Garmin 350, 400 Reference Guide

®

G1000

Cockpit Reference Guide for the Cessna 350/400

Integrated Flight Deck

System Software 0534.11 or later

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2006-2009 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0534.11 or later for the Cessna
350/400. 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: [phone] Fax: [phone]

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone] Fax [phone]

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]

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.; XM® is a registered trademark of XM
Satellite Radio, Inc.

March, 2009 190-00567-03 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 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 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 system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.

WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only

for weather avoidance, not penetration.

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 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: The Garmin G1000, as installed in the Cessna 350/400 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
Cessna 350/400 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.

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.”

190-00567-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Warnings, Cautions & Notes

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 anomalies in the earth’s magnetic field, operating
the G1000 within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.

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.

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Warnings, Cautions & Notes

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.

190-00567-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Warnings, Cautions & Notes

Blank Page

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Record of Revisions

Part Number Change Summary

190-00567-00

Rev A

Production release

Rev B

Added C350 parameters, TAWS changes, and Stormscope.

190-00567-01

Rev A

Rev B

Added GDU 8.10 parameters, WAAS, VNAV, Airways, and Charts

Changed company references to Cessna

190-00567-02 Reformatted manual

Added GDU 9.03 parameters

190-00567-03 Added GDU 9.05 with Synthethic Vision System (SVS)

Removed Stormscope

Revision Date of Revision Affected Pages Description

A 3/09 i-Index-4 Production release

190-00567-03 Rev. A RR-1

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Record of Revisions

Blank Page

RR-2

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 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 ............................................................................................................ 2

Set Barometric Minimum Descent Altitude ........................................................................ 3

Displaying Wind Data ..............................................................................................................3

Changing HSI Format ............................................................................................................... 3

ENGINE INDICATION SYSTEM ................................................................................................. 5

Engine Page................................................................................................................................ 6

Engine Leaning Assist Mode ................................................................................................. 10

NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 13

ADF Tuning (Optional) ............................................................................................................ 13

DME Tuning (Optional) ........................................................................................................... 13

Enter a Transponder Code..................................................................................................... 13

Selecting a COM Radio .......................................................................................................... 14

Selecting a NAV Radio ........................................................................................................... 14

NAV/COM Tuning ..................................................................................................................... 14

Digital Clearance Recorder and Player .............................................................................. 14

Intercom System (ICS) Isolation .......................................................................................... 15

GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................17

Flight Director Activation ..................................................................................................... 17

Vertical Modes ......................................................................................................................... 18

Lateral Modes .......................................................................................................................... 19

GPS NAVIGATION ........................................................................................................................ 21

Direct-to Navigation .............................................................................................................. 21

Activate a Stored Flight Plan ............................................................................................... 22

Activate a Flight Plan Leg ..................................................................................................... 22

Stop Navigating a Flight Plan .............................................................................................. 23

Vertical Navigation (VNAV)................................................................................................... 23

FLIGHT PLANNING ...................................................................................................................... 25

Trip Planning ............................................................................................................................ 25

Create a New User Waypoint ............................................................................................... 27

Delete a User Waypoint ......................................................................................................... 28

Create a New Flight Plan ...................................................................................................... 28

Insert a Waypoint in the Active Flight Plan ...................................................................... 29

190-00567-03 Rev. A i

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Table of Contents

Enter an Airway in a Flight Plan .......................................................................................... 30

Invert An Active Flight Plan .................................................................................................. 30

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 31

Store a Flight Plan .................................................................................................................. 31

Edit a Stored Flight Plan ....................................................................................................... 31

Delete a Waypoint from the Flight Plan ............................................................................ 32

Invert and Activate a Stored Flight Plan ........................................................................... 32

Copy a Flight Plan ................................................................................................................... 33

Delete a Flight Plan ................................................................................................................ 33

Graphical Flight Plan Creation ............................................................................................. 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 ............................................................................ 38

Activate A Missed Approach in the Active Flight Plan ................................................... 38

