Garmin GPS Receiver TBM850 User Manual

G1000 Integrated Flight Deck

Cockpit Reference Guide

System Software 0719.06 or later

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Flight instruments

engine & AirFrAme sYstems

nAv/Com/trAnsponder/Audio pAnel

AutomAtiC Flight Control sYstem

gps nAvigAtion

Flight plAnning

proCedures

hAzArd AvoidAnCe

AdditionAl FeAtures

AbnormAl operAtion

AnnunCiAtions & Alerts

Appendix

index

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This manual reﬂects the operation of System Software version 0719.06 or later for the Socata TBM

850. Some differences in operation may be observed when comparing the information in this

manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200

Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411

Fax 503/364.2138

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,

Southampton, SO40 9RB, U.K.

Tel: 44/0870.8501241

Fax: 44/0870.8501251

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199

Fax: 886/02.2642.9099

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. WATCH^®,

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.

May, 2009

190-00708-02 Rev. A

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Warnings, Cautions & notes

WARNING: Navigation and terrain separation must NOT be predicated upon

the use of the terrain avoidance feature. The terrain avoidance feature is NOT

intended to be used as a primary reference for terrain avoidance and does

not relieve the pilot from the responsibility of being aware of surroundings

during ﬂight. The terrain avoidance feature is only to be used as an aid for

terrain avoidance. Terrain data is obtained from third party sources. Garmin

is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory

in nature and should not be relied upon as the sole source of obstacle and

terrain avoidance information. Always refer to current aeronautical charts

for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric

height above Mean Sea Level and could vary signiﬁcantly from the altitude

displayed by pressure altimeters, such as the GDC 74B Air Data Computer,

or other altimeters in the aircraft. GPS altitude should never be used for

vertical navigation. Always use pressure altitude displayed by the G1000

PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in

the G1000 system must be updated regularly in order to ensure that the

information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for

primary navigation. Basemap data is intended only to supplement other

approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: Trafﬁc information shown on system displays is provided as an

aid in visually acquiring trafﬁc. Pilots must maneuver the aircraft based only

upon ATC guidance or positive visual acquisition of conﬂicting trafﬁc.

WARNING: 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.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Warnings, Cautions & notes

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.

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 SocataTBM 850 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 NAVigationAID (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

SocataTBM 850Airplane Flight Manual. 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.

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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 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 ANTI-

REFLECTIVE 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 anti-

reﬂective 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.

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Warnings, Cautions & notes

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.

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Warnings, Cautions & notes

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record of revisions

part number

Change summary

190-00708-00

Initial Release

190-00708-01

Rev A

Added SVS and other GDU 9.02 parameters.

Rev B

Clerical changes

190-00708-02

Added temporary user waypoints

Added import/export ﬂight plans

Added CDI availability during Dead Reckoning mode

Added GDU 9.14 parameters.

revision date of revision Affected pages

description

Production release

May, 2009

All

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record of revisions

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RR-2

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table of Contents

Flight instruments ................................................................................................................ 1

s ele c ting the A ltimeter ba rometri c p ressure s ettin g ...................................................... 1

s ele c ting s t a nd a rd ba rometri c p ressure ............................................................................. 1

C h a nge A ltimeter ba rometri c p ressure s etting u nit s ...................................................... 1

sy n c hronizing the A ltimeter ba rometri c p ressure s ettings ........................................... 1

sy n c hronize Cdi ......................................................................................................................... 1

C h a nge na vig a tion s our c es ................................................................................................... 2

e n a ble /d is a ble obs m ode W hile na vig a ting w ith gps .................................................... 2

g eneri c t imer ............................................................................................................................. 2

C on ﬁ gure v speed b ugs ............................................................................................................ 2

s et ba rometri c/ra d a r A ltimeter m inimum d es c ent A ltitud e ......................................... 3

t esting the ra d a r A ltimeter ................................................................................................... 3

d ispl ay ing W ind da t a .............................................................................................................. 3

C h a nging hsi F orm a t ............................................................................................................... 4

engine & AirFrAme sYstems ............................................................................................. 5

e le c tri ca l sy stem ....................................................................................................................... 6

F uel sy ste m ................................................................................................................................ 8

g ener a l sy stems ....................................................................................................................... 9

nAv/Com/trAnsponder/Audio pAnel ....................................................................... 11

e nter or C h a nge F light id ..................................................................................................... 11

AdF t uning (o ption a l )............................................................................................................ 11

dme t uning ............................................................................................................................... 11

e nter a t r a nsponder C ode ..................................................................................................... 12

s ele c ting a Com ra di o .......................................................................................................... 12

s ele c ting a nAv ra di o ........................................................................................................... 12

nAv/Com t uning ..................................................................................................................... 12

i nter c om .................................................................................................................................... 13

pa ssenger A ddress (pA) sy stem ........................................................................................... 13

C le a r a n c e r e c order a nd p l ay er ........................................................................................... 13

AutomAtiC Flight Control sYste m .......................................................................... 15

F light d ire c tor Ac tiv a tion ..................................................................................................... 15

v erti ca l m odes ......................................................................................................................... 16

la ter a l m odes .......................................................................................................................... 17

gps nAvigAtio n ........................................................................................................................ 19

d ire c t -to na vig a tion .............................................................................................................. 19

Ac tiv a te a s tored F light p l a n ............................................................................................... 20

Ac tiv a te a F light p l a n l eg ..................................................................................................... 20

s top na vig a ting a F light p l a n .............................................................................................. 21

v erti ca l na vig a tion (vnAv)................................................................................................... 21

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table of Contents

Flight plAnnin g ...................................................................................................................... 23

W eight p l a nning ...................................................................................................................... 23

t rip p l a nnin g ............................................................................................................................ 23

C re a te a n e w u ser Way point d e ﬁ ned b y la titude & l ongitude ................................. 25

C re a te a n e w u ser Way point d e ﬁ ned b y ra di a ls f rom o ther Way points ................. 26

C re a te a n e w u ser Way point d e ﬁ ned b y a ra di a l & d ist a n c e f rom A nother

Way point ................................................................................................................................ 28

d elete a u ser Way point ......................................................................................................... 29

C re a te a n e w F light p l a n ...................................................................................................... 30

i mport a F light p l a n f rom a n sd Ca r d ................................................................................ 31

i nsert a Way point in the Ac tive F light p l a n ...................................................................... 31

e nter a n A ir way in a F light p l a n .......................................................................................... 32

i nvert A n Ac tive F light p l a n .................................................................................................. 33

r emove a d ep a rture , A rriv a l , A ppro ac h , or A ir way f rom a F light p l a n ..................... 33

s tore a F light p l a n .................................................................................................................. 34

e dit a s tored F light p l a n ....................................................................................................... 34

d elete a Way point f rom the F light p l a n ............................................................................ 34

i nvert a nd Ac tiv a te a s tored F light p l a n ........................................................................... 35

C op y a F light p l a n ................................................................................................................... 35

d elete a F light p l a n ................................................................................................................ 35

g r a phi ca l F light p l a n C re a tion ............................................................................................. 36

e xport a F light p l a n to a n sd Ca rd ..................................................................................... 36

proCedures ................................................................................................................................. 37

l o a d a nd Ac tiv a te a d ep a rture p ro c edure ....................................................................... 37

Ac tiv a te A d ep a rture l eg ..................................................................................................... 37

l o a d A n A rriv a l p ro c edure .................................................................................................... 37

Ac tiv a te A n A rriv a l l eg ......................................................................................................... 38

l o a d a nd /or Ac tiv a te a n A ppro ac h p ro c edure ................................................................. 38

Ac tiv a te A n A ppro ac h in the Ac tive F light p l a n ............................................................... 39

Ac tiv a te a v e c tor to F in a l A ppro ac h F ix ............................................................................ 39

Ac tiv a te A m issed A ppro ac h in the Ac tive F light p l a n ................................................... 40

hAzArd AvoidAnC e ................................................................................................................ 41

C ustomizing the ha z a rd d ispl ay s on the na vig a tion ma p ............................................ 41

stormsCope® (o ption a l ).................................................................................................... 41

xm W e a ther (o ption a l ).......................................................................................................... 43

t r afﬁc sy stems ........................................................................................................................ 44

t err a in A nd o bst ac le p roximit y ........................................................................................... 46

t err a in -sv s ............................................................................................................................... 47

t err a in Awa reness & Wa rning sy stem (tAWs) d ispl ay ................................................... 49

A irborne C olor W e a ther ra d a r ............................................................................................ 50

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table of Contents

AdditionAl FeAture s ........................................................................................................... 55

sy ntheti c v ision ....................................................................................................................... 55

t ermin a l p ro c edure C h a rts ................................................................................................... 56

xm^®radio e ntert a inment ..................................................................................................... 58

AbnormAl operAtion .......................................................................................................... 61

r eversion a r y m ode ................................................................................................................ 61

A bnorm a l Com o per a tion .................................................................................................... 61

ha z a rd d ispl ay s w ith l oss o f gps p osition ....................................................................... 61

u nusu a l A ttitudes ................................................................................................................... 62

d e a d r e ck oning ...................................................................................................................... 63

AnnunCiAtions & Alerts ................................................................................................... 65

CAs m ess a ges .......................................................................................................................... 65

C omp a r a tor A nnun c i a tions ................................................................................................... 68

r eversion a r y s ensor A nnun c i a tions ................................................................................... 68

AFCs A lert s ............................................................................................................................... 69

t err a in -svs A lerts ................................................................................................................... 70

t err a in -svs sy stem s t a tus A nnun c i a tion s ........................................................................ 71

tAWs A lert s .............................................................................................................................. 71

v oi c e A lerts .............................................................................................................................. 73

mFd & pFd m ess a ge A dvisories .......................................................................................... 74

da t a b a se m ess a ge A dvisories ............................................................................................. 75

gmA 1347d m ess a ge A dvisorie s ......................................................................................... 78

giA 63W m ess a ge A dvisorie s ............................................................................................... 79

geA 71 m ess a ge A dvisories .................................................................................................. 82

gtx 33/33d m ess a ge A dvisories .......................................................................................... 82

grs 77 m ess a ge A dvisories .................................................................................................. 83

gmu 44 m ess a ge A dvisories ................................................................................................ 85

gdl 69A m ess a ge A dvisorie s ............................................................................................... 85

gWx 68 A lert m ess a ges ......................................................................................................... 86

gdC 74b m ess a ge A dvisorie s ............................................................................................... 86

gCu 475 m ess a ge A dvisories ............................................................................................... 87

gmC 710 m ess a ge A dvisories .............................................................................................. 87

m is c ell a neous m ess a ge A dvisories ..................................................................................... 88

F light p l a n i mport /e xport m ess a ge s .................................................................................. 92

Appendix ....................................................................................................................................... 93

pFd s o f t k e y ma p .................................................................................................................... 93

mFd s o f t k e y ma p ................................................................................................................... 98

inde x .........................................................................................................................................Index-1

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table of Contents

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Flight instruments

seleCting the Altimeter bArometriC pressure setting

Turn the BARO Knob to select the desired setting.

seleCting stAndArd bArometriC pressure

Press the BARO Knob.

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.

sYnChronizing the Altimeter bArometriC pressure settings

1) Select the AUX-SYSTEM SETUP Page on the MFD.

2) Press the FMS Knob to activate the cursor.

3) Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION

Window.

4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.

sYnChronize Cdi

1) Select the AUX-SYSTEM SETUP Page on the MFD.

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.

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Flight instruments

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.

enAble/disAble obs mode While nAvigAting With gps

1) Select the OBS Softkey to select OBS Mode.

2) Turn a CRS Knob to select the desired course to/from the waypoint. Press

the CRS Knob to synchronize the Selected Course with the bearing to the

next waypoint.

3) Select the OBS Softkey again to disable OBS Mode.

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.

