Garmin | G1000: Beechcraft King Air 300/B300 | Garmin G1000: Beechcraft King Air 300/B300 G1000 Cockpit Reference Guide for KingAir 300/B300 Series - SSV 0985.08

Garmin G1000: Beechcraft King Air 300/B300 G1000 Cockpit Reference Guide for KingAir 300/B300 Series - SSV 0985.08
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Beechcraft 300/B300 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 © 2011 - 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.08 or later for the
Beechcraft 300 and B300. Some differences in operation may be observed when comparing
the information in this manual to earlier or later software versions.
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limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to licensee.
March, 2016
190-01344-02 Rev. B
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WARNING: Do not use outdated database information.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: Do not rely solely upon the display of traffic information for
collision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Warnings, Cautions & Notes
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be significantly older than the indicated weather
product age.
WARNING: Do not rely on information from the lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to the documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: The Garmin system, as installed in this 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.
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: 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Warnings, Cautions & Notes
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
300 and B300 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.
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
WARNING: Do not use the system to attempt to penetrate a thunderstorm.
The illustrations in this guide are only examples. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding any thunderstorm identified as severe of giving
intense radar echo by at least 20 miles.
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 (GRS 77 installations only). 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.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Warnings, Cautions & Notes
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.
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Warnings, Cautions & Notes
NOTE: When operating the G1000 in DG Free Mode (GRS 7800 installations
only), the heading information used by some system components (e.g. GTS
8000, AFCS, and GWX) will be different from the heading displayed on the
GDU by an amount equal to the difference between the current Magnetic
Field Variation Database (MV DB) value, and the MV DB value when DG Free
Mode was activated. Due to the convergence of isogonic lines, this condition
is most noticeable at or near the North and South poles.
NOTE: System navigation utilities may not reliably calculate range and bearing information when the aircraft is operating north of 80° North latitude or
south of 80° South latitude. This may result in the system displaying small
gaps in racetrack holding pattern depictions (GRS 7800 installations only).
NOTE: The Terrain Awareness and Warning System (TAWS) may not operate
reliably north of 89º North latitude and south of 89º South latitude. This is
due to limitations present within the Terrain database and the system’s ability
to process the data representing the affected areas (GRS 7800 installations
only).
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Warnings, Cautions & Notes
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory
and advisory guidance and information related to the use of databases in
the National Airspace System.
• Garmin equipment will only recognize and use databases that are
obtained from Garmin or Jeppesen. Databases obtained from Garmin
or Jeppesen are assured compliance with all data quality requirements
(DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A
copy of the Type 2 LOA is available for each database and can be viewed
at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established AFM(S) and regulatory guidance or
limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support to coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes;
or any other displayed item used for navigation or communication in the air
or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data
Error Report.’
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Record of Revisions
Part Number
190-01344-00
Rev A
Rev B
190-01344-01
190-01344-02
Rev. A
Change Summary
Initial release
Removed reference to TCAS II pitch attitude cue.
Added User Defined Holds
Removed Reports Page
Added temperature compensated altitude
Added DG Mode
Added Pilot Profiles
Added GRS 7800, GTS 8000, GTX 3000, GRA 5500
Changed Garmin Flight Data Services to Garmin Connext™
Added other GDU 13.06 parameters
Updated Softkey Map
Added GDU 13.31 parameters
Updated Support for SiriusXM Weather Service
Updated Warnings, Cautions, and Notes
Updated System Messages
Revision Date of Revision Affected Pages
B
March, 2016
All
190-01344-02 Rev. B
Description
Clerical
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Table of Contents
FLIGHT INSTRUMENTS................................................................................................................. 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Synchronize CDI......................................................................................................................... 1
Selecting DG Mode (GRS 7800 Installations Only)............................................................. 2
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs Individually...................................................................................... 3
Turn Vspeed Bugs On or Off by Category............................................................................. 3
Set Barometric/Radar Altimeter Minimum Descent Altitude.......................................... 3
Testing the Radar Altimeter.................................................................................................... 4
Displaying Wind Data............................................................................................................... 4
NAV/COM/TRANSPONDER/AUDIO PANEL.......................................................................... 5
ADF Tuning (Optional)............................................................................................................... 5
DME Tuning................................................................................................................................. 5
Enter a Transponder Code....................................................................................................... 5
Select Transponder Mode........................................................................................................ 5
Selecting a COM Radio............................................................................................................. 6
Selecting a NAV Radio.............................................................................................................. 6
NAV/COM Tuning........................................................................................................................ 6
Intercom....................................................................................................................................... 7
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 User Waypoint Defined by Latitude & Longitude............................................ 19
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
i
Table of Contents
Create a User Waypoint Defined by Radials from Other Waypoints............................ 20
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 22
Delete a User Waypoint.......................................................................................................... 23
Create a 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
Creating a User-Defined Hold at an Active Flight Plan Waypoint................................. 27
Creating a User-Defined Hold at the Aircraft Present Position..................................... 27
Creating a User-Defined Hold at a Direct-To Waypoint................................................... 28
Exiting a User-Defined Hold Inserted in the Active Flight Plan.................................... 28
Removing a User-Defined Hold Inserted in the Active Flight Plan............................... 29
Removing a User-Defined Hold at an Off-route Direct-to.............................................. 29
Invert An Active Flight Plan................................................................................................... 29
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 29
Store a Flight Plan................................................................................................................... 30
Edit a Stored Flight Plan........................................................................................................ 30
Delete a Waypoint from the Flight Plan............................................................................. 30
Invert and Activate a Stored Flight Plan............................................................................ 31
Copy a Flight Plan.................................................................................................................... 31
Delete a Flight Plan................................................................................................................. 32
Graphical Flight Plan Creation.............................................................................................. 32
Export a Flight Plan to an SD Card...................................................................................... 32
PROCEDURES.................................................................................................................................. 33
Load and Activate a Departure Procedure........................................................................ 33
Activate A Departure Leg...................................................................................................... 33
Load An Arrival Procedure..................................................................................................... 33
Activate An Arrival Leg.......................................................................................................... 34
Load and/or Activate an Approach Procedure.................................................................. 34
Activate An Approach in the Active Flight Plan................................................................ 35
Activate a Vector to Final Approach Fix............................................................................. 36
Activate A Missed Approach in the Active Flight Plan.................................................... 36
Temperature Compensated Altitude................................................................................... 36
HAZARD AVOIDANCE................................................................................................................. 39
Customizing the Hazard Displays on the Navigation Map............................................. 39
STORMSCOPE® (Optional)...................................................................................................... 39
SiriusXM Weather (Optional)................................................................................................ 41
Garmin Connext™ Weather.................................................................................................... 43
Traffic Avoidance Systems..................................................................................................... 53
Terrain Awareness & Warning System................................................................................ 57
Airborne Color Weather Radar............................................................................................. 60
ii
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Table of Contents
ADDITIONAL FEATURES............................................................................................................ 65
Synthetic Vision........................................................................................................................ 65
Terminal Procedure Charts.................................................................................................... 66
Airport Directory..................................................................................................................... 68
Satellite Telephone and Data Link Services...................................................................... 69
WI-FI Connections.................................................................................................................... 82
SiriusXM Radio Entertainment............................................................................................. 85
Pilot Profiles............................................................................................................................. 87
Electronic Stability & Protection (ESP™)............................................................................. 89
ANNUNCIATIONS & ALERTS.................................................................................................... 93
WARNING Annunciation......................................................................................................... 93
ADVISORY Annunciations....................................................................................................... 93
Message Advisory Alerts........................................................................................................ 93
Comparator Annunciations.................................................................................................... 94
Reversionary Sensor Annunciations.................................................................................... 94
AFCS Alerts................................................................................................................................ 95
TAWS-A Alerts........................................................................................................................... 96
TAWS-B Alerts........................................................................................................................... 99
Additional Voice Alerts......................................................................................................... 102
MFD & PFD Message Advisories......................................................................................... 103
Database Message Advisories............................................................................................ 105
GMA 1347D Message Advisories........................................................................................ 108
GIA 63W Message Advisories.............................................................................................. 109
GSD 41 Message Advisories (Optional)............................................................................. 113
GEA 71 Message Advisories................................................................................................. 113
GTX 33/33D/33ES/3000 Message Advisories..................................................................... 113
GRS 77/7800 Message Advisories....................................................................................... 114
GMU 44 Message Advisories............................................................................................... 116
GDL 59 Message Advisories................................................................................................. 116
GSR 56 Message Advisories................................................................................................. 117
GDL 69/69A/69 SXM Message Advisories......................................................................... 117
GWX 68/70 Message Advisories.......................................................................................... 117
GDC 74B/7400 Message Advisories.................................................................................... 118
GCU 477 Message Advisories.............................................................................................. 118
GMC 710 Message Advisories............................................................................................. 119
GTS 800/820/825/850/855/8000 Message Advisories...................................................... 119
GRA 5500 Message Advisories............................................................................................ 120
Miscellaneous Message Advisories.................................................................................... 120
Flight Plan Import/Export Messages................................................................................. 124
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
iii
Table of Contents
APPENDIX...................................................................................................................................... 127
PFD Softkey Map................................................................................................................... 127
MFD Navigation Page Softkey Map.................................................................................. 138
Loading Updated Databases............................................................................................... 139
INDEX..........................................................................................................................................Index-1
iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
Select the AUX-SYSTEM SETUP Page on the MFD.
Appendix
1)
1
SELECTING DG MODE (GRS 7800 INSTALLATIONS ONLY)
1)
Press the PFD Softkey.
2)
Press the HDG MODE Softkey.
3)
Press the DG FREE Softkey to activate DG mode. Press the DG SLAVE
Softkey to deactivate DG mode.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
•
Pressing the HDG- or HDG+ Softkey to slew the counterclockwise or
clockwise.
•
Pressing the HDG SYNC Softkey to sychronize the heading to the
current selected heading.
•
Pressing the TRACK SYNC Softkey to synchronize the heading to the
current track.
Flight
Planning
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.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
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.
GENERIC TIMER
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
1)
Procedures
CHANGE NAVIGATION SOURCES
2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Flight Instruments
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.
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
2)
CONFIGURE VSPEED BUGS INDIVIDUALLY
AFCS
GPS Nav
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
speed has been changed from a default value, an asterisk appears next to
the speed).
5)
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.
Procedures
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
Flight
Planning
4)
TURN VSPEED BUGS ON OR OFF BY CATEGORY
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.
Additional
Features
Press the TMR/REF Softkey.
Hazard
Avoidance
1)
SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE
Annun/Alerts
1) Press the TMR/REF Softkey.
3)
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘MINIMUMS’.
Appendix
2)
3
TESTING THE RADAR ALTIMETER
1)
Select the AUX-SYSTEM STATUS Page on the MFD.
