map Page Pop-Up Alert Reduced Required Terrain Clearance Warning (RTC) 190-00929-02 Rev. A Procedures GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being received. PFD/MFD TAWS Page Annunciation GPS Nav * Alert Type Nav/Com/ XPDR/Audio TAWS-A Status RTC ITI ROC IOI PDA EDR ECR NCR Annunciation Displayed Alert Type PFD/MFD TAWS Page Annunciation MFD Map Page Pop-Up Alert Reduced Required Obstacle Clearance Warning (ROC) or Imminent Obstacle Impact Warning (IOI) or Aural Message “Obstacle, Obstacle; Pull Up, Pull Up” or “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” or “Obstacle, Obstacle; Pull Up, Pull Up” Excessive Descent Rate Warning (EDR) “Pull Up” Reduced Required Terrain Clearance Caution (RTC) or Imminent Terrain Impact Caution (ITI) or Reduced Required Obstacle Clearance Caution (ROC) or Imminent Obstacle Impact Caution (IOI) or “Caution, Terrain; Caution, Terrain” or “Terrain Ahead; Terrain Ahead” “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain” “Caution, Obstacle; Caution, Obstacle” or “Obstacle Ahead; Obstacle Ahead” “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle” Premature Descent Alert Caution (PDA) “Too Low, Terrain” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) or “Don’t Sink” or “Too Low, Terrain” Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 92 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Aural Message TAWS FAIL “TAWS System Failure” System Test in progress TAWS TEST None AFCS TAWS System Fail Nav/Com/ XPDR/Audio PFD/MFD Additional TAWS-A Page TAWS-A Page Annunciation Annunciation Alert Type Flight Instruments TAWS-B System Status Annunciations None None “TAWS System Test OK” MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases None TERRAIN DATABASE FAILURE None No GPS position, excessively degraded GPS signal NO GPS POSITION “TAWS Not Available” “TAWS Available” when sufficient GPS signal is received. Out of database coverage area None “TAWS Not Available” “TAWS Available” when aircraft enters database coverage area. GPS Nav System Test pass Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 93 Additional Aural Alerts Aural Alert “Minimums” Description 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. “Traffic” Played when a Traffic Advisory (TA) is issued with the TIS system. “Traffic Not Available” The aircraft is outside the Traffic Information Service (TIS) coverage area. “Traffic, Traffic” Played when first Traffic Advisory (TA) is issued with an optional TAS system. “Traffic” for each subsequent TA. Played when the traffic system passes a pilot-initiated self test. “Traffic Advisory - SKY 497 TAS System Test Passed” “SKYWATCH System Test Passed” - SKY 899 TAS “TAS System Test OK” - KTA 870 TAS Played when the traffic system fails a pilot-initiated self test. - SKY 497 TAS “Traffic Advisory System Test Failed” “SKYWATCH System Test Failed” - SKY 899 TAS “TAS System Test Fail” - KTA 870 TAS Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 94 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Flight Instruments MFD & PFD Message Advisories Message Comments DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts lost. Recheck settings. to default pilot profile and settings. The pilot may reconfigure the MFD & PFDs with preferred settings, if desired. XTALK ERROR – A flight display The MFD and PFDs are not communicating with crosstalk error has occurred. each other. The system should be serviced. PFD1 SERVICE – PFD1 needs service. Return unit for repair. PFD2 SERVICE – PFD2 needs The PFD and/or MFD self-test has detected a service. Return unit for repair. problem. The system should be serviced. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch, communication halted. MANIFEST – PFD2 software The PFD and/or MFD has incorrect software mismatch, communication halted. installed. The system should be serviced. MANIFEST – MFD1 software mismatch, communication halted. PFD1 CONFIG – PFD1 config error. The PFD configuration settings do not match Config service req’d. backup configuration memory. The system PFD2 CONFIG – PFD2 config error. should be serviced. Config service req’d. MFD1 CONFIG – MFD1 config The MFD configuration settings do not match error. Config service req’d. backup configuration memory. The system should be serviced. SW MISMATCH – GDU software The MFD and PFDs have different software version mismatch. Xtalk is off. versions installed. The system should be serviced. Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 95 MFD & PFD Message Advisories (Cont.) PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. PFD2 COOLING – PFD2 has poor cooling. Reducing power usage. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. PFD1 KEYSTK – PFD1 [key name] Key is stuck. PFD2 KEYSTK – PFD2 [key name] Key is stuck. MFD1 KEYSTK – MFD [key name] Key is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage PFD2 VOLTAGE – PFD2 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced. A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. The PFD1 configuration module backup memory has failed. The system should be serviced. The PFD1 voltage is low. The system should be serviced. The PFD2 voltage is low. The system should be serviced. The MFD voltage is low. The system should be serviced. Database Message Advisories Message MFD1 DB ERR – MFD1 navigation database error exists. PFD1 DB ERR – PFD1 navigation database error exists. PFD2 DB ERR – PFD2 navigation database error exists. Comments The MFD and/or 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 Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 96 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts The MFD and/or PFD detected a failure in the basemap database. AFCS The MFD and/or 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. GPS Nav Flight Planning Procedures The terrain database is present on another LRU, but is missing on the specified LRU. Hazard Avoidance Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix