Garmin Beechcraft A36 Reference Guide

®
G1000
Cockpit Reference Guide for the Beechcraft A36/G36
Integrated Flight Deck
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2005-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0858.07 or later for the Beechcraft A36/G36. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138
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Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts® and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are registered trademarks of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.;
July, 2010 190-00525-03 Rev. A Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system. 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 74A Air Data Computer, or other altimeters in the aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.
WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Warnings, Cautions & Notes
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance.
WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration.
WARNING: The Garmin G1000, as installed in the Beechcraft A36/G36 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the Beechcraft A36/G36 Pilot’s Operating Handbook (POH). Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Warnings, Cautions & Notes
WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.”
WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI­REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti­reflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Warnings, Cautions & Notes
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data.
NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft.
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Warnings, Cautions & Notes
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Record of Revisions
Part Number Change Summary
190-00525-00 Initial release. 190-00525-01
Rev A
Added GDU software version 6.13 parameters. Added TAWS
Rev B
Changed system software number to 0464.08.
190-00525-02
Rev A
Changed to smaller format Added Airways, WAAS, VNAV & Charts Updated G1000 System Messages Added other GDU 8.10 parameters
Rev B
Removed FD Formatting feature
190-00525-03 Added GDU 11.01 parameters
Added Synthetic Vision System Added flight plan import/export Updated procedure for entering User Waypoints Updated XM weather products Updated TAWS annunciations Added CDI operation in Dead Reckoning mode Added AOPA Airport Directory Added temporary user waypoints Added database synchronization Added GTS 820 TAS Removed support for non-WAAS systems Various clerical corrections
Revision Date of Revision Affected Pages Description
A July, 2010 All Production release
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
RR-1
Record of Revisions
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Table of Contents
FLIGHT INSTRUMENTS ................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting ...................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg) .................................................... 1
Change Altimeter Barometric Pressure Setting Units ...................................................... 1
Change Navigation Sources ................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS .................................................... 2
Generic Timer ............................................................................................................................. 2
Configure Vspeed Bugs Individually ..................................................................................... 2
Set Barometric Minimum Descent Altitude ........................................................................ 3
Displaying Wind Data ..............................................................................................................3
Changing HSI Format ............................................................................................................... 3
ENGINE INDICATION SYSTEM ................................................................................................. 5
Engine Display ........................................................................................................................... 5
Lean Engine Display ................................................................................................................. 6
Engine System Display ............................................................................................................ 8
NAV/COM/TRANSPONDER/AUDIO PANEL ......................................................................... 9
ADF Tuning (Optional) .............................................................................................................. 9
DME Tuning (Optional) ............................................................................................................. 9
Enter a Transponder Code....................................................................................................... 9
Activate ADS-B Transmit ......................................................................................................... 9
Selecting a COM Radio .......................................................................................................... 10
Selecting a NAV Radio ........................................................................................................... 10
NAV/COM Tuning ..................................................................................................................... 10
Digital Clearance Recorder and Player .............................................................................. 11
Intercom System (ICS) Isolation .......................................................................................... 11
AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 13
Flight Director Activation ..................................................................................................... 13
Vertical Modes ......................................................................................................................... 14
Lateral Modes .......................................................................................................................... 15
GPS NAVIGATION ........................................................................................................................17
Direct-to Navigation .............................................................................................................. 17
Activate a Stored Flight Plan ............................................................................................... 18
Activate a Flight Plan Leg ..................................................................................................... 18
Stop Navigating a Flight Plan .............................................................................................. 19
Vertical Navigation (VNAV)................................................................................................... 19
FLIGHT PLANNING ...................................................................................................................... 21
Trip Planning ............................................................................................................................ 21
Create a New User Waypoint Defined by Latitude & Longitude ................................. 23
Create a New User Waypoint Defined by Radials from Other Waypoints ................. 23
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
i
Table of Contents
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint ............................................................................................................................. 25
Delete a User Waypoint ......................................................................................................... 26
Create a New Flight Plan ...................................................................................................... 27
Import a Flight Plan from an SD Card ................................................................................ 28
Insert a Waypoint in the Active Flight Plan ...................................................................... 29