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.
DISPLAYING WIND DATA
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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)
Flight
Planning
ENTER A TRANSPONDER CODE
Press the XPDR Softkey (XPDR/TFC if the TCAS II option is available).
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder. If these softkeys are not
present, proceed to step 3.
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)
Annun/Alerts
2)
Press the MODE Softkey to display the transponder mode selection
softkeys.
3)
Press the desired transponder mode softkey (STBY, ON, or ALT).
Appendix
Press the XPDR/TFC Softkey.
Additional
Features
With TCAS II Option
1)
Hazard
Avoidance
SELECT TRANSPONDER MODE
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
5
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
Flight
Instruments
Without TCAS II Option
1)
Press the XPDR Softkey.
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.
3)
Press the desired transponder mode softkey (STBY, ON, or ALT).
AFCS
SELECTING A COM RADIO
Transmit/Receive
GPS Nav
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
SELECTING A NAV RADIO
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
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.
Index
1)
Annun/Alerts
NAV/COM TUNING
Appendix
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Receive Only
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
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.
Flight
Instruments
INTERCOM
PASSENGER ADDRESS (PA) SYSTEM
Annun/Alerts
Appendix
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.
Additional
Features
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.
Hazard
Avoidance
CLEARANCE RECORDER AND PLAYER
Procedures
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.
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
7
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.
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
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
190-01344-02 Rev. B
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 300/B300 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 300/B300 Series
190-01344-02 Rev. B
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 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 300/B300 Series
190-01344-02 Rev. B
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
1)
3)
5)
7)
9)
11)
Direct-to Navigation from the PFD
2)
3)
5)
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 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 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 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 300/B300 Series
190-01344-02 Rev. B
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 300/B300 Series
17
Index
Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page
group.
Appendix
1)
190-01344-02 Rev. B
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 300/B300 Series
190-01344-02 Rev. B
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 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.
Appendix
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
Annun/Alerts
1)
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
19
Flight Planning
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
GPS Nav
AFCS
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 LAT/LON (latitude and longitude).
9)
Press the ENT Key.
Hazard
Avoidance
Procedures
Flight
Planning
CREATE A 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.
Additional
Features
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Appendix
Annun/Alerts
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/RAD (radial/radial).
9)
Press the ENT Key.
Index
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:
20
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Flight Planning
b) Turn the large FMS Knob to select the desired waypoint.
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Nav/Com/
XPDR/Audio
c) Press the ENT Key.
Flight
Instruments
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
AFCS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
GPS Nav
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
Procedures
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
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.
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.
Additional
Features
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Hazard
Avoidance
Or:
d) Press the ENT Key.
12) Press the ENT Key.
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.
Index
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Appendix
13) Repeat step 10 to enter the next waypoint name.
Annun/Alerts
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
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 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 300/B300 Series
190-01344-02 Rev. B
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 300/B300 Series
Appendix
Turn the large FMS Knob to select the ‘WPT’ page group.
Annun/Alerts
1)
190-01344-02 Rev. B
Flight
Planning
d) Press the ENT Key.
CREATE A FLIGHT PLAN
NOTE: When creating a 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 300/B300 Series
190-01344-02 Rev. B
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:
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 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 300/B300 Series
190-01344-02 Rev. B
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
CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The
HOLD AT window appears with the course field highlighted.
4)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
Procedures
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the Length mode highlighted.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
27
Index
2)
Appendix
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Annun/Alerts
1)
Additional
Features
CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION
Hazard
Avoidance
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
190-01344-02 Rev. B
Flight
Planning
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
GPS Nav
1)
3)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
4)
Use the FMS Knobs to edit the length, and press the ENT Key.
5)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
6)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
7)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate
the hold.
Press a Direct-to Key on the Control Unit and set up the Direct To
waypoint as desired, but select ‘HOLD?’ instead of ‘ACTIVATE?’ when
finished.
2)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
10) Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the Direct To
with the user-defined hold defined at the Direct To waypoint.
EXITING A USER-DEFINED HOLD INSERTED IN THE ACTIVE FLIGHT PLAN
Press the SUSP Softkey. The system will provide guidance to follow the
holding pattern to the inbound course and resume automatic waypoint
sequencing.
Index
Appendix
Annun/Alerts
Procedures
Flight
Planning
1)
Hazard
Avoidance
CREATING A USER-DEFINED HOLD AT A DIRECT-TO WAYPOINT
Additional
Features
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
28
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Flight Planning
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
Nav/Com/
XPDR/Audio
1)
3)
Press the ENT Key. The holding pattern is removed.
Procedures
Press the MENU Key to display the PAGE MENU with the cursor on the
‘Cancel Direct-To NAV’ selection.
Flight
Planning
2)
INVERT AN ACTIVE FLIGHT PLAN
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.
Additional
Features
Press the FPL Key to display the active flight plan.
Hazard
Avoidance
1)
Appendix
Press the FPL Key on the Control Unit to display the active flight plan. Press
the FMS Knob to activate the cursor.
Annun/Alerts
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
1)
GPS Nav
Press a Direct To Key to display the DIRECT TO Window (PFD or MFD).
AFCS
REMOVING A USER-DEFINED HOLD AT AN OFF-ROUTE DIRECT-TO
1)
Flight
Instruments
REMOVING A USER-DEFINED HOLD INSERTED IN THE ACTIVE FLIGHT PLAN
Or:
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
29
Flight Planning
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
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.
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.
STORE A FLIGHT PLAN
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.
Additional
Features
Annun/Alerts
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)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or:
Index
Appendix
1)
EDIT A STORED FLIGHT PLAN
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
2)
AFCS
d) Select the EDIT Softkey.
30
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Flight Planning
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
d) Select the EDIT Softkey.
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.
Flight
Planning
INVERT AND ACTIVATE A STORED 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 desired flight plan.
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.
Procedures
1)
Additional
Features
Annun/Alerts
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.
Appendix
1)
31
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Hazard
Avoidance
COPY A FLIGHT PLAN
190-01344-02 Rev. B
GPS Nav
Turn the large FMS Knob to highlight the waypoint to be deleted.
AFCS
2)
DELETE A FLIGHT PLAN
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.
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.
Press the FPL Key on the Control Unit to display the Active Flight Plan Page.
2)
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.
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.
EXPORT A FLIGHT PLAN TO AN SD CARD
Index
Appendix
Annun/Alerts
Procedures
Flight
Planning
1)
Hazard
Avoidance
GRAPHICAL FLIGHT PLAN CREATION
Additional
Features
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Planning
32
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
33
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.
AFCS
10) With ‘LOAD?’ highlighted, press the ENT Key.
11) The arrival will become part of the active flight plan.
ACTIVATE AN ARRIVAL LEG
Procedures
Flight
Planning
GPS Nav
Turn the large FMS Knob to highlight the desired arrival.
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
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.
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
4)
34
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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,
optional RAD ALT, or TEMP COMP.
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.
GPS Nav
Press the ENT Key. The cursor moves to the MINIMUMS field.
AFCS
7)
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
6)
10) Press the ENT Key. If BARO, RAD ALT, or OFF was selected step 8, proceed
to step 11. If TEMP COMP was selected in step 8, the cursor moves to the
‘TEMP AT....” field. Turn the small FMS Knob to enter the temperature at
the destination airport. The temperature compensated altitude minimum is
displayed below the previously enter minimum altitude value.
Flight
Planning
11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
Procedures
12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Hazard
Avoidance
Additional
Features
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 activates the
first leg of the approach.
13) Press the ENT Key.
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Appendix
1)
Annun/Alerts
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
35
ACTIVATE A VECTOR TO FINAL APPROACH FIX
Nav/Com/
XPDR/Audio
Flight
Instruments
Procedures
1)
Press the PROC Key.
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.
GPS Nav
AFCS
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
1)
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.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Or:
5)
After activating the missed approach procedure, and the CDI has changed
to TERM mode sensitivity, another approach procedure may be loaded.
TEMPERATURE COMPENSATED ALTITUDE
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Press the go-around button.
Altitudes Displayed With
Temperature Compensation
Index
Appendix
Altitudes Displayed Without
Temperature Compensation
36
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Procedures
Flight
Instruments
Enable Temperature Compensated Altitude
From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Use the small FMS Knob to select the temperature at the <airport>. The
Nav/Com/
XPDR/Audio
1)
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
GPS Nav
5)
shown in the flight plan.
Flight
Planning
Disable Temperature Compensated Altitude
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
Procedures
Press the ENT Key. The temperature compensated altitude at the FAF
is cancelled.
Hazard
Avoidance
5)
AFCS
compensated altitude is computed as the temperature is selected.
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
37
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Procedures
Blank Page
38
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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 300/B300 Series
Index
1)
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
190-01344-02 Rev. B
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)
39
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.
40
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Displaying SiriusXM 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
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).
Procedures
Turn the large FMS Knob to select the WPT Page Group.
Flight
Planning
1)
Displaying Weather on the Weather Data Link Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Select the available softkeys to select the desired SiriusXM 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.
Hazard
Avoidance
1)
Annun/Alerts
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
SIGMETs, PIREPs or AIREPs.
3)
Press the ENT Key to display pertinent information for the selected product.
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.
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features
Map Panning Information – Weather Data Link Page
190-01344-02 Rev. B
Nav/Com/
XPDR/Audio
WARNING: Do not use data link weather information for maneuvering in, near,
or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
Flight
Instruments
SIRIUSXM WEATHER (OPTIONAL)
41
Hazard Avoidance
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
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.
Weather Products and Symbols
Weather Product
Symbol
Expiration Time
(Minutes)
Refresh Rate
(Minutes)
5 (U.S.)
10 (Canada)
Next-generation Radar
(NEXRAD)
30
Cloud Top
60
Echo Top
30
7.5
SiriusXM Lightning
30
5
Cell Movement
30
12
SIGMETs/AIRMETs
60
12
Meteorological Aerodrome
Report (METARS)
90
12
City Forecast
60
12
Surface Analysis
90
12
Freezing Levels
120
12
Winds Aloft
90
12
County Warnings
60
5
42
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
15 (69/69A)
30 (69/69A SXM)
190-01344-02 Rev. B
Hazard Avoidance
90
22
Pilot Weather Report
(PIREPs)
90
12
Air Report (AIREPs)
90
12
Turbulence
180
12
no product image
30
5
no product image
60
12
no product image
60
12
Radar Coverage
Temporary Flight
Restrictions
Terminal Aerodrome
Reports
Procedures
Icing Potential (CIP and
SLD)
Flight
Planning
12
GPS Nav
60
AFCS
Cyclone Warnings
Nav/Com/
XPDR/Audio
Refresh Rate
(Minutes)
Symbol
Flight
Instruments
Expiration Time
(Minutes)
Weather Product
1)
Appendix
Accessing Garmin Connext Weather Products
Turn the large FMS Knob to select the Map Page Group.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
43
Index
2) Turn the small FMS Knob to select the Connext Weather Data Link Page.