3) Press the ENT Key to START, STOP, or RESET the timer (if the timer is

counting DOWN, it will start counting UP after reaching zero). Press the

CLR Key or the TMR/REF Softkey to remove the window.

ConFigure vspeed bugs

1) Select 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).

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Flight instruments

4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF

ﬁeld

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.

set bArometriC/rAdAr Altimeter minimum desCent Altitude

1) Press the TMR/REF Softkey.

2) Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT ﬁeld to the

right of ‘MINIMUMS’.

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.

testing the rAdAr Altimeter

1) Select the AUX-SYSTEM STATUS Page on the MFD.

2) Select the RA TEST Softkey. 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) Select the PFD Softkey.

2) Select the WIND Softkey to display wind data below the Selected Heading.

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.

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Flight instruments

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.

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engine & Airframe systems

engine & AirFrAme sYstems

EIS Display (Reversionary Mode)

EIS Display (Normal Mode)

Torque

CAS Display

Fuel Flow

Propeller Speed

Generator Speed

Interturbine Temperature

Oil Pressure

Cabin Pressure Altitude and

Change Rate

Differential Pressure

Fuel Pressure

Battery and Generator

Currents

Selected Cabin Altitude

Oxygen Pressure

Fuel Quantity

Battery and Essential Bus

Voltages

Elevator, Aileron, and

Rudder Trim and Flap

Position

Oil Temperature

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engine & Airframe systems

eleCtriCAl sYstem

1) Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2) Select the ELEC Softkey to display the Electrical System Page.

Standby Generator

Main Generator

Battery

Battery Bus

Essential Bus

Power Buses

Main Bus

Ground Power

Unit Door

Emergency Switch

Electrical Synoptics Page

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engine & Airframe systems

Battery connection status to the main bus is indicated in green; direction of

current ﬂow is indicated with an arrow next to the current readout. If the battery is

disconnected from the main bus, the switch is closed. Battery overheating is indicated

in red with a ‘BAT OVHT’ annunciation; a CAS message is also generated.

Switch Open

Switch Closed

Main

Standby

Generator Switch Status

Battery Overheat Indication

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engine & Airframe systems

Fuel sYstem

1) Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2) Select the FUEL Softkey to display the Fuel System Page.

Left Fuel Tank

Left Fuel Line

Fuel Pressure

Auxiliary Boost Pump

Fuel Selector

Right Fuel Line

Fuel Flow Data

Right Fuel Tank

Fuel Synoptics Page

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engine & Airframe systems

Status of the fuel selector is indicated between the fuel tank symbols. The mode,

automatic (AUTO), manual (MAN), or off (no indication; CAS message ‘FUEL OFF’

generated) is shown beneath the fuel selector symbol.

Left Fuel

Tank

Selected

Switching

Fuel Tank Fuel Tank Fuel Tank

Selection Selected Selection

Right

Unknown

Fuel Selector Status

If the auxiliary fuel boost pump is on, the symbol is displayed in green. The mode,

automatic (AUTO) or manual (MAN) is displayed next to the pump symbol. If the

boost pump is off, the symbol is shown in light blue (automatic mode) or red (manual

mode).

generAl sYstems

1) Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2) Select the GEN Softkey to display the Fuel System Page.

The General Synoptics Page aircraft diagram displays open doors in red (CAS

messages also generated). Statuses of propeller, stall sensor heater, pitot probe, and

windshield heat are also indicated on the diagram:

• White indicates that heat is off (propeller and windshield)

• Light blue indicates heat has been selected (windshield)

• Green indicates heat is on

• Yellow indicates heat has failed (propeller, pitot tube, and stall sensor).

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engine & Airframe systems

General Synoptics Page

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nav/Com/xpdr/Audio panel

nAv/Com/trAnsponder/Audio pAnel

enter or ChAnge Flight id

1) Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the

Flight ID ﬁeld.

2) Turn the small FMS Knob to enter the ﬁrst character.

3) Turn the large FMS Knob to select the next ﬁeld.

4) Turn the small FMS Knob to enter the next desired character.

5) Repeat steps 3 and 4 until the desired Flight ID is entered.

6) Press the ENT Key to update the Flight ID. Do not perform any other

G1000 functions until ‘updating’ is no longer displayed.

AdF tuning (optionAl)

1) Press 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

1) Press 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.

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nav/Com/xpdr/Audio panel

enter A trAnsponder Code

1) Press the XPDR Softkey to display the transponder mode selection softkeys.

2) Press the XPDR1 or XPDR2 Softkey to select the active transponder.

3) Press the CODE Softkey to display the transponder code selection softkeys,

for digit entry.

4) Press the digit softkeys to enter the code in the code ﬁeld. When entering

the code, the next key in sequence must be pressed within 10 seconds, or

the entry is cancelled and restored to the previous code. Five seconds after

the fourth digit has been entered, the transponder code becomes active.

seleCting A Com rAdio

transmit/receive

Press the COM1 MIC or COM2 MIC on the audio panel.

receive only

Press the COM1 or COM2 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.

nAv/Com tuning

1) Press the small tuning knob to select the desired radio for tuning. A light

blue box highlights the radio frequency to be tuned.

2) Turn the respective tuning knobs to enter the desired frequency into the

standby frequency ﬁeld. The large knob enters MHz and the small knob

enters kHz.

3) Press the Frequency Transfer Key to place the frequency into the active

frequency ﬁeld.

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nav/Com/xpdr/Audio panel

interCom

Pressing the INTR COM Key on either Audio Panel selects and deselects the

intercom on both Audio Panels. The annunciator is lit when the intercom is active.

The intercom connects the pilot and copilot together. Either the pilot or copilot may

select or deselect the intercom.

The CABIN Key initiates two way communication between the pilot or copilot and

the passengers in the cabin. The annunciator is lit when the cabin intercom is active

on either Audio Panel.

The MAN SQ Key allows either automatic or manual control of the intercom

squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated

by the MAN SQ annunciator.

During manual squelch operation, pressing the ICS Knob switches between volume

and squelch adjustment, lighting the associated annunciator beneath the knob. When

the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When

the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.

pAssenger Address (pA) sYstem

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

INTR COM Key is enabled. PA messages are one way from the ﬂight deck to the

passengers.

CleArAnCe reCorder And plAYer

NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio

to the Pilot. Pressing the play key on the Copilot’sAudio Panel plays recorded

audio to the Copilot.

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 ﬂashes to indicate

when play is in progress. The PLAY annunciator turns off after playback is ﬁnished.

Pressing the PLAY Key once plays the latest recorded memory block and then

returns to normal operation. Pressing the PLAY Key again during play of a memory

block stops play. If a COM input signal is detected during play of a recorded memory

block, play is halted.

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nav/Com/xpdr/Audio panel

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.

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AFCs

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.

Modes Selected

Control Pressed

Lateral

Roll Hold (default)

Go Around

Vertical

Pitch Hold (default)

Go Around

FD Key

AP Key

ROL

PIT

ALT

CWS Button

GA Switch

ALT Key

Roll Hold (default)

ROL

Altitude Hold

VS Key

Vertical Speed

VNV Key

ROL Vertical Path Tracking* VPTH

GPS

NAV Key

BC Key

Navigation**

VOR

LOC

Pitch Hold (default)

PIT

Backcourse***

Pitch Hold (default)

Glidepath

PIT

GPS

VOR

LOC

APR Key

HDG Key

Approach**

Glideslope

Heading Select

HDG

Pitch Hold (default)

*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.

***The selected navigation receiver must have a valid LOC signal before BC Key press activates ﬂight

director.

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AFCs

vertiCAl modes

Vertical Mode

Description

Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

may be used to climb/descend to the (default)

Selected Altitude

PIT

AFCS armed to capture the altitude

displayed in the Selected Altitude

window

Selected Altitude

Armed

ALTS

Altitude Hold

Vertical Speed

Holds the current Altitude Reference

Maintains the current aircraft vertical

speed; may be used to climb/descend VS Key

ALT Key ALT nnnnn f T

VS nnnn f p m

to the Selected Altitude

Flight Level Change,

IAS Hold

Maintains the current aircraft airspeed

(in KIAS or Mach Number) while the

aircraft is climbing/descending to the

Selected Altitude

FLC

nnn k T

FLC Key

Flight Level Change,

Mach Hold

FLC M .nnn

VPTH

Captures and tracks the VNAV ﬂight

path

VNV

Key

VNAV

AFCS armed to capture the altitude

displayed in the VNAV Target Altitude

window

VNAV Target

Altitude Armed

ALTV

Captures and tracks the WAAS

glidepath on approach

Glidepath

Glideslope

APR Key

Captures and tracks the ILS glideslope

on approach

Commands a preprogrammed constant

pitch attitude and wings level in

preparation for takeoff

Takeoff

Switch

Disengages the autopilot and

commands a constant preprogrammed

pitch attitude and wings level

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

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AFCs

lAterAl modes

Lateral Mode

Description

Control Annunciation

Holds current aircraft roll attitude

or rolls wings level, depending on

commanded bank angle

Roll Hold

(default)

ROL

BANK

Key

Low Bank

Limits maximum commanded roll angle

Captures and tracks Selected Heading

HDG

Key

Heading Select

HDG

GPS

Navigation, GPS

Arm/Capture/Track

Navigation, VOR

Enroute Arm/

Capture/Track

Captures and tracks selected navigation

source (GPS, VOR, LOC)

NAV

Key

VOR

LOC

Navigation, LOC

Arm/Capture/Track

(No Glideslope)

Backcourse Arm/

Capture/Track

Captures and tracks a localizer signal

for backcourse approaches

BC Key

GPS

Approach, GPS

Arm/Capture/Track

Approach, VOR

Arm/Capture/Track

VAPP

Captures and tracks selected navigation

source (GPS, VOR, LOC)

APR Key

Approach, ILS Arm/

Capture/Track

(Glideslope Mode

automatically armed)

LOC

Commands a constant preprogrammed

constant pitch attitude and wings level

in preparation for takeoff

Takeoff

Switch

Disengages autopilot and commands

a preprogrammed constant pitch

attitude and wings level

Go Around

* 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.

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AFCs

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gps navigation

gps nAvigAtion

direCt-to nAvigAtion

direct-to navigation using the mFd

1) Press the Direct-to Key on the MFD Control Unit.

2) Enter the waypoint identiﬁer.

(

)

3) Press the ENT Key to conﬁrm the identiﬁer. The ‘Activate?’ ﬁeld is

highlighted.

4) If no altitude constraint or course is desired, press the ENT Key to activate.

To enter an altitude constraint, proceed to step 5.

5) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude ﬁeld.

6) Enter the desired altitude.

7) 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.

8) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

9) Press the ENT Key. The cursor is now ﬂashing in the VNV offset distance

ﬁeld.

10) Enter the desired offset distance before (-) the waypoint.

11) Press the ENT Key. The ‘Activate?’ ﬁeld is highlighted.

12) Press the ENT Key to activate.

direct-to navigation using the pFd

1) Press the Direct-to Key

(

)

on the PFD or controller.

2) Turn the large FMS Knob to place the cursor in the desired selection ﬁeld.

3) Turn the small FMS Knob to begin selecting the desired identiﬁer, location,

etc.

4) Press the ENT Key.

5) 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.

6) Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude ﬁeld.

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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’ ﬁeld.

11) Turn the small FMS Knob to enter the desired target altitude offset from

the selected Direct-to.

12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to

highlight the ‘CRS’ ﬁeld.

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 Key again to activate the Direct-to.

ACtivAte A stored Flight plAn

1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan

Catalog Page.

2) Press the FMS Knob to activate the cursor.

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.

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.

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) With ‘Activate’ highlighted, press the ENT Key.

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gps navigation

stop nAvigAting A Flight plAn

1) Press the FPL Key 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.

vertiCAl nAvigAtion (vnAv)

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.