HAZARD AVOIDANCE ................................................................................................................39

Customizing the Hazard Displays on the Navigation Map ............................................ 39

XM Weather (Optional) .......................................................................................................... 39

Traffic Systems ........................................................................................................................ 40

Terrain And Obstacle Proximity ........................................................................................... 42

Terrain-SVS ............................................................................................................................... 43

Terrain Awareness & Warning System (TAWS) Display (Optional) ............................... 45

ADDITIONAL FEATURES ........................................................................................................... 47

Synthetic Vision ....................................................................................................................... 47

Terminal Procedure Charts ...................................................................................................48

XM® Radio Entertainment..................................................................................................... 50

ABNORMAL OPERATION..........................................................................................................53

Reversionary Mode ................................................................................................................ 53

Abnormal COM Operation .................................................................................................... 53

Hazard Displays with Loss of GPS Position ....................................................................... 53

Unusual Attitudes ................................................................................................................... 54

Dead Reckoning ...................................................................................................................... 54

ii

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Table of Contents

ANNUNCIATIONS & ALERTS ................................................................................................... 57

WARNING Alerts ...................................................................................................................... 57

CAUTION Alerts ........................................................................................................................ 57

Annunciation Advisory .......................................................................................................... 58

Message Advisory Alerts ....................................................................................................... 58

CO Guardian Messages .......................................................................................................... 58

AFCS Alerts ............................................................................................................................... 59

Terrain-SVS Alerts ................................................................................................................... 60

TAWS Alerts .............................................................................................................................. 61

Voice Alerts .............................................................................................................................. 63

MFD & PFD Message Advisories .......................................................................................... 63

Database Message Advisories ............................................................................................. 64

GMA 1347 Message Advisories ............................................................................................ 67

GIA 63 Message Advisories ................................................................................................... 67

GIA 63W Message Advisories ............................................................................................... 70

GEA 71 Message Advisories .................................................................................................. 73

GTX 33 Message Advisories .................................................................................................. 73

GRS 77 Message Advisories .................................................................................................. 74

GMU 44 Message Advisories ................................................................................................ 74

GDL 69A Message Advisories ............................................................................................... 75

GDC 74A Message Advisories ............................................................................................... 75

GCU 476 Message Advisories ............................................................................................... 75

Miscellaneous Message Advisories ..................................................................................... 76

APPENDIX ....................................................................................................................................... 81

PFD Softkey Map .................................................................................................................... 81

MFD Softkey Map ................................................................................................................... 86

INDEX .........................................................................................................................................Index-1

190-00567-03 Rev. A iii

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Table of Contents

Blank Page

iv

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 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)

Select the PFD Softkey.

2)

Select the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

Select the PFD Softkey to display the second-level softkeys.

2)

Select the ALT UNIT Softkey.

3)

Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).

Or

:

Select the HPA Softkey to display the barometric pressure setting in
hectopascals.

4)

Select 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)

Select 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)

Select 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)

Select the CDI Softkey a third time to return to GPS.

190-00567-03 Rev. A 1

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Flight

1)

InstrumentsEIS

Select 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)

Select the OBS Softkey again to disable OBS Mode.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GENERIC TIMER

1)

Select 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

Hazard

Avoidance

1)

Select 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 Cessna 350/400

190-00567-03 Rev. A

Flight Instruments

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)

Select 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 select the TMR/REF Softkey.

DISPLAYING WIND DATA

1)

Select the PFD Softkey.

2)

Select the WIND Softkey to display wind data to the left of the HSI.

3)

Select one of the OPTN softkeys to change how wind data is displayed.

4)

To remove the Wind Data Window, select the OFF Softkey.

CHANGING HSI FORMAT

1)

Select the PFD Softkey.

2)

Select the HSI FRMT Softkey.

3)

Select the 360 HSI Softkey to display the full size HSI.