When a weather product is selected for display on the Connext Weather Data Link
Page, a box containing a symbol for the product and its age (in minutes) are shown
190-01344-02 Rev. B
Annun/Alerts
Weather data are provided when the pilot initiates either a manual or automatic
Garmin Connext™ data request on the Connext Weather Data Link Page on the MFD.
No weather data is displayed until the first Garmin Connext Weather Data Request is
made.
Additional
Features
WARNING: Do not use data link weather information for maneuvering in, near,
or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
Hazard
Avoidance
GARMIN CONNEXT™ WEATHER
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
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 Garmin Connext 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.
Weather Product
Symbol
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)
Expiration
Time
(Minutes)
Refresh Rate
(Minutes)
30
U.S./Canada: 3*
Europe: 15
60
30
30
Continuous
60
Continuous
90
Continuous
60
Continuous
90
Continuous
60
Continuous
60
Continuous
* The composite precipitation image is updated every 3 minutes, but individual radar sites may take
between 3 and 10 minutes to provide new data.
44
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Hazard Avoidance
Flight
Instruments
Setting Up and Customizing the Connext 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 Connext Weather Data
Link Page with the changed settings.
AFCS
Select the Connext Weather Data Link Page.
Nav/Com/
XPDR/Audio
1)
GPS Nav
Procedures
Garmin Connext Weather
Product
Precipitation
Next-generation Radar
(NEXRAD)
(PRECIP)
Cloud Top
Infrared Satellite
(CLD TOP)
(IR SAT)
SiriusXM Lightning
Connext 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)
Flight
Planning
On aircraft equipped with both Garmin Connext and SiriusXM Weather services,
customizing the display settings for the corresponding weather products shown in
following table will result in identical settings for both services.
SiriusXM Weather Product
Additional
Features
Annun/Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Hazard
Avoidance
190-01344-02 Rev. B
45
Hazard Avoidance
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Press the MENU Key.
5)
Highlight the desired default(s) to restore (all or for selection) and press
ENT Key.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Restoring Default Connext Weather Data Link Page Settings
Procedures
Flight
Planning
GPS Nav
Switching Between Garmin Connext and SiriusXM Weather Sources
1)
Turn the large FMS Knob on the MFD to select the MAP page group.
2)
Turn the small FMS Knob to select the Connext (or XM) Weather Data Link
Page.
3)
Press the MENU Key.
4)
Turn the large FMS Knob to select ‘Display Connext Weather’ or ‘Display
XM Weather’ (choice dependent on current weather source) and press the
ENT Key.
Hazard
Avoidance
Viewing Legends for Displayed Connext Weather Products
1)
Select the Connext Weather Data Link Page.
2)
Select the LEGEND Softkey to display the legends for the displayed
weather products.
Additional
Features
Or:
a) Press the MENU Key.
Appendix
Annun/Alerts
b) Select ‘Weather Legend’ and press the ENT Key.
3)
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.
Index
Setting Up and Customizing Weather Data for the Navigation Map
Page
46
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
Nav/Com/
XPDR/Audio
With ‘Map Setup’ highlighted, press the ENT Key.
AFCS
GPS Nav
Connext Weather Data Requests
Press the MENU Key.
3)
With ‘Connext 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
2)
Hazard
Avoidance
Select the Connext Weather Data Link Page.
Procedures
Requesting Connext Weather Data Manually
Flight
Planning
The Connext Data Request window provides the flight crew with the options to
define the requested weather coverage area(s), choose automatic weather update
intervals (if desired), and the ability to send or cancel weather data requests. The
window also displays the status of the Connext data request process.
1)
Flight
Instruments
3)
• PRESENT POSITION – Requests data based on current location.
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).
Annun/Alerts
• DESTINATION – Requests data based on active flight plan
destination (if the flight plan contains no destination, dashes ‘------” are
displayed.)
• WAYPOINT – Requests data based on any valid waypoint.
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
47
5)
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.
6)
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 Connext Data Link Page without requesting data.
During a Connext Data Request, the Request Status box displays “Processing...” and
the ‘CANCEL REQ’ button is highlighted. If desired, the Connext Data Request window
may be closed while the data request is processing by pressing the FMS Knob; the data
request will continue in the background. Connext 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 Connext Weather products within the selected
coverage area during an initial Connext 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.
Cancelling a Connext Weather Data Request in Progress
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Connext 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 Connext Weather Datalink Page.
Index
Appendix
Annun/Alerts
Enabling Automatic Connext Data Requests
48
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Connext 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Or:
Press the FMS Knob to return to the Connext Weather Data Link Page.
AFCS
Garmin Connext™ Weather Products
Nav/Com/
XPDR/Audio
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 Connext Data
Request.
Flight
Instruments
6)
Precipitation
Index
49
Appendix
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Annun/Alerts
190-01344-02 Rev. B
Additional
Features
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.
Hazard
Avoidance
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 Connext Weather Data Link Page. For
the Precipitation legend, select the LEGEND Softkey when Precipitation is selected
for display.
Procedures
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 Connext Weather Data Link Page.
2) Select the PRECIP Softkey.
Flight
Planning
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.
GPS Nav
NOTE: Precipitation data cannot be displayed at the same time as terrain.
Hazard Avoidance
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.
Displaying Cloud Tops information
1) Select the Connext Weather Data Link Page.
2) Select the IR SAT Softkey.
To display the Infrared Satellite legend, select the LEGEND Softkey when Infrared
Satellite data is selected for display.
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.
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 Connext Weather Data Link Page.
2) Select the DL LTNG Softkey.
To display the Datalink Lightning legend on the Weather Data Link Page, select the
LEGEND Softkey when Datalink Lightning is selected for display.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
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
50
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Appendix
Index
51
Annun/Alerts
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features
190-01344-02 Rev. B
Hazard
Avoidance
Displaying METAR and TAF text
1) On the Connext 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 Connext 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.
Procedures
METAR and TAF text are displayed on the Weather Information Page. TAF
information is displayed in its raw form when it is available.
Flight
Planning
NOTE: METAR information is only displayed within the installed aviation
database service area.
GPS Nav
METARs and TAFs
AFCS
To display the SIGMET and AIRMET legend, select the LEGEND Softkey when
SIGMETs and AIRMETs are selected for display.
Nav/Com/
XPDR/Audio
Displaying SIGMETs and AIRMETs
1) Select the Connext 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.
Flight
Instruments
SIGMETs and AIRMETs
The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring
within the coverage area of the Connext data request.
3)
Use the FMS Knob to enter the desired airport and press the ENT Key.
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 Connext 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.
Procedures
Hazard
Avoidance
Additional
Features
Press the FMS Knob to display the cursor.
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.
To display the METAR legend on the Connext Weather Data Link Page, select the
LEGEND Softkey when METARs are selected for display.
To display the Winds Aloft legend, select the LEGEND Softkey when Winds Aloft
is selected for display.
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).
Displaying PIREP text
1) Select the Connext 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.
Index
Appendix
Annun/Alerts
2)
4)
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
52
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
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 Connext Weather Data Link Page.
To display the PIREP or AIREP legend, select the LEGEND Softkey when PIREPs
or AIREPs are selected for display.
Nav/Com/
XPDR/Audio
Press the ENT Key. The PIREP tex is first displayed in a decoded fashion,
then as raw text.
Flight
Instruments
5)
AFCS
The PIREP color is determined by the type (routine or urgent).
TRAFFIC AVOIDANCE SYSTEMS
Hazard
Avoidance
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Procedures
Description
Flight
Planning
Traffic Symbol
GPS Nav
• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey will be displayed.
• If a Traffic Advisory System (TAS) or Traffic Collision Avoidance System (TCAS I)
is configured, a STANDBY, OPERATE or NORMAL, TEST, and ALT MODE
Softkey will be displayed.
• If a Traffic Collision Avoidance System (TCAS II) is configured, an REL, ABS,
TFC STBY, TA ONLY, TA/RA, TEST, and ALT RNG Softkey will be displayed.
Proximity Advisory (PA)(not available with TIS)
(intruder is within 5 nm and less than 1200’ vertical separation)
Additional
Features
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Annun/Alerts
Traffic Advisory Off Scale
Resolution Advisory (RA)(TCAS II only)
(Potential collision area is within 15 to 35 seconds)
Appendix
Resolution Advisory Off Scale (TCAS II only)
Traffic Symbol Description
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
53
Hazard Avoidance
Flight
Instruments
Traffic Information Service (TIS)
Nav/Com/
XPDR/Audio
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Procedures
Flight
Planning
GPS Nav
AFCS
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
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.
Hazard
Avoidance
Displaying Traffic on the Navigation Map
1)
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.
Additional
Features
Traffic Advisory System (TAS) or Traffic Collision Avoidance System
(TCAS 1, GTS 850/855 only) (Optional)
Index
Appendix
Annun/Alerts
System Self Test
54
1)
Set the range to 2/6 nm.
2)
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 Annunciations & 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Flight
Instruments
Displaying Traffic on the Traffic Map Page
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 800/820/825/850/855 only) to enable or
disable Flight ID displayed with the intruder information.
GPS Nav
2)
Flight
Planning
With the Navigation Map displayed, select the MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Procedures
Displaying Traffic on the Navigation Map
1)
System Test
3)
Select the TEST Softkey. A test pattern of traffic symbols is displayed on
the Traffic Page and inset map on the PFD. The VSI will display red with
a green climb indication from 0 to 2000 feet per min. The self test takes
approximately eight seconds to complete, after which a voice alert “TCAS
System Test OK” is heard. In the event the system test fails, a voice alert
“TCAS System Test Failed” is heard and a visual annunciation ‘TCAS FAIL’
appears on the PFD. In addition, a yellow visual annunciation ‘FAILED’
appears in the center of the Traffic Map Page.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
Turn the small FMS Knob to select the Traffic Map Page.
Appendix
2)
Annun/Alerts
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
NOTE: If the system is configured to use TIS or TAS, the optional TCAS II is
not available for use.
Hazard
Avoidance
Traffic Collision Avoidance System (TCAS II) (Optional)
1)
AFCS
Turn the large FMS Knob to select the Map Page Group.
Nav/Com/
XPDR/Audio
1)
55
Hazard Avoidance
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA/RA’ or
‘TA ONLY’ respectively, is displayed in the TCAS Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘TFC STBY’ will be displayed in the TCAS Mode field.
5)
Select the ABS (absolute) or REL (relative) Softkey to display intruder
altitude as an absolute altitude or an altitude relative to own aircraft
altitude.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Procedures
Flight
Planning
Changing the Altitude Range
1)
On the Traffic Page, select the ALT RNG Softkey.