Large White

Text

Large Light

Blue Text

Small Light

Blue Text

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

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gps navigation

Since altitudes loaded with an arrival procedure are published only for turbojet

aircraft, the altitudes are displayed as white text indicating that the altitudes are

displayed for reference only. An arrival waypoint altitude may be used (or “designated”)

as is, or changed to a different altitude. An altitude is designated by pressing the FMS

Knob and turning the large FMS Knob to place the cursor on the desired altitude and

pressing the ENT Key or entering a different value and pressing the ENT Key. The

altitude is now displayed as blue text, indicating that the altitude is now designated to

give vertical speed and deviation guidance.

Approach waypoint altitude constraints are designated in the same way as

previously described for arrivals. These altitudes are also displayed as blue text after

being designated for use. Waypoint altitude constraints may be designated up to, but

not including the FAF. The FAF is always a “reference only” altitude and cannot be

designated, unless the selected approach does not provide vertical guidance. In this

case, the FAF altitude can be designated.

White Text

Light Blue Text

Light Blue

Subdued Text

Altitude calculated by

the system estimating

the altitude of the

aircraft as it passes over for use in giving vertical

the navigation point. ﬂight path guidance.

This altitude is provided Altitude does not match

Altitude has been

entered by the pilot.

Altitude is designated

The system cannot

use this altitude

in determining

vertical ﬂight path

guidance.

Large Text

as a reference and is

not designated to be

used in determining

vertical ﬂight path

guidance.

the published altitude

in navigation database

or no published altitude

exists.

Altitude is not

Altitude is designated for The system cannot

use in giving vertical ﬂight use this altitude in

Small Text

designated to be used

in determining vertical

ﬂight path guidance.

Altitude has been

retrieved from the

navigation database

and is provided as a

reference.

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.

determining vertical

ﬂight path guidance.

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Flight planning

Flight plAnning

Weight plAnning

All procedures apply to the MFD unless otherwise stated.

entering Weight parameters

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 ﬁrst rectangular page icon.

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.

entering Fuel parameters

1) If necessary, press the FMS Knob to activate the cursor.

2) Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ ﬁeld.

3) Select the FOB SYNC Softkey to enter the fuel on board quantity as read

from the aircraft fuel quantity sensors.

Or:

Manually enter the desired fuel quantity.

4) Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ ﬁeld.

5) Enter the desired reserve fuel quantity.

6) Press the FMS Knob to remove the cursor.

trip plAnning

1) Turn the large FMS Knob to select the ‘AUX’ page group.

2) Turn the small FMS Knob to select the second rectangular page icon.

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.

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Flight planning

4) For Direct-to planning:

a) Select the WPTS Softkey and verify that the starting waypoint ﬁeld

indicates ‘P.POS’ (present position).

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.

d) Enter the identiﬁer of the ending waypoint and press the ENT Key to

accept the waypoint.

Or:

For point-to-point planning:

a) Enter the identiﬁer of the starting waypoint.

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.

d) Press the ENT Key to accept the waypoint.

Or:

For ﬂight plan leg planning:

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.

c) Turn the large FMS Knob to highlight the ‘LEG’ ﬁeld.

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’ displays 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.

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.

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.

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Flight planning

6) Enter the departure time. Press the ENT Key when ﬁnished. Departure time

may be entered in local or UTC time, depending upon system settings.

7) 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.

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.

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.

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.

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.

13) The ﬂashing cursor moves to the air temperature (TOTALAIRTEMP) 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.

CreAte A neW user WAYpoint deFined bY lAtitude & longitude

1) 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) Press the NEW Softkey. A waypoint is created at the current aircraft

position.

4) Enter the desired waypoint name.

5) Press the ENT Key.

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Flight planning

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.

a) Turn the large FMS Knob one click to the left to highlight

‘TEMPORARY’. This list is populated only when there is an active ﬂight

plan.

b) Press the ENT Key to place a check-mark in the box.

7) The cursor is now in the ‘WAYPOINT TYPE’ ﬁeld. Turn the small FMS Knob

to display a list of waypoint types.

8) Turn the small FMS Knob to select LAT/LON (latitude and longitude).

9) Press the ENT Key.

CreAte A neW user WAYpoint deFined bY rAdiAls From other

WAYpoints

1) Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page

group.

2) Turn the small FMS Knob to select the User WPT Information Page.

3) Press 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.

a) Turn the large FMS Knob one click to the left to highlight

‘TEMPORARY’. This list is populated only when there is an active ﬂight

plan.

b) Press the ENT Key to place a check-mark in the box.

7) The cursor is now 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.

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Flight planning

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:

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:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints

to the aircraft’s current position.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘RECENT’

waypoints.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12) Press the ENT Key.

13) Repeat step 10 to enter the next waypoint name.

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.

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Flight planning

15) Press the ENT Key.

16) Press the FMS Knob to remove the ﬂashing cursor.

CreAte A neW user WAYpoint deFined bY A rAdiAl & distAnCe From

Another WAYpoint

1) 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) Press 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.

a) Turn the large FMS Knob one click to the left to highlight

‘TEMPORARY’. This list is populated only when there is an active ﬂight

plan.

b) Press the ENT Key to place a check-mark in the box.

7) The cursor is now 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.

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:

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:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

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Flight planning

b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints

to the aircraft’s current position.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘RECENT’

waypoints.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12) Press the ENT Key.

13) The cursor is now displayed in the ‘DIS’ (distance) ﬁeld. Enter the desired

distance from the reference waypoint.

14) Press the ENT Key.

15) Press the FMS Knob to remove the ﬂashing cursor.

delete A user WAYpoint

1) Turn the large FMS Knob to select the ‘WPT’ page group.

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‘USERWAYPOINT LIST’

ﬁeld.

5) Turn the small FMS Knob to highlight the desired waypoint.

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Flight planning

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.

CreAte A neW Flight plAn

NOTE: When creating a new ﬂight plan in the Active Flight Plan Window,

the ﬁrst leg is activated automatically after it is created.

using the mFd

1) Press the FPL Key on the MFD Control Unit.

2) Turn the small FMS Knob to display the Flight Plan Catalog Page.

3) Select the NEW Softkey to display a blank ﬂight plan for the ﬁrst empty storage

location.

4) Turn the small FMS Knob to display the Waypoint Information Window.

5) Enter the identiﬁer of the departure waypoint.

6) Press the ENT Key.

7) Repeat step number 4, 5, and 6 to enter the identiﬁer for each additional

ﬂight plan waypoint.

8) 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.

using the pFd

NOTE: If a ﬂight plan is active, an additional ﬂight plan cannot be entered

using the PFD.

1) Press the FPL Key on the PFD.

2) Turn the small FMS Knob to display the Waypoint Information Page.

3) Turn the small FMS Knob to enter the ﬁrst letter of the destination waypoint

identiﬁer.

4) Turn the large FMS Knob to the right to move the cursor to the next character

position.

5) Repeat step 3 and 4 to spell out the rest of the waypoint identiﬁer.

6) Press the ENT Key and the cursor is now ready for entering of the next ﬂight

plan waypoint.

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Flight planning

7) Repeat steps 3 through 6 to enter the identiﬁer for each additional ﬂight plan

waypoint.

8) Once all waypoints have been entered, press the FMS Knob to remove the

cursor. The new ﬂight plan is now active.

import A Flight plAn From An sd CArd

1) Insert the SD card containing the ﬂight plan in the top card slot on the

MFD.

2) Press the FPL Key on the MFD 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) Press the IMPORT Softkey.

If an empty ﬂight plan is selected, a list of the available ﬂight plans on

the SD card will be displayed.

or:

If an existing ﬂight plan is selected, an ‘Overwrite existing ﬂight plan?

OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to

overwrite the selected ﬂight plan and see a list of the available ﬂight

plans on the SD card. If overwriting the existing ﬂight plan is not

desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select

another existing or empty ﬂight plan, and again press the IMPORT

Softkey.

7) Turn the small FMS Knob to highlight the desired ﬂight plan for importing.

8) Press the ENT Key.

insert A WAYpoint in the ACtive Flight plAn

1) Press the FPL Key to display the active ﬂight plan.

2) If necessary, press the FMS Knob to activate the cursor.

3) Turn the large FMS Knob to highlight the desired ﬂight plan waypoint. The

new waypoint is inserted before the highlighted waypoint.

4) Turn the small FMS Knob. The Waypoint Information Window is now

displayed.

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Flight planning

5) Enter the new ﬂight plan waypoint by one of the following:

a) Enter the user waypoint identiﬁer, facility, or city.

b) Press the ENT Key.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

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.

Or:

a) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list

is displayed.

b) Turn the small FMS Knob to the right to display the ‘RECENT’

waypoints.

c) Turn the large FMS Knob to select the desired waypoint.

d) Press the ENT Key.

e) Press the ENT Key again to “accept” the waypoint.

enter An AirWAY in A Flight plAn

1) Press the FPL Key.

2) Press the FMS Knob to activate the cursor (not required on the PFD).

3) Turn the large FMS Knob to highlight the waypoint ﬁeld after the desired

airway entry point. If this previous 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”. 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.

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Flight planning

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.

invert An ACtive Flight plAn

1) Press the FPL Key to display the 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.

remove A depArture, ArrivAl, ApproACh, or AirWAY From A Flight

plAn

1) Press the FPL Key to display the active ﬂight plan. Press the FMS Knob to

activate the cursor.

Or, for a stored ﬂight plan:

a) Press the MFD FPL Key and 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.

d) Select the EDIT Softkey.

2) 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.

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Flight planning

store A Flight plAn

1) 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.

edit A stored Flight plAn

1) Press the FPL Key for the MFD 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, for a stored ﬂight plan:

a) Press the FPL Key of the MFD and 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.

d) Select the EDIT Softkey.

2) Turn the large FMS Knob to highlight the waypoint to be deleted.

3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation

window.

4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel

the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press

the ENT Key.

5) Once all changes have been made, press the FMS Knob to remove the

cursor.

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Flight planning

invert And ACtivAte A stored Flight plAn

1) Press the FPL Key for the MFD.

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?’ is

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.

CopY A Flight plAn

1) Press the FPL Key for the MFD.

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.

delete A Flight plAn

1) Press the FPL Key for the MFD.

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.

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Flight planning

grAphiCAl Flight plAn CreAtion

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.

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 is 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

1) Insert the SD card into the top card slot on the MFD.

2) Press the FPL Key on the MFD 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) Press the EXPORT Softkey.

7) Press the ENT Key to conﬁrm the export.

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procedures

proCedures

loAd And ACtivAte A depArture proCedure

1) Press the PROC Key.

2) 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 is active when

the ﬂight plan is active.

ACtivAte A depArture leg

1) Press the FPL Key for the MFD 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 departure.

4) Select the ACT LEG Softkey. A conﬁrmation window showing the selected

leg is displayed.

5) With ‘ACTIVATE’ highlighted, press the ENT Key.

loAd An ArrivAl proCedure

1) 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.

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procedures

4) Turn the large FMS Knob to highlight the desired arrival.

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 may be displayed for the selected

arrival.

8) Turn the large FMS Knob to highlight the desired runway.

9) Press the ENT Key.

10) With ‘LOAD?’ highlighted, press the ENT Key.

11) The arrival becomes part of the active ﬂight plan.

ACtivAte An ArrivAl leg

1) Press the FPL Key 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 (WAAS, 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.

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procedures

6) Turn either FMS Knob to select the desired transition. The “Vectors”

option assumes vectors will be received to the ﬁnal course segment of

the approach and will provide navigation guidance relative to the ﬁnal

approach course.

7) Press the ENT Key. The cursor moves to the MINIMUMS ﬁeld.

8) If desired, the DA/MDA for the selected approach procedure may be

entered and displayed on the PFD. Turn the small FMS Knob in the

direction of the green arrow to change the display from OFF to BARO.

9) Press the ENT Key. The cursor moves to the altitude ﬁeld. Turn the small

FMS Knob to enter the published DA/MDA for the selected approach

procedure.

10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’

highlighted.