Enter an Airway in a Flight Plan .......................................................................................... 29
Invert An Active Flight Plan .................................................................................................. 30
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 30
Store a Flight Plan .................................................................................................................. 31
Edit a Stored Flight Plan ....................................................................................................... 31
Delete a Waypoint from the Flight Plan ............................................................................ 31
Invert and Activate a Stored Flight Plan ........................................................................... 32
Copy a Flight Plan ................................................................................................................... 32
Delete a Flight Plan ................................................................................................................ 32
Graphical Flight Plan Creation ............................................................................................. 33
Export a Flight Plan to an SD Card ..................................................................................... 33
PROCEDURES ................................................................................................................................. 35
Load and Activate a Departure Procedure ....................................................................... 35
Activate A Departure Leg ..................................................................................................... 35
Load An Arrival Procedure .................................................................................................... 35
Activate An Arrival Leg ......................................................................................................... 36
Load and/or Activate an Approach Procedure ................................................................. 36
Activate An Approach in the Active Flight Plan ............................................................... 37
Activate a Vector to Final Approach Fix ............................................................................ 37
Activate A Missed Approach in the Active Flight Plan ................................................... 38
HAZARD AVOIDANCE ................................................................................................................ 39
Customizing the Hazard Displays on the Navigation Map ............................................ 39
STORMSCOPE® (Optional) .................................................................................................... 39
XM Weather (Subscription Optional) ................................................................................. 41
Traffic Systems ........................................................................................................................ 42
Terrain Awareness & Warning System (TAWS) Display ................................................... 44
ADDITIONAL FEATURES ........................................................................................................... 47
Synthetic Vision ....................................................................................................................... 47
Terminal Procedure Charts ...................................................................................................48
AOPA Airport Directory ......................................................................................................... 50
XM® Radio Entertainment (Subscription Optional) ........................................................ 51
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
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Table of Contents
ABNORMAL OPERATION..........................................................................................................53
Reversionary Mode ................................................................................................................ 53
Abnormal COM Operation .................................................................................................... 53
Hazard Displays with Loss of GPS Position ....................................................................... 53
Unusual Attitudes ................................................................................................................... 54
Dead Reckoning ...................................................................................................................... 55
ANNUNCIATIONS & ALERTS ................................................................................................... 57
WARNING Annunciation ........................................................................................................ 57
CAUTION Annunciation .......................................................................................................... 57
ADVISORY Annunciation........................................................................................................ 58
Alert Message .......................................................................................................................... 58
AFCS ALERTS ............................................................................................................................ 58
TAWS-B Alerts .......................................................................................................................... 59
TAWS-B System Status Annunciations ...............................................................................61
Voice Alerts .............................................................................................................................. 62
MFD & PFD Message Advisories .......................................................................................... 63
Database Message Advisories ............................................................................................. 64
GMA 1347 Message Advisories ............................................................................................ 66
GIA 63W Message Advisories ............................................................................................... 67
GEA 71 Message Advisories .................................................................................................. 69
GTX 33 Message Advisories .................................................................................................. 70
GRS 77 Message Advisories .................................................................................................. 70
GMU 44 Message Advisories ................................................................................................ 71
GDL 69/69A Message Advisories .........................................................................................71
GDC 74A Message Advisories ............................................................................................... 71
GTS 820 Message Advisories ................................................................................................ 72
Miscellaneous Message Advisories ..................................................................................... 72
Flight Plan Import/Export Messages .................................................................................. 76
Appendix ......................................................................................................................................... 79
PFD Softkey Map .................................................................................................................... 79
MFD Softkey Map ................................................................................................................... 84
Database Updates .................................................................................................................. 86
Index ...........................................................................................................................................Index-1
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