2)
Select one of the following Softkeys:
ABOVE: Displays non-threat and proximity traffic from 9900 feet above the
aircraft to 2700 feet below the aircraft. Typically used during climb phase
of flight.
Hazard
Avoidance
NORMAL: Displays non-threat and proximity traffic from 2700 feet above
the aircraft to 2700 feet below the aircraft. Typically used during enroute
phase of flight.
Additional
Features
BELOW: Displays non-threat and proximity traffic from 2700 feet above the
aircraft to 9900 feet below the aircraft. Typically used during descent phase
of flight.
Annun/Alerts
UNREST (unrestricted): All traffic is displayed.
3)
To return to the Traffic Page, select the BACK Softkey.
1)
Ensure TCAS II system is operating. With the Navigation Map displayed,
select the MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Index
Appendix
Displaying Traffic on the Navigation Map
56
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Flight
Instruments
TERRAIN AWARENESS & WARNING SYSTEM
TAWS-A (Optional)
GPS Nav
NOTE: TAWS-A operation is only available when the system is configured for
a TAWS-A installation.
AFCS
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Nav/Com/
XPDR/Audio
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Manual System Test
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.
Procedures
While the TAWS-A Page is displayed, press the MENU Key.
Flight
Planning
1)
When all is in working order, “TAWS System Test, OK” is heard.
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.
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
Terrain/Obstacle Location
Appendix
190-01344-02 Rev. B
Color
Annun/Alerts
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
1)
Hazard
Avoidance
Displaying the TAWS-A Page
57
Hazard Avoidance
Nav/Com/
XPDR/Audio
Flight
Instruments
Enable/Disable Aviation Data
1)
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.
AFCS
Inhibiting/Enabling FLTA and PDA Alerting
1)
Select the TAWS-A Page.
2)
Select the TAWS INH Softkey to inhibit or enable TAWS-A (choice
dependent on current state).
Flight
Planning
GPS Nav
Overriding Flaps-based FIT Alerting
1)
Select the TAWS-A Page.
2)
Select the FLAP OVR Softkey.
Procedures
Inhibiting/Enabling GPWS Alerting
1)
Select the TAWS-A Page.
2)
Select the GPWS INH Softkey to inhibit or enable GPWS alerts (choice
dependent on current state).
Hazard
Avoidance
Inhibiting/Enabling GSD Alerting
Annun/Alerts
Additional
Features
NOTE: Only available during a GSD alert.
1)
Select the TAWS-A Page.
2)
Select or press the GS INH or GP INH Softkey to inhibit or enable GSD
alerts (softkey choice dependent on present GSD alert type).
TAWS-B
Appendix
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Index
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
NOTE: TAWS-B operation is only available when the system is configured for
a TAWS-B installation.
58
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
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.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
Manual System Test
When all is in working order, “TAWS System Test, OK” is heard.
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.
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.
Additional
Features
Red
Hazard
Avoidance
Terrain/Obstacle Location
Procedures
Color
Flight
Planning
Turn the large FMS Knob to select the Map Page Group.
GPS Nav
1)
AFCS
Display Terrain and Obstacles on the TAWS-B Page
Enable/Disable Aviation Data
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.
Annun/Alerts
1)
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
59
Index
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.
Appendix
TAWS Inhibit
Hazard Avoidance
Flight
Instruments
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
1)
Press the MENU Key.
2)
Turn the small FMS Knob to select ‘Inhibit TAWS’.
3)
Press the ENT Key.
AFCS
Nav/Com/
XPDR/Audio
Or:
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Flight
Planning
GPS Nav
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.
Procedures
Displaying Terrain and Obstacles on the Navigation Map
1)
With the Navigation Map displayed, select the MAP Softkey.
2)
Select the TERRAIN Softkey. Terrain and obstacles will now be displayed
on the map.
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.
Annun/Alerts
Additional
Features
Hazard
Avoidance
1)
Appendix
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.
Index
Displaying Weather on the Weather Radar Page
60
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
Or:
5)
Turn the Joystick to select the desired range.
6)
If desired, select the VERTICAL Softkey for vertical scanning.
AFCS
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.
GPS Nav
Adjusting Antenna Tilt
Annun/Alerts
Appendix
Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.
61
Index
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features
Vertically Scan a Storm Cell
190-01344-02 Rev. B
Hazard
Avoidance
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.
Procedures
Adjusting Antenna Bearing
Flight
Planning
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.
2)
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
4)
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
3)
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
1)
Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
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.
Procedures
Flight
Planning
GPS Nav
AFCS
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.
Additional
Features
Hazard
Avoidance
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.
Index
Appendix
Annun/Alerts
Sector Scan
62
1)
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Hazard Avoidance
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.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
Antenna Stabilization
Flight
Planning
Procedures
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.
GPS Nav
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.
AFCS
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.
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
63
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Hazard Avoidance
Blank Page
64
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
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Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
Hazard
Avoidance
Additional
Features
Annun/Alerts
Displaying SVT 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 Technology (SVT) functionality is offered as an optional
enhancement to the G1000 system.
SVT is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the primary flight display (PFD).
In addition to SVT enhancement to the PFD, the following features have been
added to the PFD:
AFCS
WARNING: Do not use SVT runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVT is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
65
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
66
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 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.
67
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.
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Change Day/Night View
1)
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)
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.
AIRPORT DIRECTORY
The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK
Airport Directory databases offer detailed information regarding services, hours of
operation, lodging options, and more.
Both Airport Directories are available for downloading at flygarmin.com. However,
copy only one of the databases to the Supplemental Data Card. The system cannot
recognize both databases simultaneously.
Index
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. Airport
Directory information is displayed on the right half of the display.
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
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Additional Features
AFCS
Operation of these features in the cockpit is accomplished through the AUXTELEPHONE, AUX-TEXT MESSAGING, AUX-REPORT STATUS, and AUX-WIFI 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
Registering with Garmin Connext™
Hazard
Avoidance
2)
Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the
System ID number in the AIRFRAME field.
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)
Select ‘Register With Connext’ in the menu list.
7)
Press the ENT Key. The Garmin Flight Data Service Registration window is
now displayed.
8)
Enter the access code obtained from Garmin Connext in the ACCESS CODE
field.
Additional
Features
With the aircraft outside and having a clear view of the sky, turn the large
FMS Knob on the MFD to select the AUX page group.
Annun/Alerts
Appendix
69
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Procedures
1)
190-01344-02 Rev. B
Flight
Planning
Registering the system for datalink services
GPS Nav
A subscriber account must be established for each Iridium transceiver prior to
using the Iridium Satellite System for telephone services. Before setting up an Iridium
account, obtain the serial number of the Iridium Transceiver (GSR1) and the System
ID by selecting the AUX- SYSTEM STATUS Page. Contact Garmin at 1-866-739-5687
in the United States or 913-397-8200, ext. 1135.
After a subscriber account has been established, the system must be registered for
datalink features such as reporting services or Garmin Connext Weather. Registration
is accomplished by entering the required access code. This process is only performed
when initially setting up the system for Connext services.
Additional Features
Disable/Enable Iridium Transceiver
Iridium telephone and data communications may be turned on or off by performing
these simple steps.
Disable/Enable Telephone and Low Speed Data Services:
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
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.
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.
3)
If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page.
Index
Appendix
Annun/Alerts
Press the ENT Key. REGISTER will now be highlighted.
10) Press the ENT Key. System registration is complete when ‘REGISTERED’ is
displayed in the STATUS field.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
9)
70
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
71
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
72
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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 300/B300 Series
Index
Select the HOLD Softkey again to resume the call.
190-01344-02 Rev. B
Procedures
To exit the call, select the HANGUP Softkey.
1)
Flight
Instruments
Outgoing Calls
73
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.
1) Select the TRANS Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’.
c) Press the ENT Key.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
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.
Making a Conference Call from the Cockpit
Hazard
Avoidance
1)
Select the CONF Softkey on the MFD.
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’.
2)
Press the ENT Key. The cursor now highlights the phone number entry
field.
3)
Enter the phone number as discussed earlier for making an external call on
the Iridium satellite network.
4)
Press the ENT Key. ‘OK’ is now highlighted.
5)
Press the ENT Key again to place the call.
Index
Appendix
Annun/Alerts
c) Press the ENT Key.
74
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
75
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.
76
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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)
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
77
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
78
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
79
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.
80
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
81
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.
82
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
83
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.
84
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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.
Nav/Com/
XPDR/Audio
1)
SIRIUSXM RADIO ENTERTAINMENT
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Flight
Planning
1)
GPS Nav
Selecting the XM Radio Page
AFCS
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
Procedures
Active Channel and Channel List
Hazard
Avoidance
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.
Selecting a Category
Additional
Features
Annun/Alerts
Appendix
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.
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
85
Additional Features
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.
Nav/Com/
XPDR/Audio
Flight
Instruments
Select an Available Channel within the Selected Category
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.
86
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Additional Features
Flight
Instruments
PILOT PROFILES
Creating a Profile
2)
Nav/Com/
XPDR/Audio
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
Press the ENT Key. A ‘Create Profile’ window is displayed.
AFCS
4)
5) Use the FMS Knob to enter a profile name up to 16 characters long and
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.
7)
Press the ENT Key.
Flight
Planning
6)
GPS Nav
press the ENT Key. Pilot profile names cannot begin with a blank as the
first letter.
Procedures
8) With ‘CREATE’ highlighted, press the ENT Key to create the profile
Or:
9)
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
Additional
Features
Selecting an Active Profile
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
Press the FMS Knob momentarily to activate the flashing cursor.
Annun/Alerts
2)
Hazard
Avoidance
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
3) Turn the large FMS Knob to highlight the active profile field in the Pilot
Profile Box.
Appendix
4) Turn the small FMS Knob to display the pilot profile list and highlight the
desired profile.
5) Press the ENT Key. The system loads and displays the system settings for
the selected profile.
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
87
Additional Features
Flight
Instruments
Renaming a Profile
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
Nav/Com/
XPDR/Audio
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
4)
Press the ENT Key.
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
AFCS
rename.
6)
Press the ENT Key.
GPS Nav
7) Use the FMS Knob to enter a new profile name up to 16 characters long
and press the ENT Key.
8) With ‘RENAME’ highlighted, press the ENT Key.
Flight
Planning
9)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Procedures
Deleting a Profile
1) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Hazard
Avoidance
3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
4)
Press the ENT Key.
5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to
Additional
Features
delete.
6)
Press the ENT Key.
7) With ‘DELETE’ highlighted, press the ENT Key.
Annun/Alerts
8)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Appendix
Importing a Profile
1)
Insert the SD card containing the Pilot Profile into the top card slot on the
MFD.