11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.

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.

12) Press the ENT Key.

ACtivAte An ApproACh in the ACtive Flight plAn

1) Press the PROC Key.

2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.

3) Press the ENT Key.

ACtivAte A veCtor to FinAl ApproACh Fix

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.

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procedures

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 is displayed.

4) With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the go-around button.

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hazard Avoidance

hAzArd AvoidAnCe

Customizing the hAzArd displAYs on the nAvigAtion mAp

1) 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.

stormsCope® (optionAl)

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.

displaying stormscope lightning data on the navigation map page

1) Press the MAP Softkey.

2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove

Stormscope Lightning Data from the Navigation Map Page.

Lightning Age

Symbol

Strike is less than 6 seconds old

Strike is between 6 and 60 seconds old

Strike is between 1 and 2 minutes old

Strike is between 2 and 3 minutes old

Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode

1) With the Weather Group selected, press the ENT Key. The cursor ﬂashes on

‘STRMSCP LTNG’.

2) Turn the large FMS Knob to select ‘STRMSCP MODE’.

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hazard Avoidance

3) Turn the small FMS Knob to display the ‘Cell/Strike’ window.

4) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.

5) Push the Fms Knob to return to the Navigation Map Page.

Clear Stormscope Lightning Data from 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.

NOTE: If heading input is lost, strikes and/or cells must be cleared manually

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.

stormscope page

1) Turn the large FMS Knob until the Map Page group is selected.

2) Turn the small FMS Knob until the Stormscope Page is selected.

Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’

1) Select the Stormscope Page.

2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.

Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey

to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box

located in the upper left corner of the Stormscope Page.

NOTE:“Cell mode”uses a clustering program to identify clusters of electrical

activity that indicate cells.

Change the Viewing Mode Between 360˚ and 120˚

1) Select the Stormscope Page.

2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press

the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to

display a 120˚ viewing area.

Press the CLEAR Softkey to remove all Stormscope lightning data from the

display.

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hazard Avoidance

xm WeAther (optionAl)

WARNING: Use of XM weather for hazardous weather penetration is not

recommended. Weather information provided by XM Radio Service is

approved only for weather avoidance, not penetration.

displaying xm Weather on the navigation map page

1) Select the MAP Softkey.

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.

display metAr and tAF information on the Airport information page

1) Turn the large FMS Knob to select the WPT Page Group.

2) Turn the small FMS Knob to select the Airport Information Page.

3) Select the WX Softkey to display METAR and TAF text (METAR and TAF

information is updated every 12 minutes).

displaying Weather on the Weather data link page

1) 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 XM weather product.

4) Select the LEGEND Softkey to view the legends for the selected products.

If necessary, turn either FMS Knob to scroll through the list. Press the small

FMS Knob or the ENT Key to return to the map.

map panning information – Weather data link page

1) Push in the Joystick to display the panning arrow.

2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,

or SIGMETs.

3) Press the ENT Key to display pertinent information for the selected product.

Note that pressing the ENT Key when panning over an AIRMET or a

SIGMET displays an information box that shows the text of the report.

Panning over an airport with METAR information does not display more

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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

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Cyclone Warnings

Freezing Levels

City Forecast

AIREPs

Cell Movement

Icing Potential

XM Lightning

METARs Surface Analysis

County Warnings

Turbulence PIREPs

NEXRAD

Cloud Top

Winds Aloft

SIGMETs/AIRMETs

trAFFiC sYstems

• If Trafﬁc information Service (TIS) is conﬁgured, STANDBY, OPERATE, and

TNA MUTE softkeys are displayed.

• If a Trafﬁc Advisory System (TAS) is conﬁgured, STANDBY, NORMAL, TEST,

and ALT MODE softkeys are displayed.

Trafﬁc Symbol

Description

Non-Threat Trafﬁc

(intruder is beyond 5 nm and greater than 1200’ vertical separation)

Proximity Advisory (PA) (Not available with TIS system)

(intruder is within 5 nm and less than 1200’ vertical separation)

Trafﬁc Advisory (TA)

(closing rate, distance, and vertical separation meet TA criteria)

Trafﬁc Advisory Off Scale

Trafﬁc Symbol Description

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trafﬁc information service (tis)

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.

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) Press the OPERATE Softkey to begin displaying trafﬁc. ‘OPERATING’ is

displayed in the Trafﬁc Mode ﬁeld.

4) Press the STANDBY Softkey to place the system in the Standby Mode.

‘STANDBY’ is displayed in the Trafﬁc Mode ﬁeld.

5) Rotate the Joystick clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

6) Press the TNA MUTE Softkey to mute the “Trafﬁc Not Available” aural

alert.

Displaying Trafﬁc on the Navigation Map

1) Ensure TIS is operating. With the Navigation Map displayed, press the

MAP Softkey.

2) Press the TRAFFIC Softkey. Trafﬁc is now displayed on the map.

trafﬁc Advisory system (tAs) (optional)

System Self Test

1) Set the range to 2/6 nm.

2) Select the STANDBY Softkey.

3) Select the TEST Softkey.

4) Self test takes approximately eight seconds to complete. When completed

successfully, trafﬁc symbols are displayed and a voice alert “TAS System Test

OK” is heard. If the self test fails, the system reverts to Standby Mode and

a voice alert “TAS System Test Fail” is heard.

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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 second rectangular page icon.

3) Select the NORMAL Softkey to begin displaying trafﬁc. ‘OPERATING’ is

displayed in the Trafﬁc Mode ﬁeld.

4) Select the ALT MODE Softkey to change the altitude volume. Select the

desired altitude volume by pressing 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’ is displayed in the Trafﬁc Mode ﬁeld.

6) Rotate the Joystick clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

Displaying Trafﬁc on the Navigation Map

1) Ensure TAS is operating.

2) With the Navigation Map displayed, select the MAP Softkey.

3) Select the TRAFFIC Softkey. Trafﬁc is now displayed on the map.

terrAin And obstACle proximitY

NOTE: Terrain data is not displayed when the aircraft latitude is greater than

75 degrees north or 60 degrees south.

displaying terrain and obstacles on the terrain proximity page

1) Turn the large FMS Knob to select the Map Page Group.

2) Turn the small FMS Knob to select the last rectangular page icon.

3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys.

When the ARC Softkey is pressed, a radar-like 120° view is displayed. Press

the 360 Softkey to return to the 360° default display.

4) Rotate the Joystick clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

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Color

Terrain/Obstacle Location

Terrain/Obstacle above or within 100’

below current aircraft altitude.

Red

Terrain/Obstacle between 100’ and

1000’ below current aircraft altitude.

Yellow

Black

Terrain/Obstacle is more than 1000’

below aircraft altitude.

displaying terrain and obstacles on the navigation map

1) With the Navigation Map displayed, press the MAP Softkey.

2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be

displayed on the map.

terrAin-svs

NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)

option is installed and the TAWS option has not been installed.

NOTE: Terrain data is not displayed when the aircraft latitude is greater than

75 degrees north or 60 degrees south.

display terrain on the terrAin-svs page

1) Turn the large FMS Knob to select the Map Page Group.

2) Turn the small FMS Knob to select the Terrain-SVS Page.

3) If desired, press the VIEW Softkey to access the ARC and 360 softkeys.

When the ARC Softkey is selected, a radar-like 120° view is displayed.

Press the 360 Softkey to return to the 360° default display.

4) Rotate the Joystick clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

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Color

Terrain/Obstacle Location

Terrain/Obstacle above or within 100’

below current aircraft altitude.

Red

Yellow

Black

Terrain/Obstacle between 100’ and

1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

enable/disable Aviation data

1) While the Terrain-SVS 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.

terrain-svs inhibit

Inhibit Terrain

While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.

Or:

1) Press the MENU Key.

2) Turn the small FMS Knob to select ‘Inhibit Terrain’.

3) Press the ENT Key.

Enable Terrain

While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.

1) While the Terrain-SVS Page is displayed, press the MENU Key.

2) Turn the small FMS Knob to select ‘Enable Terrain’.

3) Press the ENT Key.

NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the

active waypoint in a GPS WAAS 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.

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terrAin AWAreness & WArning sYstem (tAWs) displAY

WARNING:TheTAWS display shows supplemental information only. It should

not be used for navigation.

NOTE: Terrain data is not displayed when the aircraft latitude is greater than

75 degrees north or 60 degrees south.

NOTE: TAWS operation is only available when the G1000 is conﬁgured for a

TAWS-B installation.

manual system test

1) While the TAWS-B Page is displayed, press the MENU Key.

2) Turn the small FMS Knob to select ‘Test TAWS’.

3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center

of the TAWS-B Page.

When all is in working order, “TAWS System Test, OK” is heard.

display terrain on the tAWs-b page

1) Turn the large FMS Knob to select the Map Page Group.

2) Turn the small FMS Knob to select the TAWS-B Page.

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 display a larger area or rotate counter-

clockwise to display a smaller area.

Color

Terrain/Obstacle Location

Terrain/Obstacle above or within 100’

below current aircraft altitude.

Red

Terrain/Obstacle between 100’ and

1000’ below current aircraft altitude.

Yellow

Black

Terrain/Obstacle is more than 1000’

below aircraft altitude.

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enable/disable Aviation data

1) 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.

tAWs inhibit

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active

waypoint in a GPS WAAS 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.

Inhibit TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

Or:

1) Press the MENU Key.

2) Turn the small FMS Knob to select ‘Inhibit TAWS’.

3) Press the ENT Key.

Enable TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

1) 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.

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.

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.

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displaying Weather on the Weather radar page

1) Turn the large FMS Knob to select the Map Page Group.

2) Turn the small FMS Knob to select the Weather Radar Page.

3) Select the MODE Softkey.

4) If the aircraft is on the ground, select the STANDBY Softkey to initiate the

one minute warm-up period. After the warm-up is complete, the radar will

enter the Standby Mode. After the aircraft is airborne, select the WEATHER

Softkey.

If the aircraft is already airborne, select the WEATHER or GROUND

Softkey. The one-minute warm-up period will be initiated, after which the

radar will begin transmitting. The horizontal scan is initially displayed.

5) Turn the Joystick to select the desired range.

6) If desired, select the VERTICAL Softkey for vertical scanning.

Adjusting Antenna tilt

Move the Joystick up or down to adjust the tilt of the antenna up or down.

Monitor the displayed tilt value in the TILT ﬁeld.

When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt

of the antenna. If the Tilt Line is not displayed, perform the following steps:

1) Press the MENU Key

2) Turn the large FMS Knob to select ‘Show Tilt Line’.

3) Press the ENT Key.

Adjusting Antenna bearing

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.

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Vertically Scan a Storm Cell

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.

2) Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now

be displayed.

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

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.

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.

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.

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sector scan

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.

Antenna stabilization

1) To activate or deactivate the antenna stabilization, select the MODE

Softkey.

2) Select the STAB ON Softkey to activate antenna stabilization or select

the STAB OFF Softkey to deactivate. The current stabilization condition is

shown in the upper right of the weather radar display.

Weather Attenuated Color highlight (WAtCh^®)

To activate or deactivate the WATch^®feature, select the WATCH Softkey. This

feature is only available in the Horizontal Scan Mode.

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating

and deactivating will also enable or inhibit the alert on the PFD.

Automatic standby

When the weather radar system is in the Weather or Ground Map Mode, upon

landing the system will automatically switch to Standby Mode.

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Blank Page

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Additional Features

AdditionAl FeAtures

sYnthetiC vision

WARNING: Use appropriate primary systems for navigation, and for terrain,

obstacle, and trafﬁc avoidance. SVS is intended as an aid to situational

awareness only and may not provide the accuracy and/or ﬁdelity upon which

to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or

trafﬁc.

Synthetic Vision System (SVS) functionality is offered as an optional enhancement

to the G1000 Integrated Flight Deck System.