Or

:

Select 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

190-00567-03 Rev. A 3

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Alerts Appendix Index

Annun/

Flight Instruments

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

4

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

10

Engine Indication System

Instruments EIS

ENGINE INDICATION SYSTEM

1

2

3

4

5

6

6

7

8

9

9

10

Cessna 350 Cessna 400

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

EIS Display

1

Engine Manifold Pressure Gauge

2

Tachometer

3

Fuel Quantity Indicator

4

Fuel Flow Indicator

5

Oil Pressure Indicator

6

Oil Temperature Indicator

190-00567-03 Rev. A 5

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

7

Exhaust Gas Temperature Indicator
(Cessna 350 only)

8

Turbine Inlet Temperature Indicator
(Cessna 400 only)

9

Cylinder Head Temperature Indicator

10

Trim Group

Alerts Appendix Index

Annun/

Engine Indication System

ENGINE PAGE

Flight

Selecting the SYSTEM Softkey on the MFD accesses the Engine Page, which

InstrumentsEIS

displays all Engine Indication System instruments; selecting the softkey again exits the
Engine Page.

Oxygen quantity and outlet pressure are also shown on the Engine Page. The
OXYGEN Softkey can be used to turn the optional oxygen system on/off. If an oxygen
system is not installed, blank gauges are displayed.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

1 2 3 5

11

10

9

1

Oil Temperature/Pressure Gauge

2

Engine Manifold Pressure Gauge

3

Tachometer

4

Fuel Calculations Group

5

Oxygen Quantity Gauge

6

Oxygen Outlet Pressure Gauge

Engine Page (Cessna 350)

7

Electrical Group

8

Trim Group

9

Engine Temperature Group

10

Fuel Quantity Gauges

11

Fuel Flow Gauge

4

6

7

8

Carbon
Monoxide
Warning

6

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Engine Indication System

1 2 3 5

11

10

9

4

6

7

8

Engine Page (Cessna 400)

Carbon Monoxide Detection

If carbon monoxide (CO) in the cabin becomes too high (exceeds 50 ppm), a
flashing red annunciation and the current level of CO in parts per million (ppm) are
displayed in the lower right corner of the Engine Page.

When a warning is generated, the CO RST Softkey becomes available to reset the
CO Guardian and acknowledge the alert.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00567-03 Rev. A 7

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Alerts Appendix Index

Annun/

Engine Indication System

Fuel Calculations Group

Flight

InstrumentsEIS

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and

are calculated from the last time the fuel was reset.

Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all
calculated based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer.
The fuel remaining can be adjusted using the following softkeys:

Nav/Com/

XPDR/AudioAFCSGPS Nav

• DEC FUEL – Decreases totalizer-based fuel remaining in one-gallon incre-
ments

• INC FUEL – Increases totalizer-based fuel remaining in one-gallon
increments

• RST FUEL – Resets totalizer-based fuel remaining to the aircraft’s fuel capacity
(98 gal or 102 gal usable) and sets the GAL USED display to zero

Flight

PlanningProcedures

Fuel

Remaining

Endurance
Calculation

Range
Calculation

Hazard

Fuel Used

Calculation

Avoidance

Fuel Calculations Group

Features

Additional

Engine Temperature Group

Abnormal

The temperature group displays the Cylinder Head Temperature (CHT) and Exhaust

Operation

Gas Temperature (EGT) in degrees Fahrenheit for each cylinder using bar graphs and
digital readouts. For the Cessna 400, Turbine Inlet Temperature (TIT) is shown on a
sliding bar scale.

AlertsAppendixIndex

Annun/

The following softkeys can be used to modify the display of engine temperature

information:

• DCLTR – Removes/displays the EGT and CHT readouts from the display

• ASSIST – Accesses the Engine Leaning Assist Mode

8

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Engine Indication System

Exhaust Gas
Temperature

Exhaust Gas
Temperature

Cylinder Head

Temperature

Engine Temperature Group (Cessna 350)

Turbine Inlet
Temperature

Cylinder Head

Temperature

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Engine Temperature Group (Cessna 400)

190-00567-03 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine Indication System

ENGINE LEANING ASSIST MODE

Flight

InstrumentsEIS

NOTE: Consult the Cessna 350/400 Aircraft Flight Manual (AFM) for leaning

procedures.