Index
2) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
3)
88
Press the IMPORT softkey. If the correct Pilot Profile file is selected; with
‘IMPORT’ highlighted press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Additional Features
Flight
Instruments
Or:
If the SD card contains more than one Pilot Profile:
Nav/Com/
XPDR/Audio
a) Turn the large FMS Knob to highlight the select file field in the Pilot
Profile Importing Box.
b) Turn the small FMS Knob to display the pilot profile list and highlight
the desired profile to import and press the ENT Key.
c) With ‘IMPORT’ highlighted, press the ENT Key.
AFCS
4)
“Pilot profile import succeeded.” is shown in the import results box. Press
the ENT Key. The imported profile becomes the active Pilot Profile.
1)
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
4)
Press the EXPORT softkey.
5)
With ‘EXPORT’ highlighted press the ENT Key.
6)
“Pilot profile export succeeded.” is shown in the export results box. Press
the ENT Key to exit the Pilot Profile Exporting Box.
Hazard
Avoidance
Activate the desired Pilot Profile to export. Only the active Pilot Profile can
be exported.
Index
89
Appendix
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Annun/Alerts
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo and/
or Mmo) 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
normal flight envelope. This is perceived by the pilot as resistance to control movement
in the undesired direction when the aircraft approaches a steep attitude or high airspeed.
As the aircraft deviates further from the normal attitude and/or airspeed range continues
to increase, the force increases (up to an established maximum) to encourage control
movement in the direction necessary to return to the normal 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.
Additional
Features
ELECTRONIC STABILITY & PROTECTION (ESP™)
190-01344-02 Rev. B
Procedures
3)
Flight
Planning
2) Use the FMS Knob to select the AUX - SYSTEM SETUP 1 Page.
GPS Nav
Exporting a Profile
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 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.
Turn the large FMS Knob to select the AUX Page Group.
Flight
Planning
2)
Turn the small FMS Knob to select the System Setup Page.
3)
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.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
6)
Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7)
Press the FMS Knob to remove the cursor.
Index
Appendix
Annun/Alerts
Additional
Features
1)
Procedures
To enable or disable ESP:
Hazard
Avoidance
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°.
90
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Additional Features
GPS Nav
Flight
Planning
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.
AFCS
High Airspeed Protection
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
Pitch Engagement
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
91
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Additional Features
Blank Page
92
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
WARNING ANNUNCIATION
Alerts Window
Text
Aural Alert
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
GPS Nav
ADVISORY ANNUNCIATIONS
AFCS
“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.
Nav/Com/
XPDR/Audio
Annunciation
Window Text
UNDERSPEED
PROTECT ACTIVE
PFD FAN FAIL - PFD #2 cooling fan is inoperative.
Hazard
Avoidance
MESSAGE ADVISORY ALERTS
Alerts Window Message
Additional
Features
ESP DEGRADE – ESP AOA mode is inoperative.*
ESP DEGRADE – ESP IAS mode is inoperative.*
ESP FAIL – ESP is inoperative.*
ESP OFF – ESP selected off.*
ESP CONFIG – ESP config error. Config service req’d.*
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.
Annun/Alerts
Appendix
Index
* Available with ESP™ option only
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
93
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
94
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 300/B300 Series
190-01344-02 Rev. B
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
Yaw axis control failure.
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
Hazard
Avoidance
Yaw Damper/
Rudder Boost
Failure
Elevator Mistrim
Up
AFCS
AFCS ALERTS
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.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
Preflight system test has failed.
Appendix
Aileron Mistrim
Left
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
95
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
Voice Message
Excessive Descent Rate
Warning (EDR)
Appendix
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
96
“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 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
or
Voice 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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
97
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
Voice
Message
98
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
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 300/B300 Series
99
Index
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
Appendix
or
Voice Message
Annun/Alerts
MFD Map Page
Pop-Up Alert
Reduced Required Terrain
Clearance Warning (RTC)
190-01344-02 Rev. B
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
Voice 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
100
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Voice
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
101
ADDITIONAL VOICE ALERTS
Voice Alert
“Minimums”
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
The aircraft has descended below the preset minimum
descent altitude or decision altitude.
The aircraft is one minute from Top of Descent. Issued only
when vertical navigation is enabled.
“Airspeed”
The aircraft is in an underspeed condition. See the AFCS
section for more details.
“Engaging autopilot”
The ESP system is engaging the autopilot. See the AFCS
section for more details.
“Traffic”
Played when a Traffic Advisory (TA) is issued with the
TIS system, the optional GTS 800/820/825 TAS system,
or the optional GTS 850/855 TCAS I system. See the
Hazard Avoidance section for additional details on GTS
820/825/850/855 voice alerts.
“TIS Not Available”
The aircraft is outside the Traffic Information Service (TIS)
coverage area.
“Traffic, Traffic”
Played when a Traffic Advisory (TA) is issued with the
optional SKY 497/SKY899 TAS system, or the optional KTA
870 TAS system. See the Skywatch PG or KTA 870 PG for
additional details on voice alerts.
Played for each subsequent TA (KTA 870 only).
“Traffic”
Played when the optional traffic system passes a pilotinitiated self test.
“Traffic Advisory System Test Passed” - SKY 497 TAS
- SKY 899 TAS
“SKYWATCH System Test Passed”
- KTA 870 TAS
“TAS System Test OK”
- GTS 800/820/825 TAS
“TAS System Test Passed”
- GTS 850 TCAS I
“TCAS System Test Passed”
- GTS 855 TCAS I
“TCAS One System Test Passed”
- GTS 8000 TCAS II
“TCAS Two System Test Passed”
- TCAS II
“TCAS System Test Passed”
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
“Vertical track”
Description
102
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Description
GPS Nav
Intruder relative altitude (GTS 800/820/825/850/855 only)
Procedures
“Less than one mile”,
Intruder distance (GTS 800/820/825/850/855 only)
“One Mile” through “Ten Miles”, or
“More than ten miles”
Annun/Alerts
Appendix
Index
103
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Hazard
Avoidance
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.
190-01344-02 Rev. B
Flight
Planning
“High”, “Low”, “Same Altitude” (if
within 200 feet of own altitude), or
“Altitude not available”
Intruder bearing (GTS 800/820/825/850/855 only)
AFCS
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
Nav/Com/
XPDR/Audio
Played when the optional traffic system fails a pilot-initiated
self test.
“Traffic Advisory System Test Failed” - SKY 497 TAS
- SKY 899 TAS
“SKYWATCH System Test Failed”
- KTA 870 TAS
“TAS System Test Fail”
- GTS 800/820/825 TAS
“TAS System Test Failed”
- GTS 850/855 TCAS I
“TCAS One System Test Failed”
- GTS 8000 TCAS II
“TCAS Two System Test Failed”
- TCAS II
“TCAS System Test Failed”
Flight
Instruments
Voice Alert
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
PFD1 MANIFEST – PFD1 software
mismatch, communication halted.
PFD2 MANIFEST – PFD2 software
mismatch, communication halted.
MFD1 MANIFEST – MFD1
software mismatch, communication
halted.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
PFD2 CONFIG – PFD2 config error.
Config service req’d.
MFD1 CONFIG – MFD1 config
error. Config service req’d.
Comments
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system
should be serviced.
The MFD configuration settings do not match
backup configuration memory. The system
should be serviced.
PFD1 SOFTWARE – PFD1 mismatch,
communication halted.
PFD2 SOFTWARE – PFD2 mismatch, The specified GDU has different software versions
communication halted.
installed. The system should be serviced.
MFD1 SOFTWARE – MFD1
mismatch, communication halted.
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.
104
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
Flight
Planning
Comments
Procedures
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.
Hazard
Avoidance
Additional
Features
The MFD and/or PFD detected a failure in the
basemap database.
Annun/Alerts
Appendix
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
190-01344-02 Rev. B
GPS Nav
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.
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.
AFCS
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.
The PFD1, PFD2 and/or MFD backlight calibration
cannot be found or is invalid. The system should
be serviced.
Nav/Com/
XPDR/Audio
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Flight
Instruments
Message
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
[PFD1, PFD2, or MFD1] BKLT CAL
INV – calibration lost or mismatch.
Return for repair.
105
Message
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.
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.
Comments
The terrain database is present on another LRU,
but is missing on the specified LRU.
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.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
106
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
Flight
Instruments
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.
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
107
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
GPS Nav
190-01344-02 Rev. B
AFCS
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.
DB MISMATCH – Navigation
The PFDs and MFD have different navigation
database mismatch. Xtalk is off.
database versions or regions installed. Crossfill
is off. Check the AUX-SYSTEM STATUS Page
to determine versions or regions. Also, check
the AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Standby
The PFDs and MFD have different standby
Navigation database mismatch.
navigation database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to
determine versions or regions. Also, check the
AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
Nav/Com/
XPDR/Audio
Message
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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
Comments
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
DB MISMATCH – Airport Terrain
The PFDs and MFD have different airport terrain
database mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
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.
GMA 1347D MESSAGE ADVISORIES
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.
108
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
GPS Nav
Flight
Planning
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.
109
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Appendix
The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be
serviced.
Annun/Alerts
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Additional
Features
The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.
Hazard
Avoidance
190-01344-02 Rev. B
Procedures
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.
AFCS
The audio panel has incorrect software installed. The
system should be serviced.
Nav/Com/
XPDR/Audio
The audio panel configuration settings do not
match backup configuration memory. The system
should be serviced.
Flight
Instruments
Message
GMA1 CONFIG – GMA1 config
error. Config service req’d.
GMA2 CONFIG – GMA2 config
error. Config service req’d.
GMA1 MANIFEST – GMA1
software mismatch, communication
halted.
GMA2 MANIFEST – GMA2
software mismatch, communication
halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 SERVICE – GMA2 needs
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
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.
GIA1 MANIFEST – GIA1 software
mismatch, communication halted.
GIA2 MANIFEST – GIA2 software
mismatch, communication halted.
GFC MANIFEST – GFC software
mismatch, communication halted.
COM1 MANIFEST– COM1 software
mismatch, communication halted.
COM2 MANIFEST– COM2 software
mismatch, communication halted.
NAV1 MANIFEST– NAV1 software
mismatch, communication halted.
NAV2 MANIFEST– NAV2 software
mismatch, communication halted.
COM1 CONFIG – COM1 config
error. Config service req’d.
COM2 CONFIG– COM2 config
error. Config service req’d.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
110
Comments
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
A GIA mismatch has been detected, where only
one is SBAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
COM1 and/or COM2 software mismatch. The
G1000 system should be serviced.
NAV1 and/or NAV2 software mismatch. The
G1000 system should be serviced.
COM1 and/or COM2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
111
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
GPS Nav
190-01344-02 Rev. B
AFCS
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.