The obstacle database is present on another LRU, but is missing on the specified LRU. Annun/Alerts The MFD and/or 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. Additional Features 190-00929-02 Rev. A Comments Nav/Com/ XPDR/Audio Message MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. PFD2 DB ERR – PFD2 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. PFD2 DB ERR – PFD2 terrain database error exists. MFD1 DB ERR – MFD1 terrain database missing. PFD1 DB ERR – PFD1 terrain database missing. PFD2 DB ERR – PFD2 terrain database missing. MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists. PFD2 DB ERR – PFD2 obstacle database error exists. MFD1 DB ERR – MFD1 obstacle database missing. PFD1 DB ERR – PFD1 obstacle database missing. PFD2 DB ERR – PFD2 obstacle database missing. Flight Instruments Database Message Advisories (Cont.) 97 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. PFD2 DB ERR – PFD2 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. PFD2 DB ERR – PFD2 airport terrain database missing. MFD1 DB ERR – MFD1 Safe Taxi database error exists. PFD1 DB ERR – PFD1 Safe Taxi database error exists. PFD2 DB ERR – PFD2 Safe Taxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. Comments The MFD and/or PFD detected a failure in the airport terrain database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The airport terrain database is present on another LRU, but is missing on the specified LRU. The MFD and/or 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. The MFD and/or PFDs 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 The MFD and/or PFDs detected a failure in the database error exists. FliteCharts 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 Airport The MFD detected a failure in the Airport Directory Directory database error exists. database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. 98 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Flight Planning Message Comments GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure. GMA2 FAIL – GMA2 is inoperative. The audio panel is unavailable. The system should be serviced. GMA XTALK – GMA crosstalk error An error has occurred in transferring data has occurred. between the two GMAs. The system should be serviced. 190-00929-02 Rev. A GPS Nav GMA 1347D Message Advisories AFCS Comments The PFDs and MFD have different navigation database versions or types (Americas, European, etc.) installed. Crossfill is off. Install correct navigation database version or type in all displays. DB MISMATCH – Standby The PFDs and MFD have different standby Navigation database mismatch. navigation database versions or types (Americas, European, etc.) installed. Install correct standby navigation database version or type in all displays. DB MISMATCH – Terrain database The PFDs and MFD have different terrain database mismatch. versions or types installed. Install correct terrain database version or type in all displays. DB MISMATCH – Obstacle The PFDs and MFD have different obstacle database mismatch. database installed. Install correct obstacle database in all displays. DB MISMATCH – Airport Terrain The PFDs and MFD have different airport terrrain database mismatch. databases installed. Install correct airport terrain database in all displays. NAV DB UPDATED – Active System has updated the active navigation navigation database updated. database from the standby navigation database. TERRAIN DSP – [PFD1, PFD2 or One of the terrain, airport terrain, or obstacle MFD1] Terrain awareness display databases required for TAWS in the specified PFD unavailable. or MFD is missing or invalid. Nav/Com/ XPDR/Audio Message DB MISMATCH – Navigation database mismatch. Xtalk is off. Flight Instruments Database Message Advisories (Cont.) 99 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts GMA 1347D Message Advisories (Cont.) Message GMA1 CONFIG – GMA1 config error. Config service req’d. GMA2 CONFIG – GMA2 config error. Config service req’d. MANIFEST – GMA1 software mismatch, communication halted. MANIFEST – GMA2 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. GMA2 SERVICE – GMA2 needs service. Return unit for repair. GIA 63W Message Advisories Message GIA1 CONFIG – GIA1 config error. Config service req’d. GIA2 CONFIG – GIA2 config error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. 100 Comments The audio panel configuration settings do not match backup configuration memory. The system should be serviced. The audio panel has incorrect software installed. The system should be serviced. The audio panel self-test has detected a problem in the unit. Certain audio functions may still be available, and the audio panel may still be usable. The system should be serviced when possible. Comments The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The system should be serviced. The GIA1 and/or GIA2 have an error in the audio configuration. The system should be serviced. The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. The GIA1 and/or GIA2 temperature is too high. If problem persists, the system should be serviced. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Comments The GIA1 and/or GIA2 self-test has detected a problem in the unit. The system should be serviced. Nav/Com/ XPDR/Audio AFCS A GIA mismatch has been detected, where only one is SBAS capable. GPS Nav Flight Planning The GIA1 and/or GIA 2 has incorrect software installed. The system should be serviced. Procedures Incorrect servo software is installed, or gain settings are incorrect. Appendix The COM1 and/or 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. Annun/Alerts The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The system should be serviced when possible. Additional Features The system has detected an over temperature condition in COM1 and/or COM2. The transmitter is operating at reduced power. If the problem persists, the system should be serviced. Hazard Avoidance Message GIA1 SERVICE – GIA1 needs service. Return the unit for repair. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. MANIFEST – GIA1 software mismatch, communication halted. MANIFEST – GIA2 software mismatch, communication halted. MANIFEST – GFC software mismatch, communication halted. COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. Flight Instruments GIA 63W Message Advisories (Cont.) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 101 GIA 63W Message Advisories (Cont.) COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck. The COM1 and/or 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. LOI – GPS integrity lost. Crosscheck GPS integrity is insufficient for the current phase with other NAVS. of flight. GPS NAV LOST – Loss of GPS Loss of GPS navigation due to insufficient navigation. Insufficient satellites. satellites. GPS NAV LOST – Loss of GPS Loss of GPS navigation due to position error. navigation. Position error. GPS NAV LOST – Loss of GPS Loss of GPS navigation due to GPS failure. navigation. GPS fail. ABORT APR – Loss of GPS Abort approach due to loss of GPS navigation. navigation. Abort approach. APR DWNGRADE – Approach Vertical guidance generated by SBAS is downgraded. unavailable, use LNAV only minimums. TRUE APR – True north approach. Displayed after passing the first waypoint of a Change HDG reference to TRUE. true north approach when the nav angle is set to ‘AUTO’. GPS1 SERVICE – GPS1 needs A failure has been detected in the GPS1 and/ service. Return unit for repair. or GPS2 receiver. The receiver may still be GPS2 SERVICE – GPS2 needs available. The system should be serviced. service. Return unit for repair. NAV1 SERVICE – NAV1 needs A failure has been detected in the NAV1 and/ service. Return unit for repair. or NAV2 receiver. The receiver may still be NAV2 SERVICE – NAV2 needs available. The system should be serviced. service. Return unit for repair. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 102 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts The remote NAV1 and/or 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. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. A failure has been detected in glideslope receiver 1 and/or receiver 2. The system should be serviced. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The system should be serviced when possible. Message Comments GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match Config service req’d. those of backup configuration memory. The system should be serviced. GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match Config service req’d. those of backup configuration memory. The system should be serviced. MANIFEST – GEA1 software The #1 GEA 71 has incorrect software installed. mismatch, communication halted. The system should be serviced. MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed. mismatch, communication halted. The system should be serviced. Procedures AFCS Flight Planning GEA 71 Message Advisories Nav/Com/ XPDR/Audio NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. GPS Nav Flight Instruments GIA 63W Message Advisories (Cont.) Hazard Avoidance Additional Features Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 103 Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. XPDR2 CONFIG – XPDR2 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. MANIFEST – GTX2 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR2 SRVC – XPDR2 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. XPDR2 FAIL – XPDR2 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The system should be serviced. The transponder configuration settings do not match those of backup configuration memory. The system should be serviced. The transponder has incorrect software installed. The system should be serviced. The transponder has incorrect software installed. The system should be serviced. The #1 transponder should be serviced when possible. The #2 transponder should be serviced when possible. There is no communication with the #1 transponder. There is no communication with the #2 transponder. Index Appendix Annun/Alerts Additional Features GRS 77 Message Advisories Message AHRS1 TAS – AHRS1 not receiving valid airspeed. Comments 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 TAS – AHRS2 not receiving The #2 AHRS is not receiving true airspeed from valid airspeed. the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The system should be serviced. AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path. GPS source. Primary GPS path has failed. The system should be serviced when possible. 104 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 105 GPS Nav Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series AFCS 190-00929-02 Rev. A Nav/Com/ XPDR/Audio Message Comments AHRS2 GPS – AHRS2 using backup The #2 AHRS is using the backup GPS path. GPS source. Primary GPS path has failed. The system should be serviced when possible. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful any GPS information. GPS information. Check AFMS limitations. The system should be serviced. AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving any or any useful any GPS information. GPS information. Check AFMS limitations. The system should be serviced. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS backup GPS information. information. The system should be serviced. AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving backup GPS backup GPS information. information. The system should be serviced. AHRS1 GPS – AHRS1 operating The #1 AHRS is operating exclusively in no-GPS exclusively in no-GPS mode. mode. The system should be serviced. AHRS2 GPS – AHRS2 operating The #2 AHRS is operating exclusively in no-GPS exclusively in no-GPS mode. mode. The system should be serviced. AHRS MAG DB – AHRS magnetic The #1 AHRS and #2 AHRS magnetic model model database version mismatch. database versions do not match. AHRS1 SRVC – AHRS1 Magnetic- The #1 AHRS earth magnetic field model is out of field model needs update. date. Update magnetic field model when practical. AHRS2 SRVC – AHRS2 Magnetic- The #2 AHRS earth magnetic field model is out of field model needs update. date. Update magnetic field model when practical. GEO LIMITS – AHRS1 too far North/South, no magnetic compass. The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged GEO LIMITS – AHRS2 too far as invalid. North/South, no magnetic compass. MANIFEST – GRS1 software The #1 AHRS has incorrect software installed. mismatch, communication halted. The system should be serviced. MANIFEST – GRS2 software The #2 AHRS has incorrect software installed. mismatch, communication halted. The system should be serviced. Flight Instruments GRS 77 Message Advisories (Cont.) Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred. HDG FAULT – AHRS2 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. MANIFEST – GMU2 software mismatch, communication halted. Comments 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. 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. The GMU 44 has incorrect software installed. The system should be serviced. Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures GDL 59 Message Advisories Message GDL59 CONFIG – GDL 59 config error. Config service req’d. GDL59 FAIL – GDL 59 has failed. GDL59 SERVICE – GDL 59 needs service. Return unit for repair. GDL59 RTR FAIL – The GDL 59 router has failed. REGISTER GFDS – Data services are inoperative, register w/GFDS. MANIFEST – GDL software mismatch, communication halted. 106 Comments GDL 59 configuration settings do not match those of backup configuration memory. The system should be serviced. A failure has been detected in the GDL 59. The receiver is unavailable. The system should be serviced. A failure has been detected in the GDL 59. The system should be serviced. A failure has been detected in the GDL 59 router. The system should be serviced. The GDL 59 is not registered with Garmin Flight Data Services, or it’s current registration data has failed authentication. The GDL 59 has incorrect software installed. The system should be serviced. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Comments A failure has been detected in the #1 GSR 56. The system should be serviced. Nav/Com/ XPDR/Audio Message GSR1 FAIL – GSR1 has failed. Flight Instruments GSR 56 Message Advisories GDL 69A Message Advisories Procedures GWX 68 Alert Messages 107 Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix 190-00929-02 Rev. A Annun/Alerts GWX SERVICE – GWX needs service. Return unit for repair. MANIFEST – GWX software mismatch, communication halted. WX ALERT – Possible severe weather ahead. Additional Features GWX FAIL – GWX is inoperative. Comments GWX 68 configuration settings do not match those of the GDU configuration. The system should be serviced. The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault. The GWX 68 radar system should be serviced. A failure has been detected in the GWX 68. The GWX 68 may still be usable. The GWX 68 has incorrect software installed. The system should be serviced. Possible severe weather detected within +/- 10 degrees of the aircraft heading at a range of 80 to 320 nm. Hazard Avoidance Message GWX CONFIG – GWX config error. Config service req’d. Flight Planning MANIFEST – GDL software mismatch, communication halted. GPS Nav GDL69 FAIL – GDL 69 has failed. Comments GDL 69 configuration settings do not match those of backup configuration memory. The system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The system should be serviced The GDL 69 has incorrect software installed. The system should be serviced. AFCS Message GDL69 CONFIG – GDL 69 config error. Config service req’d. Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts GDC 74B Message Advisories Message ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC2 ALT EC – ADC2 altitude error correction is unavailable. ADC1 AS EC – ADC1 airspeed error correction is unavailable. ADC2 AS EC – ADC2 airspeed error correction is unavailable. MANIFEST – GDC1 software mismatch, communication halted. MANIFEST – GDC2 software mismatch, communication halted. Additional Features GDC1 or GDC2 is reporting that the altitude error correction is unavailable. GDC1 or GDC2 is reporting that the airspeed error correction is unavailable. The GDC 74B has incorrect software installed. The system should be serviced. GCU 477 Message Advisories Message GCU CNFG – GCU Config error. Config service req’d. GCU FAIL – GCU is inoperative. MANIFEST – GCU software mismatch, communication halted. GCU KEYSTK – GCU [key name] Key is stuck. Comments GCU 477 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. A failure has been detected in the GCU 477. The GCU 477 is unavailable. The GCU 477 has incorrect software installed. The G1000 system should be serviced. A key is stuck on the GCU 477 bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists. Index Appendix Annun/Alerts Comments 108 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Error in the configuration of the GMC 710. Flight Planning Miscellaneous Message Advisories Annun/Alerts Appendix Index 109 Additional Features Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Hazard Avoidance Comments Upon power-up, the system detects that a stored flight plan waypoint is locked. This occurs when a navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted. 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. FPL WPT MOVE – Flight plan The system has detected that a waypoint waypoint moved. coordinate has changed due to a new navigation database update. Verify that stored flight plans contain correct waypoint locations. TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has expired. Procedures Message FPL WPT LOCK – Flight plan waypoint is locked. 