SVS is primarily comprised of a computer-generated forward-looking, attitude

aligned view of the topography immediately in front of the aircraft from the pilot’s

perspective. SVS information is shown on the primary ﬂight display (PFD).

SVS offers a three-dimensional view of terrain and obstacles. Terrain and

obstacles that pose a threat to the aircraft in ﬂight are shaded yellow or red.

In addition to SVS enhancement to the PFD, the following feature enhancements

have been added to the PFD:

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Trafﬁc

• Airport Signs

• Runway Display

displaying synthetic terrain

1) Press the PFD Softkey.

2) Press the SYN VIS Softkey.

3) Press the SYN TERR Softkey.

4) Press the BACK Softkey to return to the previous page.

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Additional Features

displaying pathways

1) 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.

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.

displaying Airport signs

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^®in

electronic form, it is still advisable 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

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Additional Features

ID, the VOR symbol, and intersection names if within the airport plan view. Pressing

the DCLTR Softkey a third time removes the airport runway layout, unless the airport

in view is part of an active route structure. Pressing the DCLTR Softkey again cycles

back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.

These diagrams aid in following ground control instructions by accurately displaying

the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and

services. This database is updated on a 56-day cycle.

Chartview

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.

FliteCharts^®

FliteCharts^®resemble the paper version of National Aeronautical charting Ofﬁce

(NACO) 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.

view Charts from the navigation map page

1) Select the SHW CHRT Softkey when displayed.

Move the map pointer to point to a desired point on the map and select the

SHW CHRT Softkey.

2) 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.

3) Select the GO BACK Softkey to return to the previous page.

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Additional Features

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 is displayed, if

available for the item selected.

4) Select the GO BACK Softkey to return to the previous page.

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.

xm^®rAdio entertAinment

The XM^®Radio Page provides information and control of the audio entertainment

features of the XM Satellite Radio.

selecting the xm radio page

1) 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.

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Additional Features

Active Channel and Channel list

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

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.

Turn the small FMS Knob to display the ‘Categories’ list. Highlight the

desired category with the small FMS Knob.

3) Press the ENT Key.

select an Available Channel within the selected Category

1) While on the XM Radio Page, select the CHNL Softkey.

2) Select the CH + Softkey to go up through the list in the Channel Box, or

move down the list with the CH – Softkey.

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.

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.

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Additional Features

Assigning Channel presets

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). Pressing the

MORE Softkey repeatedly cycles through the preset channels.

3) Select any one of the (PS1 - PS15) softkeys to assign a number to the

active channel.

4) Select the SET Softkey on the desired channel number to save the channel

as a preset.

Adjusting volume

1) With the XM Radio Page displayed, select the VOL Softkey.

2) Select the VOL – Softkey to reduce volume or select the VOL + Softkey to

increase volume. (Once the VOL Softkey is selected, the volume can also be

adjusted using the small FMS Knob.)

3) Select the MUTE Softkey to mute the audio. Select the MUTE Softkey

again to unmute the audio.

XM Radio volume may also be adjusted on each passenger headset.

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Abnormal operation

AbnormAl operAtion

reversionArY mode

Reversionary mode must be entered manually in the case of PFD1, PFD2,

or MFD failure. In reversionary mode, critical ﬂight instrumentation is combined

with engine instrumentation on the remaining display.

Activation of reversionary display mode is accomplished by pressing the DISPLAY

BACKUP Button on the appropriate audio panel.

• PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.

• MFD – By pressing the DISPLAY BACKUP Button on the left or the right

audio panel.

• PFD2 – By pressing the DISPLAY BACKUP Button on the right audio

panel.

NOTE: The Socata TBM 850 Airplane Flight Manual (AFM) always takes

precedence over the information found in this section.

AbnormAl Com operAtion

When a COM tuning failure is detected by the system, the emergency frequency

(121.500 Mhz) is automatically loaded into the active frequency ﬁeld of the COM

radio for which the tuning failure was detected. In the event of a failure of both PFDs,

the emergency frequency (121.500 MHz) automatically becomes the active frequency

on both COM radios.

hAzArd displAYs With loss oF gps position

If GPS position is lost, or becomes invalid, selected hazards being displayed on the

Navigation Map Page are removed until GPS position is again established.

Loss of Hazard Functions with Loss of GPS

Position

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Abnormal operation

unusuAl Attitudes

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary

functions are displayed in these situations.

The following information is removed from the PFD (and corresponding softkeys

are disabled) when the aircraft experiences unusual attitudes:

• Trafﬁc Annunciations

• AFcS Annunciations

• Flight Director

Command Bars

• System Time

• Glideslope, Glidepath,

and Vertical Deviation

Indicators

• Altimeter Barometric

Setting

• PFD Setup Menu

• Windows displayed in

the lower right corner

of the PFD:

• Inset Map

• Temperatures

• DME Information

Window

– Timer/References

– Nearest Airports

– Flight Plan

• Selected Altitude

• VNV Target Altitude

• Wind Data

– Messages

• Selected heading Box

• Selected course Box

• Transponder Status

Box

– Procedures

– ADF/DME Tuning

• Barometric Minimum

Descent Altitude Box

Extreme Pitch Indication

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Abnormal operation

deAd reCkoning

While in Enroute or Oceanic phase of ﬂight, if the G1000 detects an invalid GPS

solution or is unable to calculate a GPS position, the system automatically reverts to

Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position

combined with continuously updated airspeed and heading data (when available) to

calculate and display the aircraft’s current estimated position.

NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic

(OCN) phase of ﬂight. In all other phases, an invalid GPS solution produces

a “NO GPS POSITION” annunciation on the map and the G1000 stops

navigating in GPS Mode.

DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’

superimposed in yellow over the ‘own aircraft’ symbol as shown in the following

ﬁgure. In addition, ‘DR’ is prominently displayed, also in yellow, on the hSI slightly

above and to the right of the aircraft symbol on the CDI as shown in the following

ﬁgure. The cDI deviation bar is displayed in yellow, but will be removed from the

display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message

appears on the PFD.

Normal navigation using GPS/WAAS source data resumes automatically once a

valid GPS solution is restored.

It is important to note that estimated navigation data supplied by the G1000 in

DR Mode may become increasingly unreliable and must not be used as a sole means

of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or

not available, the DR function is not be capable of estimating your position and,

consequently, the system may display a path that is different than the actual movement

of the aircraft. Estimated position information displayed by the G1000 through

DR while there is no heading and/or airspeed data available should not be used for

navigation.

DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the

lack of satellite measurements needed to determine a position. Changes in wind speed

and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this

degraded accuracy, the crew must maintain position awareness using other navigation

equipment until GPS-derived position data is restored.

190-00708-02 Rev. A

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Abnormal operation

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Dead Reckoning Indications

As a result of operating in DR Mode, all GPS-derived data is computed based upon

an estimated position and is displayed as yellow text on the display to denote degraded

navigation source information. This data includes the following:

• Navigation Status Box ﬁelds except Active Leg, TAS, and DTK

• GPS Bearing Pointer

• Wind data and pointers in the Wind Data Box on the PFD

• current Track Indicator

• All Bearing Pointer Distances

• Active Flight Plan distances, bearings, and ETE values

Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20

minutes. Terrain Proximity, TERRAIN-SVS, and TAWS are also disabled. Additionally,

the accuracy of all nearest information (airports, airspaces, and waypoints) is

questionable. Finally, airspace alerts continue to function, but with degraded

accuracy.

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Annunciations & Alerts

AnnunCiAtions & Alerts

CAs messAges

Warning messages

Inhibits

Messages

Comments

BAT OVERHEAT

BLEED TEMP

CABIN ALTITUDE Cabin altitude over 10,000 ft

Battery temperature over 70°C

Bleed temperature high

CABIN DIFF PRESS Cabin pressure differential over 6.2 psi

DOOR

Pilot or cabin door open

Engine compartment ﬁre (temperature over

200°C; if installed)

FIRE

FLAPS ASYM

FUEL OFF

Dissymmetry between left- and right-hand ﬂaps

Fuel tank selectors set to “Off”

FUEL PRESS

Fuel pressure below 10 psi

Engine start: ITT over 1000°C, 870°C (5 s), or

840°C (20 s)

ITT

Engine running: ITT over 840°C

OIL PRESS

OXYGEN

PARK BRAKE

Oil pressure below 60 psi

Oxygen cylinder closed

Parking brake applied

Torque greater than or equal to 121.4%

maximum torque

TORQUE

190-00708-02 Rev. A

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Annunciations & Alerts

Caution messages

Inhibits

Messages

Comments

AUTO SEL

Fuel timer off or out of service

Electric fuel pump running (manual or

automatic mode)

AUX BOOST PMP ON

BAT AMP

BAT OFF

Battery current over 50 A while on ground

Battery off

X X X

Flow control and shut-off valve/shut-off

valve closed

Oil chip detector on (if installed)

BLEED OFF

CHIP

FRONT CARGO DOOR Forward baggage door open

Fuel tanks imbalanced by more than 15

USGAL for >30 seconds

Fuel quantity less than or equal to 9.1

USGAL in speciﬁed tank

FUEL IMBALANCE

FUEL LOW L-R*

GPU DOOR

IGNITION

INERT SEP FAIL

INERT SEP ON

GPU receptacle door not closed

Ignition exciter running

Inertial separator failure

Inertial separator extended

Low fuel level sensor failure for speciﬁed

tank

Battery voltage below 26 V

Starter generator unconnected

Oil pressure between 60 and 100 psi

LOW LVL FAIL L-R*

LOW VOLTAGE

MAIN GEN

OIL PRESS

Oil temperature below 0°C or above

104°C

OIL TEMP

Speciﬁed pitot heat (left or right) on while

engine off

Speciﬁed pitot heat (left or right) off

Prop deice selected and not on

Prop deice on while engine off

PITOT HT ON L-R*

PITOT NO HT L-R*

PROP DEICE FAIL

PROP DEICE ON

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

Inhibits

Messages

Comments

REAR CARGO DOOR Rear cargo door open

STALL HEAT ON

STALL NO HEAT

STARTER

Stall warning heat on while engine off

Stall warning heat off

Starter generator running

VACUUM LOW

Vacuum pressure less than 3.75 in Hg

* Only affected side (L, R, or L-R) displayed in CAS message; applicable messages listed here display

L-R for example

Inhibits prevent certain CAS messages from being displayed during the following

conditions:

• Engine off

• Aircraft in air (AIR)

• Engine on

• Landing Operation Phase Inhibit

(LOPI)

• Aircraft on ground (Ground)

• Takeoff Operation Phase Inhibit

(TOPI)

190-00708-02 Rev. A

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Annunciations & Alerts

CompArAtor AnnunCiAtions

Comparator

Window text

Condition

Difference in altitude sensors is > 200 ft.

ALT MISCOMP

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.

If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7

kts.

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors.

HDG MISCOMP

PIT MISCOMP

ROL MISCOMP

ALT NO COMP

IAS NO COMP

HDG NO COMP

PIT NO COMP

ROL NO COMP

reversionArY sensor AnnunCiAtions

reversionary

sensor Window

text

Condition

Both PFDs are displaying data from the number one Air Data Computer.

Both PFDs are displaying data from the number two Air Data Computer.

BOTH ON ADC1

BOTH ON ADC2

BOTH ON AHRS1

Both PFDs are displaying data from the number one Attitude & Heading Reference

System.

Both PFDs are displaying data from the number two Attitude & Heading Reference

System.

BOTH ON AHRS2

Both PFDs are displaying data from the number one GPS receiver.

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.

BOTH ON GPS1

BOTH ON GPS2

USING ADC1

USING ADC2

USING AHRS1

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

reversionary

sensor Window

text

Condition

PFD1 is displaying data from the #2 AHRS.