COM1 RMT XFR – COM1 remote The COM1 and/or COM2 transfer switch is stuck
transfer key is stuck.
in the enabled (or “pressed”) position. Press
COM2 RMT XFR – COM2 remote the transfer switch again to cycle its operation.
If the problem persists, the system should be
transfer key is stuck.
serviced.
RAIM UNAVAIL – RAIM is
GPS satellite coverage is insufficient to perform
not available from FAF to MAP
Receiver Autonomous Integrity Monitoring (RAIM)
waypoints.
from the FAF to the MAP waypoints.
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’.
Nav/Com/
XPDR/Audio
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.
Flight
Instruments
Message
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
GPS2 FAIL – GPS2 is inoperative.
Procedures
Flight
Planning
GPS Nav
AFCS
Message
GPS1 FAIL – GPS1 is inoperative.
Nav/Com/
XPDR/Audio
Annunciations & Alerts
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
UNABLE RNP – Estimated position
error exceeds RNP.
UNABLE RNP APR – GPS integerity
lost. Check GPS sensors.
APR ADVISORY – SBAS VNAV not
available. Using Baro VNAV.
Annun/Alerts
Additional
Features
Appendix
G/S2 FAIL – G/S2 is inoperative.
Index
Hazard
Avoidance
G/S1 FAIL – G/S1 is inoperative.
112
Comments
A failure has been detected in GPS receiver #1
and/or GPS receiver #2. The system should be
serviced.
A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be
available. The system should be serviced.
A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be
available. The system should be serviced.
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.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should
be serviced.
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.
The estimated GPS position error exceeds the RNP
limits. Check GPS sensors.
The estimated GPS position error exceeds the
requirements for the current approach. Check GPS
sensor
SBAS VNAV not available. Check GPS sensor.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
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.
GEA1 MANIFEST – GEA1 software The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GEA2 MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GPS Nav
GEA 71 MESSAGE ADVISORIES
AFCS
Comments
GSD1 and the CDU have different copies of
the GSD1 configuration.
GSD1 is reporting a low temperature
condition.
GSD1 is reporting an internal error condition.
The GSD may still be usable.
GSD1 has incorrect software installed. The
system should be serviced.
Nav/Com/
XPDR/Audio
Message
GSD1 CONFIG – GSD1 config error.
Config service req’d.
GSD1 COOLING – GSD1 temperature
too low.
GSD1 SERVICE – GSD1 needs service.
Return unit for repair.
GSD1 MANIFEST – GSD1 software
mismatch. Communication halted.
Flight
Instruments
GSD 41 MESSAGE ADVISORIES (OPTIONAL)
GTX 33/33D/33ES/3000 MESSAGE ADVISORIES
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
113
Index
The transponder has incorrect software installed.
The system should be serviced.
Appendix
190-01344-02 Rev. B
Comments
Annun/Alerts
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
GTX1 MANIFEST – GTX1 software
mismatch, communication halted.
GTX2 MANIFEST – GTX2 software
mismatch, communication halted.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
XPDR1 SERVICE – XPDR1 needs
service. Return unit for repair.
XPDR2 SERVICE – XPDR2 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is inoperative.
XPDR2 FAIL – XPDR2 is inoperative.
XPDR1 ADS-B FAIL – XPDR1 unable
to transmit ADS-B messages.
XPDR2 ADS-B FAIL – XPDR2 unable
to transmit ADS-B messages.
Comments
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.
ADS-B is inoperative. Other transponder functions
may be available. Transponder should be serviced
when possible
GRS 77/7800 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.
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.
114
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
115
AFCS
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Nav/Com/
XPDR/Audio
190-01344-02 Rev. B
Flight
Instruments
Message
Comments
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.
GRS1 MANIFEST – GRS1 software The #1 AHRS has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GRS2 MANIFEST – GRS2 software The #2 AHRS has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
AHRS1 SERVICE – AHRS1 needs
A failure has been detected in the #1 AHRS. The
service. Return unit for repair.
system should be serviced.
AHRS2 SERVICE – AHRS2 needs
A failure has been detected in the #2 AHRS. The
service. Return unit for repair.
system should be serviced.
AHRS1 CONFIG – AHRS1 config
AHRS configuration settings do not match those
error. Config service req’d.
of backup configuration memory. The system
should be serviced.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
AHRS2 CONFIG – AHRS2 config
error. Config service req’d.
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
AHRS2 CAL – AHRS2 calibration
version error. Srvc req’d.
Comments
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
The #1 AHRS calibration version error. The system
should be serviced.
The #2 AHRS calibration version error. The system
should be serviced.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
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.
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.
116
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
A failure has been detected in the GDL 59
router. The system should be serviced.
The GDL 59 is not registered with Connext,
or it’s current registration data has failed
authentication.
The GDL 59 has incorrect software installed.
The system should be serviced.
Flight
Instruments
Nav/Com/
XPDR/Audio
AFCS
Message
GDL59 RTR FAIL – The GDL 59
router has failed.
REGISTER CONNEXT – Data
services are inoperative, register w/
Connext.
MANIFEST – GDL software
mismatch, communication halted.
Comments
A failure has been detected in the #1 GSR 56.
The system should be serviced.
Flight
Planning
Message
GSR1 FAIL – GSR1 has failed.
GPS Nav
GSR 56 MESSAGE ADVISORIES
GDL 69/69A/69 SXM MESSAGE ADVISORIES
Comments
GDL 69/69A/69 SXM configuration settings
do not match those of backup configuration
memory. The system should be serviced.
A failure has been detected in the GDL
69/69A/69 SXM. The receiver is unavailable.
The system should be serviced
Hazard
Avoidance
GDL69 FAIL – GDL 69 has failed.
Procedures
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
117
Index
GWX FAIL – GWX is inoperative.
Comments
GWX 68/70 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 68/70 or the GWX 68/70 is reporting a fault.
The GWX 68/70 radar system should be serviced.
Appendix
Message
GWX CONFIG – GWX config error.
Config service req’d.
Annun/Alerts
GWX 68/70 MESSAGE ADVISORIES
Additional
Features
GDL69 MANIFEST – GDL 69
The GDL 69/69A/69 SXM has incorrect software
software mismatch, communication
installed. The system should be serviced.
halted.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Message
GWX SERVICE – GWX needs
service. Return unit for repair.
GWX MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Comments
A failure has been detected in the GWX 68/70.
The GWX 68/70 may still be usable.
The GWX 68/70 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.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
GDC 74B/7400 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.
ADC1 SERVICE – ADC1 needs
service. Return unit for repair
ADC2 SERVICE – ADC1 needs
service. Return unit for repair
GDC1 MANIFEST – GDC1 software
mismatch, communication halted.
GDC2 MANIFEST – GDC2 software
mismatch, communication halted.
Comments
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 GDC1 and/or GDC2 self-test has detected
a problem in the unit. The system should be
serviced
The GDC has incorrect software installed. The
system should be serviced.
GCU 477 MESSAGE ADVISORIES
Message
GCU CNFG – GCU Config error.
Config service req’d.
118
Comments
GCU 477 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Comments
Error in the configuration of the GMC 710.
Flight
Planning
Additional
Features
GTS 800/820/825/850/855/8000 MESSAGE ADVISORIES
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
119
Index
190-01344-02 Rev. B
Appendix
GTS MANIFEST – GTS software
mismatch, communication halted.
Comments
The GTS and GDU have incompatible
configurations. This alert is also set when the
GTS has an invalid mode S address configured or
the mode S address does not match both XPDR
mode S addresses.
The GTS has incorrect software installed. The
system should be serviced.
Annun/Alerts
Message
GTS CONFIG – GTS config error.
Config service req’d.
Hazard
Avoidance
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.
Procedures
GMC MANIFEST – GMC software
mismatch. Communication halted.
GMC KEYSTK – GMC [key name]
Key is stuck.
GPS Nav
Message
GMC CONFIG – GMC Config error.
Config service req’d.
GMC FAIL – GMC is inoperative.
AFCS
GMC 710 MESSAGE ADVISORIES
Nav/Com/
XPDR/Audio
GCU1 MANIFEST – GCU software
mismatch, communication halted.
GCU KEYSTK – GCU [key name]
Key is stuck.
Comments
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.
Flight
Instruments
Message
GCU FAIL – GCU is inoperative.
GRA 5500 MESSAGE ADVISORIES
Message
GRA1 CONFIG – GRA1 config
error. Config service req’d.
GRA1 SERVICE – GRA1 needs
service. Return unit for repair
GRA1 CAL – GRA1 calibration.
Service req’d.
GRA1 TEMP – GRA1 over
temperature.
GRA1 MANIFEST – GRA1
software mismatch, communication
halted.
The GRA has incorrect software installed. The
system should be serviced.
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Additional
Features
Annun/Alerts
FPL WPT MOVE – Flight plan
waypoint moved.
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.
The system has detected that a waypoint
coordinate has changed due to a new
navigation database update. Verify that stored
flight plans contain correct waypoint locations.
Index
Appendix
Comments
The GRA and GDU have incompatible
configurations.
The GRA self-test has detected a problem in the
unit. The system should be serviced.
GRA1 has improper calibration. The system
should be serviced.
The system has detected an over temperature
condition in GRA1.
MISCELLANEOUS MESSAGE ADVISORIES
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
120
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
121
AFCS
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Nav/Com/
XPDR/Audio
190-01344-02 Rev. B
Flight
Instruments
Message
Comments
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify user modified procedures.
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.
Message
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on CDI for
approach.
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.
VNV – Unavailable. Unsupported
leg type in flight plan.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
TRAFFIC FAIL – Traffic device has
failed.
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
122
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.
Bad parallel track geometry.
Invalid leg type for parallel offset.
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.
The system is no longer receiving data from
the traffic system. The traffic device should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Annun/Alerts
Appendix
Index
123
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Hazard
Avoidance
190-01344-02 Rev. B
Procedures
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
[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.
Flight
Planning
SCHEDULER [#] – <message>.
USER MAG VAR – User magnetic
variation is active.
GPS Nav
SVT – SVT DISABLED: Terrain DB
resolution too low.
AFCS
SVT – SVT DISABLED: Out of
available terrain region.
Nav/Com/
XPDR/Audio
STRMSCP FAIL – Stormscope has
failed.
FAILED PATH – A data path has
failed.
MAG VAR – Large magnetic
variance. Verify all course angles.
Comments
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to
the selected non-WGS84 waypoint.
Stormscope has failed. The G1000™ system
should be serviced.
A data path connected to the GDU or the GIA
63/W has failed.
The GDU’s internal model cannot determine
the exact magnetic variance for geographic
locations near the magnetic poles. Displayed
magnetic course angles may differ from the
actual magnetic heading by more than 2°.
Synthetic Vision is disabled because the aircraft
is not within the boundaries of the installed
terrain database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second
or better) is not currently installed.