1)
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).
Or
:
Press the HPA Softkey to display the barometric pressure setting in hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard

CHANGE NAVIGATION SOURCES

1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency.
3)
Press the CDI Softkey a third time to return to GPS.
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
1
Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Flight
1)
InstrumentsEIS
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.
Nav/Com/
XPDR/AudioAFCSGPS Nav

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.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.
Flight
PlanningProcedures
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it starts counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window.

CONFIGURE VSPEED BUGS INDIVIDUALLY

Hazard
Avoidance
1)
Press the TMR/REF Softkey.
2)
Turn the
large
FMS Knob to highlight the desired Vspeed.
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a speed has been changed from a default value, an asterisk appears next to the speed).
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
2
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Flight Instruments

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of ‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
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.

DISPLAYING WIND DATA

1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data to the left of the HSI.
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.

CHANGING HSI FORMAT

1)
Press the PFD Softkey.
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Or
:
Press the ARC HSI Softkey to display the arc style HSI.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Annun/
Alerts Appendix Index
3
Flight Instruments
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A

Engine Indication System

ENGINE INDICATION SYSTEM

ENGINE DISPLAY

In all cases green indicates normal operation, yellow indicates caution, and red
indicates warning.
Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys
which in turn provide access to the Lean Page and the System Page, respectively.
Manifold
Pressure
Gauge
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
RPM Gauge
Fuel Flow Numeric
Fuel Flow
Indicator
Readout Leaning
Pointer Cylinder Head
Oil Temperature
Indicator
Temperature Indicator
Oil Pressure Indicator
Ammeter
Voltmeter
Fuel Quantity
Indicator
Default Engine Page
In a maximum power climb or cruise climb, engine leaning may be done using the
Leaning Pointer as a reference when adjusting fuel mixture
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
5
Engine Indication System

LEAN ENGINE DISPLAY

Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
temperature
Exhaust Gas Temperature
Bar Graph
EGT peak
Fuel Flow Numeric Readout
Difference be­tween peak and current tempera­ture of selected cylinder
EGT Readout For Selected Cylinder
Flight
PlanningProcedures
Cylinder Head
Temperature
Bar Graph
CHT Readout For Selected Cylinder
LEAN Engine Page
Hazard
Avoidance
1)
Press the ENGINE Softkey, then the LEAN Softkey to display the LEAN Engine Page.
2)
Features
Additional
Press the CYL SLCT Softkey to select the desired cylinder for monitoring.
3)
Press the ASSIST Softkey to hightlight the first cylinder that peaks. Information for that cylinder is displayed.
Abnormal
Operation
NOTE: The pilot should follow the engine manufacturer’s recommended
leaning procedures in the Pilot’s Operating Handbook (POH).
AlertsAppendixIndex
Annun/
Pressing the CYL SLCT Softkey cycles through the cylinders; the selected cylinder is displayed in light blue. The CYL SLCT Softkey is disabled during warning or caution conditions or when the ASSIST Softkey is pressed.
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Engine Indication System
When the ASSIST Softkey is selected, the system initially highlights and selects the cylinder number with the hottest EGT and displays its temperature below the EGT bar graph. A readout showing the difference between peak (DPEAK) and the current temperature for the selected cylinder is displayed above the EGT bar graph.
As the mixture is leaned, a light blue line will appear above each cylinder to indicate EGT peak.
When the system detects the first cylinder to peak, the cylinder numbers below the EGT graph disappear, and “1st” is annunciated below the first peaked cylinder to indicate the other cylinders are rich of peak. As the mixture is further leaned, “Last” is annunciated below the last peaked cylinder indicating all cylinders are lean of peak. Refer to the POH and AFM for the recommended mixture adjustment procedures.
Monitoring of the cylinder continues until the ASSIST Softkey is pressed again which disables lean assist and removes the peak lines from the bar graph and the temperature deviation from peak (DPEAK). The system then returns to seeking the hottest cylinder.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
7
Engine Indication System

ENGINE SYSTEM DISPLAY

Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
1)
Press the ENGINE Softkey, then the SYSTEM Softkey to display the SYSTEM Engine Page.
2)
If desired, use the
DEC FUEL, INC FUEL
and
RST FUEL
Softkeys to
adjust the amount of fuel remaining for totalizer calculations.
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset.
System
Information
Fuel Calculation Information
Features
Additional
Electrical Information
Abnormal
Operation
AlertsAppendixIndex
Annun/
SYSTEM Engine Page
Any exceedance of default Engine Page parameters, while viewing the System Engine Page, causes the display to automatically switch back to the default Engine Page.
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

Tune the ADF using the remote ADF control head.

DME TUNING (OPTIONAL)

1)
Press the DME Softkey.
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.
Nav/Com/XPDR/Audio Panel
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/

ENTER A TRANSPONDER CODE

1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the CODE Softkey to display the transponder code selection softkeys, for digit entry.
3)
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.