USING AHRS2

USING GPS1

USING GPS2

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

AFCs Alerts

Alert Condition

Annunciation

Description

Rudder Mistrim Right

Yaw servo providing sustained force in the

indicated direction

Rudder Mistrim Left

Aileron Mistrim Right

Aileron Mistrim Left

Elevator Mistrim Down

Elevator Mistrim Up

Roll servo providing sustained force in the

indicated direction

Pitch servo providing sustained force in the

indicated direction

If AP engaged, take control of the aircraft and

disengage AP

Pitch Trim Failure

If AP disengaged, move MEPT switches separately

to check if a stuck switch is causing the annunciation

If AP engaged, take control of the aircraft and

disengage AP

(or stuck MEPT Switch)

Yaw Trim Failure

If AP disengaged, move the MEYT switch to check

if a stuck switch is causing the annunciation

(or stuck MEYT Switch)

Yaw Damper Failure

Roll Failure

YD control failure; AP still operative

Roll axis control failure; AP inoperative

Pitch axis control failure; AP inoperative

Pitch Failure

AP and MEPT are unavailable; FD may still be

available

System Failure

190-00708-02 Rev. A

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Annunciations & Alerts

Alert Condition

Annunciation

Description

Performing preﬂight system test; aural alert sounds

at completion

Do not press the AP DISC Switch during servo

power-up and preﬂight system tests as this may

cause the preﬂight system test to fail or never to

start (if servos fail their power-up tests). Power

must be cycled to the servos to remedy the

situation.

Preﬂight Test

Preﬂight system test failed; aural alert sounds at

failure

terrAin-svs Alerts

PFD/MFD

TERRAIN-SVS

Page

MFD

Pop-Up Alert

Aural

Message

Alert Type

Annunciation

Reduced Required Terrain

Clearance Warning (RTC)

“Warning;Terrain,

Terrain”

Imminent Terrain Impact

Warning (ITI)

“Warning;Terrain,

Terrain”

Reduced Required Obstacle

Clearance Warning (ROC)

“Warning; Obstacle,

Obstacle”

Imminent Obstacle Impact

Warning (IOI)

“Warning; Obstacle,

Obstacle”

Reduced Required Terrain

Clearance Caution (RTC)

“Caution;Terrain,

Terrain”

Imminent Terrain Impact

Caution (ITI)

“Caution;Terrain,

Terrain”

Reduced Required Obstacle

Clearance Caution (ROC)

“Caution; Obstacle,

Obstacle”

Imminent Obstacle Impact

Caution (IOI)

“Caution; Obstacle,

Obstacle”

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

terrAin-svs sYstem stAtus AnnunCiAtions

PFD/MFD

Alert Type

System Test fail

TERRAIN-SVS Page

Annunciation

Aural Message

“Terrain System Failure”

None

Terrain Alerting is disabled

No GPS position or excessively

degraded GPS signal

“Terrain System Not Available”

“Terrain Available” will be

heard when sufﬁcient GPS

signal is re-established.

System Test in progress

System Test pass

None

Chime

tAWs Alerts

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

Alert Type

Aural Message

Excessive Descent

“Pull Up”

Rate Warning (EDR)

Reduced Required

Terrain Clearance

Warning (RTC)

“Terrain, Terrain; Pull Up,

Pull Up”

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Imminent Terrain

Impact Warning (ITI)

Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

Reduced Required

Obstacle Clearance

Warning (ROC)

“Obstacle, Obstacle; Pull

Up, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

190-00708-02 Rev. A

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Annunciations & Alerts

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

Alert Type

Aural Message

Imminent Obstacle

Impact Warning

(IOI)

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

Reduced Required

Terrain Clearance

Caution (RTC)

“Caution, Terrain; Caution,

Terrain”

“Terrain Ahead;Terrain

Ahead”

Imminent Terrain

Impact Caution (ITI)

“Terrain Ahead;Terrain

Ahead”

“Caution, Terrain; Caution,

Terrain”

Reduced Required

Obstacle Clearance

Caution (ROC)

“Caution, Obstacle; Cau-

tion, Obstacle”

“Obstacle Ahead; Obstacle

Ahead”

Imminent Obstacle

Impact Caution (IOI)

“Obstacle Ahead; Obstacle

Ahead”

“Caution, Obstacle; Cau-

tion, Obstacle”

Premature Descent

Alert Caution (PDA)

“Too Low, Terrain”

“Five-Hundred”

“Sink Rate”

Altitude Callout

“500”

None

Excessive Descent

Rate Caution (EDR)

Negative Climb

Rate Caution (NCR)

“Don’t Sink”

“Too Low, Terrain”

* Default conﬁguration

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

tAWs system status Annunciations

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

Alert Type

Aural Message

TAWS System Test Fail

None

“TAWS System Failure”

None

TAWS Alerting is disabled

No GPS position or

excessively degraded GPS

signal

“TAWS Not Available”

“TAWS Available” will be

heard when sufﬁcient GPS

signal is re-established.

System Test in progress

System Test pass

None

Chime

voiCe Alerts

voice Alert

description

“Minimums, minimums” The aircraft has descended below the preset barometric minimum

descent altitude.

“Vertical track”

The aircraft is one minute from Top of Descent. Issued only when

vertical navigation is enabled.

“Trafﬁc”

Played when a Trafﬁc Advisory (TA) is issued with the TIS system.

The aircraft is outside the Trafﬁc Information Service (TIS) coverage area.

Played when a Trafﬁc Advisory (TA) is issued with a TAS system.

Played when the TAS system passes a pilot-initiated self test.

Played when the TAS system fails a pilot-initiated self test.

“Trafﬁc Not Available”

“Trafﬁc, Trafﬁc”

“TAS System Test OK”

“TAS System Test

Failed”

190-00708-02 Rev. A

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Annunciations & Alerts

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

crosstalk error has occurred.

The MFD and PFDs are not communicating

with each other. The G1000 system should be

serviced.

PFD1 SERVICE – PFD1 needs

service. Return unit for repair.

PFD2 SERVICE – PFD2 needs

service. Return unit for repair.

The PFD and/or MFD self-test has detected a

problem. The G1000 system should be serviced.

MFD1 SERVICE – MFD1 needs

service. Return unit for repair.

MANIFEST – PFD1 software

mismatch, communication halted.

MANIFEST – PFD2 software

The PFD and/or MFD has incorrect software

mismatch, communication halted. installed. The G1000 system should be serviced.

MANIFEST – MFD1 software

mismatch, communication halted.

PFD1 CONFIG – PFD1 conﬁg error.

The PFD conﬁguration settings do not match

Conﬁg service req’d.

backup conﬁguration memory. The G1000

system should be serviced.

PFD2 CONFIG – PFD2 conﬁg error.

Conﬁg service req’d.

MFD1 CONFIG – MFD1 conﬁg

error. Conﬁg service req’d.

The MFD conﬁguration settings do not match

backup conﬁguration memory. The G1000

system should be serviced.

SW MISMATCH – GDU software

version mismatch. Xtalk is off.

The MFD and PFDs have different software

versions installed. The G1000 system should be

serviced.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

mFd & pFd messAge Advisories (Cont.)

Message

Comments

PFD1 COOLING – PFD1 has poor

cooling. Reducing power usage.

The PFD and/or MFD is overheating and is

PFD2 COOLING – PFD2 has poor reducing power consumption by dimming the

cooling. Reducing power usage.

display. If problem persists, the G1000 system

should be serviced.

MFD1 COOLING – MFD1 has poor

cooling. Reducing power usage.

PFD1 KEYSTK – PFD1 [key name]

Key is stuck.

A key is stuck on the PFD and/or MFD bezel.

PFD2 KEYSTK – PFD2 [key name] Attempt to free the stuck key by pressing it

Key is stuck.

several times. The G1000 system should be

serviced if the problem persists.

MFD1 KEYSTK – MFD [key name]

Key is stuck.

CNFG MODULE – PFD1

conﬁguration module is

inoperative.

The PFD1 conﬁguration module backup memory

has failed. The G1000 system should be

serviced.

PFD1 VOLTAGE – PFD1 has low

voltage. Reducing power usage

The PFD1 voltage is low. The G1000 system

should be serviced.

PFD2 VOLTAGE – PFD2 has low

voltage. Reducing power usage

The PFD2 voltage is low. The G1000 system

should be serviced.

MFD1 VOLTAGE – MFD1 has low

voltage. Reducing power usage

The MFD voltage is low. The G1000 system

should be serviced.

dAtAbAse messAge Advisories

Message

Comments

MFD1 DB ERR – MFD1 aviation

database error exists.

The MFD and/or PFD detected a failure in

the aviation database. Attempt to reload the

aviation database. If problem persists, the

G1000 system should be serviced.

PFD1 DB ERR – PFD1 aviation

database error exists.

PFD2 DB ERR – PFD2 aviation

database error exists.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

dAtAbAse messAge Advisories (Cont.)

Message

Comments

MFD1 DB ERR – MFD1 basemap

database error exists.

PFD1 DB ERR – PFD1 basemap

database error exists.

The MFD and/or PFD detected a failure in the

basemap database.

PFD2 DB ERR – PFD2 basemap

database error exists.

MFD1 DB ERR – MFD1 terrain

database error exists.

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 G1000 system should be

serviced.

PFD1 DB ERR – PFD1 terrain

database error exists.

PFD2 DB ERR – PFD2 terrain

database error exists.

MFD1 DB ERR – MFD1 terrain

database missing.

PFD1 DB ERR – PFD1 terrain

database missing.

The terrain database is present on another LRU,

but is missing on the speciﬁed LRU.

PFD2 DB ERR – PFD2 terrain

database missing.

MFD1 DB ERR – MFD1 obstacle

database error exists.

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 G1000 system should be serviced.

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.

The obstacle database is present on another LRU,

but is missing on the speciﬁed LRU.

PFD2 DB ERR – PFD2 obstacle

database missing.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

dAtAbAse messAge Advisories (Cont.)

Message

Comments

MFD1 DB ERR – MFD1 airport

terrain database error exists.

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 G1000 system should be

serviced.

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

The airport terrain database is present on

terrain database missing.

another LRU, but is missing on the speciﬁed LRU.

PFD2 DB ERR – PFD2 airport

terrain database missing.

MFD1 DB ERR – MFD1 Safe Taxi

database error exists.

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 G1000 system should be serviced.

PFD1 DB ERR – PFD1 Safe Taxi

database error exists.

PFD2 DB ERR – PFD2 Safe Taxi

database error exists.

MFD1 DB ERR – MFD1 Chartview The MFD detected a failure in the ChartView

database error exists.

database (optional feature). Ensure that the

data card is properly inserted. Replace data card.

If problem persists, The G1000 system should be

serviced.

MFD1 DB ERR – MFD1 FliteCharts The MFD detected a failure in the FliteCharts

database error exists.

database (optional feature). Ensure that the

data card is properly inserted. Replace data card.

If problem persists, The G1000 system should be

serviced.

DB MISMATCH – Aviation

The PFDs and MFD have different aviation

database version mismatch. Xtalk database versions installed. Crossﬁll is off.

is off.

Install correct aviation database version in all

displays.

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Annunciations & Alerts

dAtAbAse messAge Advisories (Cont.)

Message

Comments

DB MISMATCH – Aviation

The PFDs and MFD have different aviation

database type mismatch. Xtalk is database types installed (Americas, European,

off.

etc.). Crossﬁll is off. Install correct aviation

database type in all displays.

DB MISMATCH – Terrain database The PFDs and MFD have different terrain

version mismatch.

database versions installed. Install correct terrain

database version in all displays.

DB MISMATCH – Terrain database The PFDs and MFD have different terrain

type mismatch.

database types installed. Install correct terrain

database type in all displays.

DB MISMATCH – Obstacle

database version mismatch.

The PFDs and MFD have different obstacle

database versions installed. Install correct

obstacle database version in all displays.

DB MISMATCH – Airport Terrain

database mismatch.

The PFDs and MFD have different airport terrrain

databases installed. Install correct airport terrain

database in all displays.

gmA 1347d messAge Advisories

Message

Comments

GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.