Message criteria entered by the user.
User magnetic variation mode was selected
during previous operation and is still active
(checked at power-up.)
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
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.
Flight
Instruments
Message
NON WGS84 WPT – Do not use
GPS for navigation to [xxxx]
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Message
[PFD1, PFD2, or MFD1] CARD 1
ERR – Card 1 is invalid.
[PFD1, PFD2, or MFD1] CARD 2
ERR – Card 2 is invalid.
FPL TRUNC – Flight plan has been
truncated.
Comments
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.
This occurs when a newly installed navigation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
HOLD EXPIRED – Holding EFC time Expect Further Clearance (EFC) time has expired
expired.
for the User Defined Hold.
BARO MISMATCH – Correct baro
Altimeter setting is not the same on PFD1 and
mismatch for VNAV guidance.
PFD2. Synchronize settings for VNAV guidance.
TRN AUD FAIL – Trn Awareness
The audio source for terrain awareness is
audio source unavailable.
offline. Check GIA1 or GIA 2.
TERRAIN AUD CFG – Trn Awareness Terrain audio alerts are not configured properly.
audio config error. Service req’d.
The system should be serviced
TERRAIN DISABLED – Terrain
TAWS is disabled because a terrain database of
Awareness DB resolution too low.
sufficient resolution (9 arc-second or better) is not
currently installed.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
Annun/Alerts
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
Index
Appendix
‘Flight plan successfully imported.’
Description
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘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.
‘No flight plan files found to import.’
124
The SD card contains no flight plan data.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Annunciations & Alerts
Description
Flight
Instruments
Flight Plan Import/Export
Results
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.
Nav/Com/
XPDR/Audio
‘Flight plan import failed.’
‘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.
Flight
Planning
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.
GPS Nav
‘Some waypoints not loaded. Waypoints
locked.’
AFCS
‘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.
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
125
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Annunciations & Alerts
Blank Page
126
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
Nav/Com/
XPDR/Audio
ALERTS
AFCS
GPS Nav
Top Level PFD Softkeys
(optional TCAS II)
TRFC/MAP
XPDR/TFC
ALERTS
STRMSCP
(optional)
(optional)
PRECIP
or
DL LTNG
or
METAR
ALERTS
Select the BACK Softkey to return
to the top-level softkeys.
TRFC-2
Level 2
INSET or
TRFC/MAP
Pressing the INSET Softkey Displays Inset Map
in the PFD lower left corner. The TRFC/MAP
Softkey is displayed when the TCAS II option
is installed. Pressing the TRFC/MAP Softkey
displays the Inset Map showing Traffic Map Page.
Removes Inset Map
Appendix
OFF
Description
Annun/Alerts
Level 1
Additional
Features
Inset Map Softkeys
Hazard
Avoidance
TRFC-1
(optional)
Procedures
(optional)
Flight
Planning
(optional TCAS II)
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
127
Level 1
Level 2
Description
DCLTR (3) 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
WX LGND Displays icon and age on the Inset Map for the
selected weather products (optional)
TRAFFIC Displays traffic information on Inset Map
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Flight
Planning
TOPO
TERRAIN
Procedures
STRMSCP
NEXRAD
Hazard
Avoidance
or
PRECIP
Additional
Features
XM LTNG
or
Annun/Alerts
DL LTNG
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)
Displays Connext Weather precipitation on Inset
Map (optional)
Displays SiriusXM lightning information on Inset
Map (optional)
Displays Connext Weather lightning information
on Inset Map (optional)
Displays METAR flags on airport symbols shown on
the Inset Map (optional)
Index
Appendix
METAR
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on Inset
Map
Displays terrain information on Inset Map
128
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
AHRS1
BACK
AHRS2
ALERTS
Select the BACK Softkey to
return to the top level softkeys.
Level 1
Level 2
AFCS
Sensor Softkeys
Description
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Flight
Planning
ADC2
GPS Nav
ADC1
Displays softkeys for selecting the #1 and #2 AHRS
and Air Data Computers
Selects the #1 Air Data Computer
SENSOR
Nav/Com/
XPDR/Audio
ADC2
ADC1
Flight
Instruments
ALERTS
Procedures
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
129
Flight
Instruments
Appendix
DME
Nav/Com/
XPDR/Audio
SYN VIS
ALERTS
HDG MODE ALT UNIT
HSI FMT
ALERTS
GPS Nav
AFCS
Select the BACK Softkey
to return to the top-level softkeys
DG FREE DG SLAVE
Flight
Planning
HDG +
360 HSI
ARC HSI
HDG -
HDG SYNC
METERS
TRK SYNC
IN
HPA
BACK
ALERTS
BACK
ALERTS
ALERTS
Procedures
ALERTS
PATHWAY
SYN TERR HRZN HDG APTSIGNS
Hazard
Avoidance
PFD Configuration Softkeys
Level 1
Additional
Features
ALERTS
Level 2
Level 3
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
PFD
Annun/Alerts
SYN VIS
PATHWAY
Appendix
Description
SYN TERR
Displays rectangular boxes
representing the horizontal and vertical
flight path of the active flight plan
Enables synthetic terrain depiction
Index
HRZN HDG Displays compass heading along the
Zero-Pitch line
130
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Level 2
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.
Resets PFD to default settings, including changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrow and speed
DFLTS
WIND
OPTN 1
OFF
Information not displayed
Flight
Planning
OPTN 3
Wind direction arrow with digital
direction and speed
Longitudinal and lateral components
OPTN 2
BRG1
Procedures
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information, and ADF/
DME
Hazard
Avoidance
frequency.
360 HSI
BRG2
Annun/Alerts
ARC HSI
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
HSI FRMT
Appendix
frequency.
HDG MODE
190-01344-02 Rev. B
Displays softkeys to select DG Modes
(GRS 7800 installations only)
Allows the DG to enter FREE mode
Slaves the DG to the AHRS.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index
DG FREE
DG SLAVE
GPS Nav
APTSIGNS
AFCS
Description
Nav/Com/
XPDR/Audio
Level 3
Flight
Instruments
Level 1
131
Level 1
Level 2
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Level 3
HDG HDG +
HDG SYNC
Slews heading counterclockwise
Slews heading clockwise
Synchronizes heading to the selected
heading
TRK SYNC
Synchronizes heading to the current
track
GPS Nav
ALT UNIT
Procedures
Flight
Planning
METERS
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)
Hazard
Avoidance
STD BARO
Description
Additional
Features
ALERTS
ALERTS
Annun/Alerts
Select the BACK Softkey to return
to the top-level softkeys.
ALERTS
Appendix
Select the BACK Softkey to return
to the previous level softkeys.
Index
Transponder Softkeys
132
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Level 2
Level 3
Description
STBY
Selects Standby Mode (transponder does
not reply to any interrogations)
White (On-Ground) - Transponder generates Mode A and Mode S replies, as well
as transmission of acquisition and extended squitters, including ADS-B out (if
equipped).
ON
GPS Nav
Selects the #2 transponder as active
AFCS
XPDR2
Nav/Com/
XPDR/Audio
XPDR1
Displays transponder mode selection
softkeys
Selects the #1 transponder as active
XPDR
Flight
Instruments
Level 1
Procedures
ALT
Flight
Planning
Green (Airborne) - Transponder generates Mode A and Mode S replies, as well
as transmission of acquisition and extended squitters, including ADS-B out (if
equipped).
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
133
Index
190-01344-02 Rev. B
Automatically enters the VFR code (1200 in
the U.S.A. only)
Appendix
VFR
Annun/Alerts
Green (Airborne) - Transponder generates
Mode A, Mode C, and Mode S replies to
interrogations, as well as transmissions of
acquisition and extended squitters including ADS-B out (if equipped).
Additional
Features
White (On-Ground) - Transponder does
not allow Mode A or Mode C replies to interrogations, , but it does permit acquisition
and extended squitters including ADS-B
out (if equipped), and replies to discretely
addressed Mode S interrogations.
Hazard
Avoidance
Selects Altitude Mode (selection is usually
automatic)
Level 1
Level 2
Level 3
Description
0—7
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
BKSP
Removes numbers entered, one at a time
CODE
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
ALERTS
Displays Alerts Window
TRFC/MAP SENSOR
Flight
Planning
GPS Nav
AFCS
IDENT
PFD
OBS
CDI
(optional)
DME
XPDR/TFC
IDENT
TMR/REF
NRST
ALERTS
Procedures
Press the BACK Softkey to return
to the top-level softkeys.
MODE
TCAS
CODE
BACK
IDENT
ALERTS
Hazard
Avoidance
Selecting BACK returns to the
previous softkey level.
REL
ABS
ALT RNG
TEST
BACK
ALERTS
Additional
Features
Selecting BACK returns to the
previous softkey level.
ABOVE NORMAL BELOW UNREST
BACK
ALERTS
Annun/Alerts
Selecting BACK returns to the
previous softkey level.
STBY
ALT
TA ONLY
BACK
TA/RA
ALERTS
Selecting BACK returns to the
previous softkey level.
0
Appendix
Index
ON
1
2
3
4
5
6
7
IDENT
BKSP
BACK
ALERTS
Transponder/Traffic Softkeys with TCAS II Option
Level 1
XPDR/TFC
134
Level 2
Level 3
Level 4
Description
Displays the transponder and
TCAS II selection softkeys
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Level 2
Level 3
MODE
Procedures
Hazard
Avoidance
Additional
Features
TCAS II system is set to
standby.
Flight
Planning
Green (Airborne) Transponder generates Mode A
and Mode S replies, as well as
transmission of acquisition and
extended squitters, including
ADS-B out (if equipped).
GPS Nav
Displays transponder mode
selection softkeys
Selects transponder Standby
Mode (transponder does not
reply to any interrogations).
When the transponder is set to
standby, the TCAS II system is
also set to standby.
White (On-Ground) Transponder generates Mode A
and Mode S replies, as well as
transmission of acquisition and
extended squitters, including
ADS-B out (if equipped).
AFCS
ON
Description
Nav/Com/
XPDR/Audio
STBY
Level 4
Flight
Instruments
Level 1
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
135
Level 1
Level 2
Level 3
ALT
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Level 4
Description
Selects Altitude Mode (selection is usually automatic)
GPS Nav
AFCS
White (On-Ground) Transponder does not allow
Mode A or Mode C replies
to interrogations, , but it
does permit acquisition and
extended squitters including
ADS-B out (if equipped), and
replies to discretely addressed
Mode S interrogations.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Green (Airborne) Transponder generates Mode
A, Mode C, and Mode S replies
to interrogations, as well as
transmissions of acquisition
and extended squitters
including ADS-B out (if
equipped).