From the Engine Page, the Engine Leaning Assist Mode may be accessed by selecting
the ASSIST Softkey. Selecting the ASSIST Softkey again returns the MFD to the
Engine Page. Use the SYSTEM Softkey to exit the Engine Page.

Nav/Com/

XPDR/AudioAFCSGPS Nav

While in Assist Mode, the EIS Display is shown along with the Fuel Flow Gauge
and an expanded Engine Temperature Group.

Cessna 350

When the ASSIST Softkey is selected, the system initially highlights the

number and EGT readout of the cylinder with the hottest EGT.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Fuel Flow Gauge

EGT Deviation
from Peak

Engine Leaning Assist Mode (Cessna 350)

10

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

Engine Indication System

When the first peak is detected, the cylinder numbers disappear, “1st” is annunciated
in light blue below that cylinder’s EGT bar, the temperature is marked in light blue on
the graph, and the EGT readout is outlined.

Temperature Deviation from Peak

(First Cylinder)

Light

Blue Bar

Represents

Peak

Indicates

First

Cylinder

to Peak

Assist Mode - First Peaked Cylinder (Cessna 350)

The system continues to detect peak EGTs for each cylinder as the fuel flow is
decreased and the peak of each cylinder’s EGT is indicated by a light blue marker. The
last cylinder to peak is denoted by the “Last” annunciation below its bar on the graph
and the EGT readout is outlined in light blue.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Temperature Deviation from Peak

(Last Cylinder)

Indicates

Last

Cylinder to

Peak

Assist Mode - Last Peaked Cylinder (Cessna 350)

190-00567-03 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine Indication System

Cessna 400

Flight

Once the ASSIST Softkey is selected, the peak of each TIT is indicated by a light

InstrumentsEIS

blue bar which moves and remains at the peak Turbine Inlet Temperature.

Peak TIT

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

Lean or Rich

PlanningProcedures

From Peak

TIT Deviation

from Peak

Engine Leaning Assist Mode (Cessna 400)

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

12

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

190-00567-03 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

1)

Select the ADF/DME Softkey.

2)

Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.

3)

Turn the large FMS Knob to select the next desired field.

4)

Turn the small FMS Knob to enter the desired number.

5)

Repeat steps 3 and 4 until the desired ADF frequency is entered.

6)

Press the ENT Key to accept the new frequency.

7)

Press the ENT Key again to transfer the frequency to the active field.

8)

Turn the large FMS Knob to select the MODE field.

9)

Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.

10)

Press the ENT Key to complete the selection.

DME TUNING (OPTIONAL)

Nav/Com/XPDR/Audio Panel

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

1)

Select the ADF/DME or 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.

ENTER A TRANSPONDER CODE

1)

Select the XPDR Softkey to display the transponder mode selection
softkeys.

2)

Select the CODE Softkey to display the transponder code selection softkeys,
for digit entry.

3)

Select 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.

190-00567-03 Rev. A 13

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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
deselect the navigation radio audio source. All radio keys can be selected

Flight

PlanningProcedures

individually or together.

NAV/COM TUNING

, or

COM3 MIC Key (optional COM, if

, or

COM3 Key (optional COM, if installed) on the

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)

Hazard

Avoidance

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.

Features

3)

Additional

Press the Frequency Transfer Key to place the frequency into the active
frequency field.

DIGITAL CLEARANCE RECORDER AND PLAYER

Abnormal

Operation

AlertsAppendixIndex

Annun/

NOTE: Only the audio for the selected

not recorded for COM3 MIC.

• PressingthePLAY Key once plays the latest recorded memory block, then returns
to normal operation.

• PressingtheMKR/MUTE Key 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.

14

Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

COM MIC

Key is recorded. Audio is

190-00567-03 Rev. A