190-00929-02 Rev. A GPS Nav A failure has been detected in the GMC 710. The GMC 710 is unavailable. The GMC 710 has incorrect software installed. The system should be serviced. A key is stuck on the GMC 710 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. AFCS MANIFEST – GMC software mismatch. Communication halted. GMC KEYSTK – GMC [key name] Key is stuck. Comments Nav/Com/ XPDR/Audio Message GMC CONFIG – GMC Config error. Config service req’d. GMC FAIL – GMC is inoperative. Flight Instruments GMC 710 Message Advisories Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts Miscellaneous Message Advisories (Cont.) Message DB CHANGE – Database changed. Verify user modified procedures. Comments This occurs when a stored flight plan contains procedures that have been manually edited. 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 CHANGE – Database changed. This occurs when a stored flight plan contains Verify stored airways. 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. LOCKED FPL – Cannot navigate This occurs when the pilot attempts to activate locked flight plan. a stored flight plan that contains locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. WPT ARRIVAL – Arriving at Arriving at waypoint [xxxx], where [xxxx] is the waypoint -[xxxx] waypoint name. STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. INSIDE ARSPC – Inside airspace. The aircraft is inside the airspace. ARSPC AHEAD – Airspace ahead Special use airspace is ahead of aircraft. The less than 10 minutes. aircraft will penetrate the airspace within 10 minutes. ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the ahead. aircraft position. ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the than 2 nm. aircraft position. APR INACTV – Approach is not The system notifies the pilot that the loaded active. approach is not active. Activate approach when required. 110 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts Hazard Avoidance Additional Features Annun/Alerts Appendix IAF waypoint for parallel offset has been passed. 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. 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. The current track angle error exceeds the limit, causing the vertical deviation to go invalid. The current crosstrack exceeds the limit, causing vertical deviation to go invalid. A parallel course has been selected, causing the vertical deviation to go invalid. Procedures VNV – Unavailable. Excessive track angle error. VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable. Parallel course selected. Invalid leg type for parallel offset. Flight Planning VNV – Unavailable. Unsupported leg type in flight plan. Bad parallel track geometry. GPS Nav PTK FAIL – Parallel track unavailable: bad geometry. PTK FAIL – Parallel track unavailable: invalid leg type. PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. AFCS SLCT NAV – Select NAV on CDI for approach. Comments The system notifies the pilot to load the approach frequency for the appropriate NAV receiver. Select the correct frequency for the approach. The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to the correct NAV receiver. Nav/Com/ XPDR/Audio Message SLCT FREQ – Select appropriate frequency for approach. Flight Instruments Miscellaneous Message Advisories (Cont.) Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 111 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts Miscellaneous Message Advisories (Cont.) Message Comments NON WGS84 WPT – Do not use GPS The position of the selected waypoint [xxxx] for navigation to [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. TRAFFIC FAIL – Traffic device has The system is no longer receiving data from failed. the traffic system. The traffic device should be serviced. STRMSCP FAIL – Stormscope has Stormscope has failed. The G1000™ system failed. should be serviced. FAILED PATH – A data path has A data path connected to the GDU or the GIA failed. 63/W has failed. MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine variance. Verify all course angles. 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°. SVS – SVS DISABLED: Out of Synthetic Vision is disabled because the aircraft available terrain region. is not within the boundaries of the installed terrain database. SVS – SVS DISABLED: Terrain DB Synthetic Vision is disabled because a terrain resolution too low. database of sufficient resolution (9 arc-second or better) is not currently installed. SCHEDULER [#] – <message>. Message criteria entered by the user. USER MAG VAR – User magnetic User magnetic variation mode was selected variation is active. during previous operation and is still active (checked at power-up.) CHECK CRS – Database course for Selected course for LOC1 differs from published LOC1 / [LOC ID] is [CRS]°. localizer course by more than 10 degrees. CHECK CRS – Database course for Selected course for LOC2 differs from published LOC2 / [LOC ID] is [CRS]°. localizer course by more than 10 degrees. 112 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Annunciations & Alerts AFCS GPS Nav Comments The SD card was removed from the top card slot of the specified PFD or MFD. The SD card needs to be reinserted. The SD card was removed from the bottom card slot of the specified PFD or MFD. The SD card needs to be reinserted. The SD card in the top card slot of the specified PFD or MFD contains invalid data. The SD card in the bottom card slot of the specified PFD or MFD contains invalid data. Nav/Com/ XPDR/Audio Message [PFD1, PFD2, or MFD1] CARD 1 REM – Card 1 was removed. Reinsert card. [PFD1, PFD2, or MFD1] CARD 2 REM – Card 2 was removed. Reinsert card. [PFD1, PFD2, or MFD1] CARD 1 ERR – Card 1 is invalid. [PFD1, PFD2, or MFD1] CARD 2 ERR – Card 2 is invalid. Flight Instruments Miscellaneous Message Advisories (Cont.) Flight Planning Flight Plan Import/Export Messages In some circumstances, some messages may appear in conjunction with others. ‘Flight plan successfully imported.’ Procedures Flight Plan Import/Export Results Description 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. Annun/Alerts ‘No flight plan files found to import.’ Additional Features ‘File contained user waypoints only. User The file stored on the SD card did not contain a flight plan, waypoints imported successfully. No only user waypoints. These waypoints have been saved to the stored flight plan data was modified.’ system user waypoints. No flight plans stored in the system have been modified. Hazard Avoidance A flight plan file stored on the SD card was successfully imported as a stored flight plan. Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 113 Flight Plan Import/Export Results ‘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. GPS Nav Flight Planning Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Description ‘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. AFCS Nav/Com/ XPDR/Audio Flight Instruments Annunciations & Alerts 114 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix Flight Instruments Appendix PFD Softkey Map Nav/Com/ XPDR/Audio ALERTS AFCS GPS Nav Top Level PFD Softkeys (optional) (optional) (optional) PRECIP or DL LTNG (optional) or METAR STRMSCP TRFC-1 ALERTS Select the BACK Softkey to return to the top-level softkeys. Hazard Avoidance TRFC-2 Displays Inset Map in PFD lower left corner Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except the active flight plan 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 115 Index DCLTR (3) Appendix Removes Inset Map Annun/Alerts OFF Additional Features Inset Map Softkeys INSET Procedures (optional) (optional) Flight Planning ALERTS Nav/Com/ XPDR/Audio Flight Instruments Appendix TRAFFIC Displays traffic information on Inset Map TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map Displays terrain information on Inset Map TERRAIN AFCS STRMSCP NEXRAD GPS Nav or Displays Worldwide Weather precipitation on Inset Map (optional) Displays XM lightning information on Inset Map (optional) PRECIP XM LTNG Flight Planning Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft) Displays NEXRAD weather and coverage information on Inset Map (optional) or Displays Worldwide Weather lightning information on Inset Map (optional) Procedures DL LTNG Hazard Avoidance ALERTS ADC2 AHRS1 AHRS2 BACK ALERTS Select the BACK Softkey to return to the top level softkeys. Sensor Softkeys ADC1 Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers Selects the #1 Air Data Computer ADC2 Selects the #2 Air Data Computer AHRS1 Selects the #1 AHRS AHRS2 Selects the #2 AHRS SENSOR Index Appendix Annun/Alerts Additional Features ADC1 116 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix DME ALERTS ALT UNIT HSI FMT Flight Instruments SYN VIS ALERTS Nav/Com/ XPDR/Audio Select the BACK Softkey to return to the top-level softkeys AFCS 360 HSI IN ALERTS HPA ALERTS PATHWAY SYN TERR HRZN HDG APTSIGNS ALERTS Procedures PFD Configuration Softkeys Hazard Avoidance SYN VIS PATHWAY APTSIGNS 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Index 190-00929-02 Rev. A Appendix HRZN HDG Displays compass heading along the Zero-Pitch line Annun/Alerts SYN TERR Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Additional Features Displays second-level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features PFD Flight Planning ALERTS GPS Nav METERS BACK ARC HSI 117 Appendix Flight Instruments DFLTS Nav/Com/ XPDR/Audio OPTN 1 AFCS WIND Resets PFD to default settings, including changing units to standard Displays softkeys to select wind data parameters Wind direction arrow and speed OPTN 3 Wind direction arrow with digital direction and speed Longitudinal and lateral components OFF Information not displayed OPTN 2 Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS/ waypoint identifier and GPS-derived distance information, and ADF/ Flight Planning GPS Nav DME BRG1 frequency. Procedures HSI FRMT 360 HSI ARC HSI Hazard Avoidance BRG2 Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS/ waypoint identifier and GPS-derived distance information, and ADF/ Additional Features frequency. Annun/Alerts ALT UNIT Index Appendix METERS STD BARO 118 Displays softkeys for setting the altimeter and BARO settings to metric units When enabled, displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals Sets barometric pressure to 29.92 in Hg (1013 hPa) Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix ALERTS Select the BACK Softkey to return to the top-level softkeys. Transponder Softkeys Flight Planning XPDR2 Selects the #2 transponder as active STBY Selects Standby Mode (transponder does not reply to any interrogations) Selects Mode A (transponder replies to interrogations) Selects Mode C – Altitude Reporting Mode (transponder replies to identification and altitude interrogations) Manually selects Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations. Annun/Alerts GND Additional Features ALT Hazard Avoidance ON Procedures XPDR1 Displays transponder mode selection softkeys Selects the #1 transponder as active XPDR GPS Nav Select the BACK Softkey to return to the previous level softkeys. AFCS ALERTS Nav/Com/ XPDR/Audio ADS-B TX Flight Instruments ALERTS Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 119 Appendix Removes numbers entered, one at a time Flight Instruments Nav/Com/ XPDR/Audio TMR/REF Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Activates/deactivates transmission of the aircraft’s three-dimensional position and aircraft heading for reception by ADS-B systems. Displays Timer/References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window AFCS IDENT ADS-B TX GPS Nav Flight Planning BKSP CODE MFD Navigation Page Softkey Map (optional) Hazard Avoidance Procedures 0—7 Automatically enters the VFR code (1200 in the U.S.A. only) Displays transponder code selection softkeys 0-7 Use numbers to enter code VFR DCLTR MAP SHW CHRT CHKLIST DCLTR-1 Additional Features DCLTR-2 Annun/Alerts DCLTR-3 TRAFFIC PROFILE TOPO (optional) TERRAIN AIRWAYS (optional) STRMSCP Select the BACK Softkey on this level to return to the top softkey level. (optional) (optional) PRECIP or NEXRAD DL LTNG or XM LTNG BACK AIRWY ON Appendix AIRWY LO AIRWAY HI Index MFD Softkeys 120 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix TRAFFIC Flight Instruments Enables second-level Navigation Map softkeys MAP Displays traffic information on Navigation Map Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map TOPO Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except the active flight plan When available, displays optional airport and terminal procedure charts When available, displays optional checklists Appendix Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Annun/Alerts 190-00929-02 Rev. A Displays Worldwide Weather lightning information on the Navigation Map (optional) Returns to top-level softkeys Additional Features CHKLIST Hazard Avoidance SHW CHRT Procedures DCLTR (3) Flight Planning BACK GPS Nav DL LTNG AFCS Displays Worldwide Weather precipitation on the Navigation Map (optional) XM LTNG Displays XM lightning information on the Navigation Map (optional) or PRECIP Nav/Com/ XPDR/Audio AIRWAYS Displays airways on the map; cycles through the following: AIRWAYS: No airways are displayed AIRWY ON: All airways are displayed AIRWY LO: Only low altitude airways are displayed AIRWY HI: Only high altitude airways are displayed STRMSCP Displays Stormscope weather and coverage information on Navigation Map (optional feature) NEXRAD Displays NEXRAD weather and coverage information on the Navigation Map (optional) or 121 Loading Updated Databases 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. If an error occurs during synchronization, an error message will be displayed, followed by the affected display in the Sync Status section of the Database Window. If synchronization completes on one display, but an error occurs on another, the error message will be displayed with the affected diaplays listed after it. When an error message is displayed, the problem must be corrected before synchronization can be completed. A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown. Error Message Description Canceled An active synchronization has been canceled using the SYNC DBS Softkey Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed-out prior to the database transfer completing Loading Garmin Database Updates Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Appendix 122 1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD. 2) Update the Garmin databases on the MFD card. 3) Insert the MFD database card into the bottom card slot of the MFD. 4) Apply power to the system, check that the databases are initialized and displayed on the power-up screen. When updating the terrain and FliteCharts databases, a ‘Verifying’ message may be seen. If this message is present, wait for the system to finish loading before proceeding to step 5. 5) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 6) Turn the large FMS Knob to select the AUX Page group on the MFD. 7) Turn the small FMS Knob to select the System Status Page. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix Make sure the SYNC DBS Softkey is in the enabled state. 9) Monitor the Sync Status in the Database Window. Wait for all databases to complete synching, indicated by ‘Complete’ being displayed. Nav/Com/ XPDR/Audio 10) Remove and reapply power to the system. Flight Instruments 8) 11) Turn the large FMS Knob to select the AUX Page group on the MFD. 12) Turn the small FMS Knob to select the System Status Page. GPS Nav Loading the Jeppesen Navigation Database as the Active Navigation Database AFCS 13) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct database cycle information is shown for each database for each display. Procedures NOTE: After the navigation database is loaded or copied, the top SD card may be removed. Flight Planning NOTE: Loading the Jeppesen navigation database as the active database prior to its effective date will result in the expiration date on the power-up screen and the effective date on the AUX-System Status Page being displayed in yellow. With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated (label of SD card facing left). Hazard Avoidance 2) Turn the system ON. A prompt similar to the following is displayed in the upper left corner of the display: Additional Features 3) 4) Press the NO Softkey to proceed to loading the active database. A prompt similar to the following is displayed. Press the YES Softkey to update the active navigation database. 5) After the update completes, the display starts in normal mode. 6) Turn the system OFF and remove the SD card from the top card slot. 7) Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD). 8) Apply power to the system and press the ENT Key to acknowledge the startup screen. 9) Turn the large FMS Knob to select the AUX Page group on the MFD. Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix 190-00929-02 Rev. A Annun/Alerts 1) 123 Appendix 11) Press the Display Database Selection Softkey to show active navigation database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct active navigation database cycle information is shown for each display. Loading the Jeppesen Navigation Database as the Standby Navigation Database AFCS Nav/Com/ XPDR/Audio Flight Instruments 10) Turn the small FMS Knob to select the System Status Page. 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the MFD. 2) Verify that an SD card is inserted in the bottom slot of each PFD and the MFD. 3) Turn the system ON. A prompt screen is displayed. 4) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the MFD. 5) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. 6) Press the ENT Key to acknowledge the startup screen. Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav NOTE: After the navigation database is loaded or copied, the top SD card may be removed. Appendix Annun/Alerts NOTE: During the synchronization process, version differences between standby navigation databases will exist. This will result in the system displaying a ‘DB Mismatch’ alert for the standby navigation databases. This alert will remain until the next power cycle. 7) Turn the large FMS Knob to select the AUX Page group on the MFD. 8) Turn the small FMS Knob to select the System Status Page. 9) If necessary, press the SYNC DBS Softkey to enable database synchronization. A confirmation box is displayed. If Database Synchronization has been enabled prior to this step, proceed to step 11. Index 10) With YES highlighted, press the ENT Key. 124 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Appendix Nav/Com/ XPDR/Audio 12) Turn system power OFF. Flight Instruments 11) The new database is copied to the SD card in bottom card slot of each PFD. Progress can be monitored in the SYNC STATUS field. When copying is finished, ‘Complete’ is displayed. 13) Remove the SD card from the top card slot of the MFD. 14) Turn system power ON. 15) Press the ENT Key to acknowledge the startup screen. AFCS 16) Turn the large FMS Knob to select the AUX Page group on the MFD. 17) Turn the small FMS Knob to select the System Status Page. 2) Turn the small FMS Knob to select the System Status Page. 3) Press the SYNC DBS Softkey (if needed) to disable automatic database synchronization. 4) Acknowledge the cancellation by pressing the ENT Key. Additional Features The SYNC DBS Softkey on the AUX–System Status Page allows enabling and disabling the automatic database synchronization feature. If the SYNC DBS Softkey is pressed while a database synchronization is in progress, the current synchronization process will be canceled. Hazard Avoidance Turn the large FMS Knob to select the AUX Page group on the MFD. Procedures 1) Flight Planning Canceling Database Synchronization GPS Nav 18) Press the Display Database Selection Softkey to show standby navigation database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct standby navigation database cycle information is shown for each display. Annun/Alerts Appendix Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 125 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Appendix Blank Page 126 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Index D Nav/Com/ XPDR/Audio Database synchronization 125 Data reports 79, 80 DCLTR Softkey 60 Declutter 115, 121 Direct-to 13 DME 5, 6 AFCS E GPS Nav Edit a flight plan 28 ESP 83, 84 F Flight Planning FD 87 Flight Director 9 Flight path marker 59 FliteCharts® 60, 61 Frequency Transfer 6 Procedures Hazard Avoidance G Gain 57 Garmin Flight Data Services 79 Additional Features Access code 64 Activate a flight plan 14 Active Channel 81 Active database 123 Active Navigation Database 123 ADF 5, 6, 118 ADS-B 120 Advisory alerts 85 AHRS 104, 105, 106, 108, 109 Air Data Computer 86 Airport Signs 59, 60 Airways 121 Alert messages 107 ALT 51 Altitude mode 51 Altitude volume 51 Antenna stabilization 58 Antenna tilt 56 AOPA’s Airport Directory 62 AP 87 Attitude & Heading Reference System 86 Audio panel controls NAV1, NAV2 6 Code selection softkeys 5 COM 5, 6 Flight Instruments A H Barometric Altitude Minimums 3 Barometric pressure 118 Bearing line 57, 58 HF 5, 6 Horizon heading 59 Horizontal scan 57 C I CDI 1, 2, 6, 111 Cell 35, 36 Cell mode 36 Channel Presets 82 ChartView 60, 61 CLD TOP Softkey 45 Inhibit 55 Inhibit TAWS 55 Inset Map 115, 116 IOI 88, 89, 92 Iridium satellite network 63, 64, 68 Index-1 Index Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series Appendix 190-00929-02 Rev. A Annun/Alerts B Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Index J Jeppesen 61 L R Level Mode 83 Lightning 35, 36, 116 Low speed data 63, 64 RADIO softkey 81 Register 63, 64 Report transmissions 79 ROC 88, 92 M S Map panning 37 Message advisories 95–106, 108–113 MET 87 METAR 37 Minimums 94 MISCOMP 86 Mistrim 87 Mode S 119 Mode selection softkeys 5 Multi Function Display (MFD) Softkeys 120 SafeTaxi® 60 SBAS 10, 32, 55, 101, 102 Sector scan 58 Sensor 86 SIGMET 46 STAB 58 Standby 56 Standby Navigation Database 99, 124 Store Flight Plan 27 Stormscope lightning data 35, 36, 116 Strike 35 Strike mode 36 SVS 59, 112 SVS Terrain 59 Synchronization 122, 125 Synthetic Vision System 59 System ID 63, 64 N NAV 6 NAV1 2, 6 NAV2 6 Navigation database 15, 16, 99, 114 NEXRAD 37, 38, 116, 121 NEXRAD Softkey 44 O OBS 2 Obstacles 99, 101 Overspeed Protection 10 P Index PIT 86 Predefined message 71, 72 Pathways 59, 60 PIREP 49 2 T TA 94 TAF 37, 47 TAS 51, 104 TAWS 52, 53, 54, 55, 88, 89, 90, 91, 93 TAWS-B 52, 54 Telephone 64 Terrain 52, 54, 88, 89, 91, 92, 99, 116, 121 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Index Flight Instruments Text message 70, 71, 73 Text messaging 69 Tilt line 56 Timer 109 Topographical data 116, 121 Traffic 35, 50, 116, 121 Traffic advisory 50 Traffic Advisory 94 Traffic Advisory (TA) 94 Traffic map page 50, 51, 52 Transponder 5, 119, 120 Nav/Com/ XPDR/Audio AFCS GPS Nav V Flight Planning Vertical speed guidance 16 Vertical track 94 VNV 13, 111 Vspeed 2 Procedures W Hazard Avoidance WATCH® 58 Waypoint Selection Submenu 24 Weather Attenuated Color Highlight 58 Weather data link page 37 Weather radar 56 Wi-Fi 76, 77, 78, 79, 80 Wind data 118 Winds Aloft 48 WIND Softkey 48 Additional Features Annun/Alerts X Appendix XM lightning 116, 121 XM Satellite Weather AIRMETs 46 SIGMETs 46 XM weather 37 XPDR Softkey 5 Index 190-00929-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 3 Index Appendix Annun/Alerts Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio Flight Instruments Index Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-02 Rev. A Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd Liberty House, Bulls Copse Road Hounsdown Business Park Southampton, SO40 9RB, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2008-2010 Garmin Ltd. or its subsidiaries 190-00929-02 Rev. A
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