Annun/Alerts
TA ONLY
TA/RA
Appendix
BACK
Index
TCAS
REL
136
TCAS II system is set to
standby.
Activates the TCAS II system
in TA Only Mode and set the
transponder to ALT
Activates the TCAS II system
in TA/RA Mode and sets the
transponder to ALT
Returns to the previous softkey
level
Displays the TCAS control
softkeys
Displays intruder altitude as
altitude relative to own aircraft
altitude
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Level 2
Level 3
ABS
ALT RNG
Appendix
Index
137
Annun/Alerts
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features
190-01344-02 Rev. B
Hazard
Avoidance
BKSP
Activates the Special Position
Identification (SPI) pulse for
18 seconds, identifying the
transponder return on the ATC
screen
Removes numbers entered, one
at a time
Procedures
IDENT
Activates Test Mode and
displays test intruder symbols
Returns to the previous softkey
level
Displays transponder code
selection softkeys 0-7
Use numbers to enter code
Flight
Planning
0—7
Displays the altitude display
range softkeys
Displays non-threat traffic from
ABOVE
9900 feet above the aircraft to
2700 feet below the aircraft.
Typically used during climb
phase of flight.
NORMAL Displays non-threat traffic from
2700 feet above the aircraft to
2700 feet below the aircraft.
Typically used during enroute
phase of flight.
BELOW Displays non-threat traffic from
2700 feet above the aircraft to
9900 feet below the aircraft.
Typically used during descent
phase of flight.
UNREST All traffic is displayed
GPS Nav
CODE
Displays intruder MSL altitude
AFCS
BACK
Description
Nav/Com/
XPDR/Audio
TEST
Level 4
Flight
Instruments
Level 1
Level 1
Level 2
Level 3
Level 4
GPS Nav
AFCS
TMR/REF
NRST
ALERTS
MFD NAVIGATION PAGE SOFTKEY MAP
(optional)
DCLTR
MAP
SHW CHRT
CHKLIST
DCLTR-1
Procedures
Flight
Planning
Description
Activates the Special Position
Identification (SPI) pulse for
18 seconds, identifying the
transponder return on the ATC
screen
Displays Timer/References
Window
Displays Nearest Airports
Window
Displays Alerts Window
IDENT
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
DCLTR-2
Hazard
Avoidance
DCLTR-3
TRAFFIC
PROFILE
TOPO
(optional)
TERRAIN
(optional)
STRMSCP
AIRWAYS
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
Additional
Features
AIRWY ON
AIRWY LO
Annun/Alerts
AIRWAY HI
MFD Softkeys
Appendix
Level 1
Level 2
Description
Enables second-level Navigation Map softkeys
MAP
TRAFFIC
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
Index
TOPO
138
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
Level 2
Description
139
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Appendix
190-01344-02 Rev. B
Annun/Alerts
LOADING UPDATED DATABASES
Database information is obtained from third party sources. Inaccuracies in the data
may be discovered from time to time. Garmin communicates this information by
issuing a Database Alert. These notifications are available on http://fly.garmin.com.
Additional
Features
CHKLIST
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
Hazard
Avoidance
SHW CHRT
Displays Connext Weather lightning information on
the Navigation Map (optional)
Returns to top-level softkeys
Procedures
DCLTR (3)
Flight
Planning
BACK
GPS Nav
DL LTNG
AFCS
Displays Connext Weather precipitation on the
Navigation Map (optional)
XM LTNG Displays SiriusXM 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
Flight
Instruments
Level 1
Garmin requests the flight crew report any observed discrepancies related to database
information. These discrepancies could come in the form of an incorrect procedure;
incorrectly identified terrain, obstacles and fixes; or any other displayed item used for
navigation or communication in the air or on the ground. Go to http://fly.garmin.com
and select “Aviation Data Error Report”.
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in maintenance being required to reboot the system.
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
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 displays 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
Database synchronization has been canceled by removing the
bottom SD card in display being updated
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
1)
140
With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
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.
8)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete syncing, indicated by ‘Complete’ being displayed.
9)
Remove and reapply power to the system.
AFCS
3)
Nav/Com/
XPDR/Audio
Update the Garmin databases on the MFD card.
Flight
Instruments
2)
GPS Nav
Flight
Planning
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
Hazard
Avoidance
Loading the Jeppesen Navigation Database as the Active Navigation
Database
Procedures
12) 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.
Additional
Features
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.
Annun/Alerts
1)
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).
Appendix
2)
Turn the system ON. A prompt is displayed in the upper left corner of the
display:
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
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
141
Index
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Appendix
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
the active navigation database.
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.
10) Turn the small FMS Knob to select the System Status Page.
GPS Nav
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
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
5)
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 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)
After the navigation database files are copied to the bottom SD card, press
any key to continue, as instructed.
Again, press any key to continue as instructed on the display.
Appendix
8)
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. The display now starts in normal mode. Do not remove
power while the display is starting.
Index
7)
9)
Press the ENT Key to acknowledge the startup screen.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
142
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Appendix
13) Turn system power OFF.
14) Remove the SD card from the top card slot of the MFD.
Nav/Com/
XPDR/Audio
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
Flight
Instruments
11) Turn the small FMS Knob to select the System Status Page.
15) Turn system power ON.
AFCS
16) Press the ENT Key to acknowledge the startup screen.
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
Flight
Planning
19) 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.
GPS Nav
18) Turn the small FMS Knob to select the System Status Page.
Magnetic Field Variation Database Update
Procedures
Hazard
Avoidance
Additional
Features
At startup, the system compares this version of the MV DB with that presently being
used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs
to be updated, a prompt is displayed on the Navigation Map Page, as shown in the
following figure. Note, in the following example, GRS1 is the first AHRS to indicate
an update is available. In actuality, this is dependent on which AHRS is the first to
report status to the system. GRS2 may be displayed before GRS1. The order is not
important, only that both AHRS be updated.
Annun/Alerts
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
143
Index
Loading the magnetic field variation database update:
1) With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key
on the MFD. A progress monitor is displayed as shown in the following
figure.
Appendix
GRS1 Magnetic Field Variation Database Update Prompt
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Appendix
GPS Nav
Uploading Database to GRS1
When the upload is complete, the prompt for the next GRS upload is
displayed, as seen in the following figure.
Procedures
Flight
Planning
2)
Hazard
Avoidance
GRS2 Magnetic Field Variation Database Update Prompt
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed as shown in the following figure. When the upload is complete,
the system is ready for use.
Appendix
Annun/Alerts
Additional
Features
3)
Index
Uploading Database to GRS2
144
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Index
FD 95
Flight Director 9
Flight path marker 65
FliteCharts® 66, 67
Frequency Transfer 6
G
Gain 62
Hazard
Avoidance
H
HF 6
Horizon heading 65
Horizontal scan 62
Additional
Features
I
Appendix
Inhibit 60
Inhibit TAWS 60
Inset Map 127, 128
IOI 96, 97, 100
Iridium satellite network 69, 70, 74
Annun/Alerts
J
Index
190-01344-02 Rev. B
F
Procedures
CDI 1, 2, 6, 122
Cell 39, 40
Cell mode 40
Channel Presets 86
ChartView 66, 67
Edit a flight plan 30
ESP 89, 90
Flight
Planning
C
E
GPS Nav
Barometric Altitude Minimums 3
Barometric pressure 132
Bearing line 61, 62
DB Mismatch 140
Declutter 128, 139
Direct-to 13
DME 5, 6
AFCS
B
D
Nav/Com/
XPDR/Audio
Access code 69
Activate a flight plan 14
Active Channel 85
Active database 141
Active Navigation Database 141
AC-U-KWIK 68
ADF 5, 6, 131
Advisory alerts 93
AHRS 114, 115, 116, 118, 119, 143
Air Data Computer 94
Airport Directory 68
Airport Signs 65, 66
Airways 139
Alert messages 117
ALT 55
Altitude mode 55
Altitude volume 55
Antenna stabilization 63
Antenna tilt 61
AOPA 68
AP 95
Attitude & Heading Reference System
94
Audio panel controls
NAV1, NAV2 6
Code selection softkeys 5
COM 6
Flight
Instruments
A
Jeppesen 67
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index-1
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
L
R
Level Mode 90
Lightning 39, 40, 42, 128
Low speed data 69, 70
Register 70
Resolution Advisory 53
ROC 96, 100
M
S
Magnetic Field Variation Database 143,
144
Map panning 41
Message advisories 103, 105, 108,
114, 116, 118, 119, 120
MET 95
METAR 41
Minimums 102
MISCOMP 94
Mistrim 95
Multi Function Display (MFD)
Softkeys 138
MV DB 143
SafeTaxi® 66
SBAS 10, 34, 59, 110, 111
Sector scan 62
Sensor 94
SiriusXM lightning 128, 139
STAB 63
Standby 61
Standby Navigation Database 107, 142
Store Flight Plan 30
Stormscope lightning data 39, 40, 128
Strike 39
Strike mode 40
SVT 65, 123
SVT Terrain 65
Synchronization 140
SYNC Status 143
Synthetic Vision System 65
System ID 69
N
NAV 6
NAV1 2, 6
NAV2 6
Navigation database 15, 16, 125
NEXRAD 41, 128, 139
NEXRAD Softkey 49
O
OBS 2
Obstacles 108, 110
Overspeed Protection 10
P
Pathways 65, 66
PIREP 52
PIT 94
Predefined message 77, 78
Index-2
T
TAF 41, 51
TAS 54, 55, 114
TAWS 57, 58, 59, 60, 96, 97, 98, 99,
101
TAWS-B 57, 58
TCAS II 5, 6, 55, 56, 127, 134, 135,
136
TCAS System Test Passed 102, 103
Telephone 70
Terrain 57, 58, 96, 97, 99, 100, 108,
128, 138
Text message 76, 77, 79
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Index
Flight
Instruments
Text messaging 75
Tilt line 61
Timer 121
Topographical data 128, 138
Traffic 39, 54, 56, 128, 138
Traffic Advisory (TA) 54, 102, 103
Traffic map page 54, 55, 56
Transponder 5, 133, 134, 135, 137,
138
Nav/Com/
XPDR/Audio
AFCS
V
GPS Nav
Vertical speed guidance 16
Vertical track 102
VNV 13, 122
Vspeed 3
Flight
Planning
W
Procedures
WATCH 63
Waypoint Selection Submenu 24
Weather Attenuated Color Highlight 63
Weather data link page 41
Weather radar 60
Wi-Fi 82, 83, 84, 85
Wind data 131
Winds Aloft 52
Hazard
Avoidance
Additional
Features
Annun/Alerts
Appendix
Index
190-01344-02 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Index-3
Index
Appendix
Annun/Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-02 Rev. B
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
© 2011-2016 Garmin Ltd. or its subsidiaries
190-01344-02 Rev. B
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