The audio panel is unavailable. The G1000

system should be serviced.

GMA2 FAIL – GMA2 is inoperative.

GMA XTALK – GMA crosstalk error An error has occurred in transferring data

has occurred.

between the two GMAs. The G1000 system

should be serviced.

GMA1 CONFIG – GMA1 conﬁg

error. Conﬁg service req’d.

The audio panel conﬁguration settings do not

match backup conﬁguration memory. The

G1000 system should be serviced.

GMA2 CONFIG – GMA2 conﬁg

error. Conﬁg service req’d.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

gmA 1347d messAge Advisories (Cont.)

Message

Comments

MANIFEST – GMA1 software

mismatch, communication halted.

The audio panel has incorrect software installed. The

G1000 system should be serviced.

MANIFEST – GMA2 software

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

The audio panel self-test has detected a problem in

the unit. Certain audio functions may still be avail-

able, and the audio panel may still be usable. The

G1000 system should be serviced when possible.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

giA 63W messAge Advisories

Message

Comments

GIA1 CONFIG – GIA1 conﬁg error.

Conﬁg service req’d.

The GIA1 and/or GIA2 conﬁguration settings do

not match backup conﬁguration memory. The

G1000 system should be serviced.

GIA2 CONFIG – GIA2 conﬁg error.

Conﬁg service req’d.

GIA1 CONFIG – GIA1 audio conﬁg

error. Conﬁg service req’d.

The GIA1 and/or GIA2 have an error in the audio

conﬁguration. The G1000 system should be

serviced.

GIA2 CONFIG – GIA2 audio conﬁg

error. Conﬁg service req’d.

GIA1 COOLING – GIA1

temperature too low.

The GIA1 and/or GIA2 temperature is too low

to operate correctly. Allow units to warm up to

operating temperature.

GIA2 COOLING – GIA2

temperature too low.

GIA1 COOLING – GIA1 over

temperature.

The GIA1 and/or GIA2 temperature is too high.

If problem persists, the G1000 system should be

serviced.

GIA2 COOLING – GIA2 over

temperature.

GIA1 SERVICE – GIA1 needs

service. Return the unit for repair.

The GIA1 and/or GIA2 self-test has detected a

problem in the unit. The G1000 system should

be serviced.

GIA2 SERVICE – GIA2 needs

service. Return the unit for repair.

190-00708-02 Rev. A

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Annunciations & Alerts

giA 63W messAge Advisories (Cont.)

Message

Comments

HW MISMATCH – GIA hardware

mismatch. GIA1 communication

halted.

A GIA mismatch has been detected, where only

one is WAAS capable.

HW MISMATCH – GIA hardware

mismatch. GIA2 communication

halted.

MANIFEST – GIA1 software

mismatch, communication halted.

The GIA1 and/or GIA 2 has incorrect software

installed. The G1000 system should be serviced.

MANIFEST – GIA2 software

mismatch, communication halted.

MANIFEST – GFC software

mismatch, communication halted.

Incorrect servo software is installed, or gain

settings are incorrect.

COM1 TEMP – COM1 over temp.

Reducing transmitter power.

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 G1000 system should be

serviced.

COM2 TEMP – COM2 over temp.

Reducing transmitter power.

COM1 SERVICE – COM1 needs

service. Return unit for repair.

The system has detected a failure in COM1

and/or COM2. COM1 and/or COM2 may still be

usable. The G1000 system should be serviced

when possible.

COM2 SERVICE – COM2 needs

service. Return unit for repair.

COM1 PTT – COM1 push-to-talk

key is stuck.

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 G1000 system should

be serviced.

COM2 PTT – COM2 push-to-talk

key is stuck.

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 the

transfer switch again to cycle its operation. If

the problem persists, the G1000 system should

be serviced.

COM2 RMT XFR – COM2 remote

transfer key is stuck.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

giA 63W messAge Advisories (Cont.)

Message Comments

LOI – GPS integrity lost. Crosscheck GPS integrity is insufﬁcient for the current phase

with other NAVS.

of ﬂight.

GPS NAV LOST – Loss of GPS

navigation. Insufﬁcient satellites.

Loss of GPS navigation due to insufﬁcient

satellites.

GPS NAV LOST – Loss of GPS

navigation. Position error.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

GPS NAV LOST – Loss of GPS

navigation. GPS fail.

ABORT APR – Loss of GPS

navigation. Abort approach.

APR DWNGRADE – Approach

downgraded.

Vertical guidance generated by WAAS is

unavailable, use LNAV only minimums.

TRUE APR – True north approach.

Change HDG reference to TRUE.

Displayed after passing the ﬁrst waypoint of a

true north approach when the nav angle is set

to ‘AUTO’.

GPS1 SERVICE – GPS1 needs

service. Return unit for repair.

A failure has been detected in the GPS1

and/or GPS2 receiver. The receiver may still be

available. The G1000 system should be serviced.

GPS2 SERVICE – GPS2 needs

service. Return unit for repair.

NAV1 SERVICE – NAV1 needs

service. Return unit for repair.

A failure has been detected in the NAV1

and/or NAV2 receiver. The receiver may still be

available. The G1000 system should be serviced.

NAV2 SERVICE – NAV2 needs

service. Return unit for repair.

NAV1 RMT XFR – NAV1 remote

transfer key is stuck.

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 G1000

system should be serviced.

NAV2 RMT XFR – NAV2 remote

transfer key is stuck.

G/S1 FAIL – G/S1 is inoperative.

G/S2 FAIL – G/S2 is inoperative.

A failure has been detected in glideslope

receiver 1 and/or receiver 2. The G1000 system

should be serviced.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

giA 63W messAge Advisories (Cont.)

Message

Comments

G/S1 SERVICE – G/S1 needs

service. Return unit for repair.

A failure has been detected in glideslope

receiver 1 and/or receiver 2. The receiver may

still be available. The G1000 system should be

serviced when possible.

G/S2 SERVICE – G/S2 needs

service. Return unit for repair.

geA 71 messAge Advisories

Message

Comments

GEA1 CONFIG – GEA1 conﬁg error. The GEA1 conﬁguration settings do not match

Conﬁg service req’d.

those of backup conﬁguration memory. The

G1000 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

G1000 system should be serviced.

MANIFEST – GEA1 software

mismatch, communication halted.

The #1 GEA 71 has incorrect software installed.

The G1000 system should be serviced.

MANIFEST – GEA2 software

mismatch, communication halted.

The #2 GEA 71 has incorrect software installed.

The G1000 system should be serviced.

gtx 33/33d messAge Advisories

Message

Comments

XPDR1 CONFIG – XPDR1 conﬁg

error. Conﬁg service req’d.

The transponder conﬁguration settings do not

match those of backup conﬁguration memory.

The G1000 system should be serviced.

XPDR2 CONFIG – XPDR2 conﬁg

error. Conﬁg service req’d.

The transponder conﬁguration settings do not

match those of backup conﬁguration memory.

The G1000 system should be serviced.

MANIFEST – GTX1 software

mismatch, communication halted.

The transponder has incorrect software installed.

The G1000 system should be serviced.

MANIFEST – GTX2 software

mismatch, communication halted.

The transponder has incorrect software installed.

The G1000 system should be serviced.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

gtx 33/33d messAge Advisories (Cont.)

Message

Comments

XPDR1 SRVC – XPDR1 needs

service. Return unit for repair.

The #1 transponder should be serviced when

possible.

XPDR2 SRVC – XPDR2 needs

service. Return unit for repair.

The #2 transponder should be serviced when

possible.

XPDR1 FAIL – XPDR1 is

inoperative.

There is no communication with the #1

transponder.

XPDR2 FAIL – XPDR2 is

inoperative.

There is no communication with the #2

transponder.

grs 77 messAge Advisories

Message

Comments

AHRS1 TAS – AHRS1 not receiving The #1 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 G1000 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 G1000 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 G1000 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 G1000 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

G1000 system should be serviced.

AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving any or any useful

any GPS information.

GPS information. Check AFMS limitations. The

G1000 system should be serviced.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

Download from Www.Somanuals.com. All Manuals Search And Download.

Annunciations & Alerts

grs 77 messAge Advisories (Cont.)

Message

Comments

AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS

backup GPS information.

information. The G1000 system should be

serviced.

AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving backup GPS

backup GPS information.

information. The G1000 system should be

serviced.

AHRS1 GPS – AHRS1 operating

exclusively in no-GPS mode.

The #1 AHRS is operating exclusively in no-GPS

mode. The G1000 system should be serviced.

AHRS2 GPS – AHRS2 operating

exclusively in no-GPS mode.

The #2 AHRS is operating exclusively in no-GPS

mode. The G1000 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

ﬁeld model needs update.

of date. Update magnetic ﬁeld model when

practical.

AHRS2 SRVC – AHRS2 Magnetic-

ﬁeld model needs update.

The #2 AHRS earth magnetic ﬁeld model is out

of 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

as invalid.

GEO LIMITS – AHRS2 too far

North/South, no magnetic compass.

MANIFEST – GRS1 software

mismatch, communication halted.

The #1 AHRS has incorrect software installed.

The G1000 system should be serviced.

MANIFEST – GRS2 software

mismatch, communication halted.

The #2 AHRS has incorrect software installed.

The G1000 system should be serviced.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

gmu 44 messAge Advisories

Message

Comments

HDG FAULT – AHRS1

magnetometer fault has occurred.

A fault has occurred in the #1 GMU 44.

Heading is ﬂagged as invalid. The AHRS uses

GPS for backup mode operation. The G1000

system should be serviced.

HDG FAULT – AHRS2

magnetometer fault has occurred.

A fault has occurred in the #2 GMU 44.

Heading is ﬂagged as invalid. The AHRS uses

GPS for backup mode operation. The G1000

system should be serviced.

MANIFEST – GMU1 software

mismatch, communication halted.

The GMU 44 has incorrect software installed.

The G1000 system should be serviced.

MANIFEST – GMU2 software

mismatch, communication halted.

gdl 69A messAge Advisories

Message

Comments

GDL69 CONFIG – GDL 69 conﬁg

error. Conﬁg service req’d.

GDL 69 conﬁguration settings do not match

those of backup conﬁguration memory. The

G1000 system should be serviced.

GDL69 FAIL – GDL 69 has failed.

A failure has been detected in the GDL 69.

The receiver is unavailable. The G1000 system

should be serviced

MANIFEST – GDL software

mismatch, communication halted.

The GDL 69 has incorrect software installed.

The G1000 system should be serviced.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

gWx 68 Alert messAges

Message

Comments

GWX CONFIG – GWX conﬁg error. GWX 68 conﬁguration settings do not match

Conﬁg service req’d.

those of the GDU conﬁguration. The G1000

system should be serviced.

GWX FAIL – GWX is inoperative.

The GDU is not recieving status packet from the

GWX 68 or the GWX 68 is reporting a fault.

The GWX 68 radar system should be serviced.

GWX SERVICE – GWX needs

service. Return unit for repair.

A failure has been detected in the GWX 68. The

GWX 68 may still be usable.

MANIFEST – GWX software

mismatch, communication halted.

The GWX 68 has incorrect software installed.

The G1000 system should be serviced.

WX ALERT – Possible severe

weather ahead.

Possible severe weather detected within +/- 10

degrees of the aircraft heading at a range of 80

to 320 nm.

gdC 74b messAge Advisories

Message

Comments

ADC1 ALT EC – ADC1 altitude error

correction is unavailable.

GDC1 or GDC2 is reporting that the altitude

error correction is unavailable.

ADC2 ALT EC – ADC2 altitude error

correction is unavailable.

ADC1 AS EC – ADC1 airspeed error

correction is unavailable.

GDC1 or GDC2 is reporting that the airspeed

error correction is unavailable.

ADC2 AS EC – ADC2 airspeed error

correction is unavailable.