ACTIVATE ADS-B TRANSMIT

1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the ADS-B TX Softkey to enable transmission of three-dimensional aircraft position and aircraft ground track.
3)
Press the ADS-B TX Softkey again to disable transmission.
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
9
Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO

Flight
InstrumentsEIS
Transmit/Receive
Press the COM1 MIC, COM2 MIC installed) on the audio panel.
Receive Only
Nav/Com/
XPDR/AudioAFCSGPS Nav
Press the COM1, COM2 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
Flight
PlanningProcedures
deselect the navigation radio audio source. All radio keys can be selected individually or together.

NAV/COM TUNING

, or
COM3 MIC Key (optional COM, if
, or
COM3 Key (optional COM, if installed) on the
Hazard
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Features
Additional
Abnormal
Operation
AlertsAppendixIndex
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1)
Press the small tuning knob to select the desired radio for tuning. A light blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active frequency field.
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
Nav/Com/XPDR/Audio Panel

DIGITAL CLEARANCE RECORDER AND PLAYER

NOTE: Only the audio for the selected
COM MIC
Key is recorded. Audio is
not recorded for COM3 MIC.
• PressingPLAY once plays the latest recorded memory block, then returns to normal operation.
• PressingMKR/MUTE while playing a memory block stops play.
• Pressingthe PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block.

INTERCOM SYSTEM (ICS) ISOLATION

Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/
Com radios and music.
Mode
PILOT KEY
ANNUNCIATOR
ALL OFF OFF
PILOT ON OFF
COPLT KEY
ANNUNCIATOR
Pilot Hears
Selected radios; pilot; copilot; passengers; music
Selected radios; pilot
Copilot
Hears
Selected radios; pilot; copilot; passengers; music
Copilot; passengers; music
Passenger
Hears
Selected radios; pilot; copilot; passengers; music
Copilot; passengers; music
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
COPILOT OFF ON
CREW ON ON
190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Selected radios; pilot; passengers; music
Selected radios; pilot; copilot
Copilot
Selected radios; pilot; copilot
Selected radios; pilot; passengers; music
Passengers; music
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Alerts Appendix Index
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Nav/Com/XPDR/Audio Panel
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
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Features
Additional
Abnormal
Operation
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A

AUTOMATIC FLIGHT CONTROL SYSTEM

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.
NOTE: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

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.
AFCS
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Control Pressed
Modes Selected
Lateral Vertical FD Key Roll Hold (default) ROL Pitch Hold (default) PIT AP Key Roll Hold (default) ROL Pitch Hold (default) PIT
CWS Switch Roll Hold (default) ROL Pitch Hold (default) PIT
GA Switch Go Around GA Go Around GA
A LT 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
GPS
NAV Key Navigation**
VOR
Pitch Hold (default) PIT
LOC
APR Key Approach**
GPS
VAPP
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT GP GS
HDG Key Heading Select HDG Pitch Hold (default) PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**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.
Planning Procedures
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190-00525-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
13
AFCS

VERTICAL MODES

Flight
InstrumentsEIS
Vertical Mode Description Control Annunciation
Holds the current aircraft pitch
Pitch Hold
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selected Altitude Armed
Altitude Hold
Vertical Speed
Flight
PlanningProcedures
Flight Level Change
VNAV
Hazard
Avoidance
VNAV Target Altitude Armed (GDU 1045
Features
Additional
only)
Glidepath
Abnormal
Operation
Glideslope
AlertsAppendixIndex
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Go Around
* ALTS armed automatically when PIT, VS, FLC, 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
attitude; may be used to climb/ descend to the Selected Altitude
AFCS armed to capture the altitude displayed in the Selected Altitude window
Holds the current Altitude Reference
Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude
Maintains the current aircraft airspeed in IAS while the aircraft is climbing/descending to the Selected Altitude
Captures and tracks the VNAV flight path
VNV Key VPTH
AFCS armed to capture the altitude displayed in the VNAV Target Altitude window
Captures and tracks the WAAS glidepath on approach
APR Key
Captures and tracks the ILS glideslope on approach
Disengages the autopilot and commands a constant pitch attitude and wings level
(default) PIT
* ALTS
A LT Key A LT nnnnn f T
VS Key VS nnnn f p m
FLC Key FLC nnn k T
** ALTV
GA
Switch
GP
GS
GA
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
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