MANIFEST – GDC1 software

mismatch, communication halted.

The GDC 74B has incorrect software installed.

The G1000 system should be serviced.

MANIFEST – GDC2 software

mismatch, communication halted.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

gCu 475 messAge Advisories

Message

Comments

GCU CNFG – GCU Conﬁg error.

Conﬁg service req’d.

GCU 475 conﬁguration settings do not match

those of backup conﬁguration memory. The

G1000 system should be serviced.

GCU FAIL – GCU is inoperative.

A failure has been detected in the GCU 475.

The GCU 475 is unavailable.

MANIFEST – GCU software

mismatch, communication halted.

The GCU 475 has incorrect software installed.

The G1000 system should be serviced.

GCU KEYSTK – GCU [key name]

Key is stuck.

A key is stuck on the GCU 475 bezel. Attempt

to free the stuck key by pressing it several times.

The G1000 system should be serviced if the

problem persists.

gmC 710 messAge Advisories

Message

Comments

GMC CONFIG – GMC Conﬁg error.

Conﬁg service req’d.

Error in the conﬁguration of the GMC 710.

GMC FAIL – GMC is inoperative.

A failure has been detected in the GMC 710.

The GMC 710 is unavailable.

MANIFEST – GMC software

mismatch. Communication halted.

The GMC 710 has incorrect software installed.

The G1000 system should be serviced.

GMC KEYSTK – GMC [key name]

Key is stuck.

A key is stuck on the GMC 710 bezel. Attempt

to free the stuck key by pressing it several

times. The G1000 system should be serviced if

the problem persists.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Annunciations & Alerts

misCellAneous messAge Advisories

Message

Comments

FPL WPT LOCK – Flight plan

waypoint is locked.

Upon power-up, the G1000 system detects

that a stored ﬂight plan waypoint is locked.

This occurs when an aviation 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,

update the waypoint name/identiﬁer to reﬂect

the new information.

FPL WPT MOVE – Flight plan

waypoint moved.

The system has detected that a waypoint

coordinate has changed due to a new aviation

database update. Verify that stored ﬂight plans

contain correct waypoint locations.

TIMER EXPIRD – Timer has expired. The system notiﬁes the pilot that the timer has

expired.

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 aviation

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 aviation database. This alert is issued only

after an aviation database update. Verify use

of airways in stored ﬂight plans and reload

airways as needed.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

misCellAneous messAge Advisories (Cont.)

Message

Comments

FPL TRUNC – Flight plan has been

truncated.

This occurs when a newly installed aviation

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.

LOCKED FPL – Cannot navigate

locked ﬂight plan.

This occurs when the pilot attempts to activate

a stored ﬂight plan that contains locked

waypoint. Remove locked waypoint from ﬂight

plan. Update ﬂight plan with current waypoint.

WPT ARRIVAL – Arriving at

waypoint -[xxxx]

Arriving at waypoint [xxxx], where [xxxx] is the

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

less than 10 minutes.

Special use airspace is ahead of aircraft. The

aircraft will penetrate the airspace within 10

minutes.

ARSPC NEAR – Airspace near and

ahead.

Special use airspace is near and ahead of the

aircraft position.

ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the

than 2 nm.

aircraft position.

APR INACTV – Approach is not

active.

The system notiﬁes the pilot that the loaded

approach is not active. Activate approach when

required.

SLCT FREQ – Select appropriate

frequency for approach.

The system notiﬁes the pilot to load the

approach frequency for the appropriate NAV

receiver. Select the correct frequency for the

approach.

SLCT NAV – Select NAV on CDI for The system notiﬁes the pilot to set the CDI to

approach.

the correct NAV receiver. Set the CDI to the

correct NAV receiver.

190-00708-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

Download from Www.Somanuals.com. All Manuals Search And Download.

Annunciations & Alerts

misCellAneous messAge Advisories (Cont.)

Message

Comments

PTK FAIL – Parallel track unavailable:

bad geometry.

Bad parallel track geometry.

PTK FAIL – Parallel track unavailable:

invalid leg type.

Invalid leg type for parallel offset.

PTK FAIL – Parallel track unavailable: IAF waypoint for parallel offset has been

past IAF.

passed.

UNABLE V WPT – Can’t reach

current vertical waypoint.

The current vertical waypoint can not be

reached within the maximum ﬂight path angle

and vertical speed constraints. The system

automatically transitions to the next vertical

waypoint.

VNV – Unavailable. Unsupported

leg type in ﬂight plan.

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.

VNV – Unavailable. Excessive track The current track angle error exceeds the limit,

angle error.

causing the vertical deviation to go invalid.

VNV – Unavailable. Excessive

crosstrack error.

The current crosstrack exceeds the limit,

causing vertical deviation to go invalid.

VNV – Unavailable. Parallel course

selected.

A parallel course has been selected, causing

the vertical deviation to go invalid.

NO WGS84 WPT – Non WGS 84

waypoint for navigation -[xxxx]

The selected waypoint [xxxx] does not use the

WGS 84 datum. Cross-check position with

alternate navigation sources.

TRAFFIC FAIL – Trafﬁc device has

failed.

The G1000 is no longer receiving data from

the trafﬁc system. The trafﬁc device should be

serviced.

FAILED PATH – A data path has

failed.

A data path connected to the GDU or the GIA

63/W has failed.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Annunciations & Alerts

misCellAneous messAge Advisories (Cont.)

Message Comments

MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine

variance. Verify all course angles.

the exact magnetic variance for geographic

locations near the magnetic poles. Displayed

magnetic course angles may differ from the

actual magnetic heading by more than 2°.

SVS – SVS DISABLED: Out of

available terrain region.

Synthetic Vision is disabled because the aircraft

is not within the boundaries of the installed

terrain database.

SVS – SVS DISABLED: Terrain DB

resolution too low.

Synthetic Vision is disabled because a terrain

database of sufﬁcient resolution (9 arc-second

or better) is not currently installed.

SCHEDULER [#] – <message>.

ECS – Service required.

Message criteria entered by the user.

The environmental control system has failed.

CRUISE I – Cruise I conditions met. Cruise I engine trend data log has been

captured.

CRUISE II – Cruise II conditions met. Cruise II engine trend data log has been

captured.

EXCEEDANCE – Engine exceedance

An engine exceedance log has been captured.

data is being logged.

190-00708-02 Rev. A

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Annunciations & Alerts

Flight plAn import/export messAges

In some circumstances, some messages may appear in conjunction with others.

Flight Plan Import/Export

Results

Description

‘Flight plan successfully imported.’

A ﬂight plan ﬁle stored on the SD card was successfully

imported as a stored ﬂight plan.

‘File contained user waypoints only.

User waypoints imported success-

fully. No stored ﬂight plan data was

modiﬁed.’

The ﬁle stored on the SD card did not contain a ﬂight plan,

only user waypoints. These waypoints have been saved to the

system user waypoints. No ﬂight plans stored in the system

have been modiﬁed.

‘No ﬂight plan ﬁles found to import.’

‘Flight plan import failed.’

The SD card contains no ﬂight plan data.

Flight plan data was not successfully imported from the SD card.

‘Flight plan partially imported.’

Some ﬂight plan waypoints were successfully imported from

the SD card, however others had errors and were not imported.

A partial stored ﬂight plan now exists in the system.

‘File contained user waypoints only.’

The ﬁle stored on the SD card did not contain a ﬂight plan,

only user waypoints. One or more of these waypoints did not

import successfully.

‘Too many points. Flight plan trun-

cated.’

The ﬂight plan on the SD card contains more waypoints than

the system can support. The ﬂight plan was imported with as

many waypoints as possible.

‘Some waypoints not loaded. Way-

points locked.’

The ﬂight plan on the SD card contains one or more waypoints

that the system cannot ﬁnd in the navigation database. The

ﬂight plan has been imported, but must be edited within the

system before it can be activated for use.

‘User waypoint database full. Not all

loaded.’

The ﬂight plan ﬁle on the SD card contains user waypoints.

The quantity of stored user waypoints has exceeded system

capacity, therefore not all the user waypoints on the SD card

have been imported. Any ﬂight plan user waypoints that were

not imported are locked in the ﬂight plan. The ﬂight plan must

be edited within the system before it can be activated for use.

‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when

imported due to naming conﬂicts with waypoints already

existing in the system.

‘Flight plan successfully exported.’

‘Flight plan export failed.’

The stored ﬂight plan was successfully exported to the SD card.

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.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Appendix

pFd soFtkeY mAp

Top Level PFD Softkeys

TRFC-1

TRFC-2

Select the BACK or OFF Softkey

to return to the top-level softkeys.

Inset Map Softkeys

Level 3 Description

Level 1

INSET

Level 2

Displays Inset Map in PFD lower left corner

Removes Inset Map

OFF

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

190-00708-02 Rev. A

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Appendix

Level 1

Level 2

Level 3

Description

TRAFFIC

cycles through trafﬁc display options:

TRFc-1: Trafﬁc displayed on inset map

TRFc-2: Trafﬁc Map Page is displayed in

the inset map window

TOPO

Displays topographical data (e.g.,

coastlines, terrain, rivers, lakes) and

elevation scale on Inset Map

TERRAIN

NEXRAD

Displays terrain information on Inset Map

Displays NEXRAD weather and coverage

information on Inset Map (optional feature)

XM LTNG

Displays XM lightning information on Inset

Map (optional feature)

ADC2

AHRS1

AHRS2

BACK

MSG

ADC1

Select the BACK Softkey to

return to the top level softkeys.

Sensor Softkeys

Level 1

Level 2

Level 3

Description

SENSOR

Displays softkeys for selecting the #1 and

#2 AHRS and Air Data Computers

ADC1

ADC2

AHRS1

AHRS2

Selects the #1 Air Data Computer

Selects the #2 Air Data Computer

Selects the #1 AHRS

Selects the #2 AHRS

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Appendix

ADF/DME

SYN VIS

HSI FMT

ALT UNIT

Select the BACK Softkey

to return to the top-level softkeys

360 HSI ARC HSI

BACK

METERS

HPA

PATHWAY SYN TERR

HRZN HDG APTSIGNS

PFD Conﬁguration Softkeys

Level 1

PFD

Level 2

Level 3

Description

Displays second-level softkeys for

additional PFD conﬁgurations

SYN VIS

Displays the softkeys for enabling or

disabling Synthetic Vision features

PATHWAY Displays rectangular boxes representing

the horizontal and vertical ﬂight path of

the active ﬂight plan

SYN TERR Enables synthetic terrain depiction

HRZN HDG Displays compass heading along the

Zero-Pitch line

APTSIGNS Displays position markers for airports

within approximately 15 nm of the

current aircraft position. Airport

identiﬁers are displayed when the

airport is within approximately 9 nm.

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Appendix

Level 1

Level 2

DFLTS

Level 3

Description

Resets PFD to default settings, including

changing units to standard

WIND

Displays softkeys to select wind data

parameters

OPTN 1

Wind direction arrows with headwind

and crosswind components

OPTN 2

OPTN 3

Wind direction arrow and speed

Wind direction arrow with direction

and speed

OFF

Information not displayed

DME

Select to display the DME information

window

BRG1

Cycles the Bearing 1 Information

Window through NAV1 or GPS/

waypoint identiﬁer and GPS-derived

distance information.

HSI FRMT

BRG2

Displays the HSI formatting softkeys

Displays the HSI in a 360 degree format

Displays the HSI in an arc format

360 HSI

ARC HSI

Cycles the Bearing 2 Information

Window through NAV2 or GPS/

waypoint identiﬁer and GPS-derived

distance information.

ALT UNIT

Displays softkeys for setting the altimeter

and BARO settings to metric units

METERS

When enabled, displays altimeter in

meters

Select to display the BARO setting as

inches of mercury

HPA

Select to display the BARO setting as

hectopacals

STD BARO

Sets altimeter setting to standard

barometric pressure

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

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Appendix

MSG

Select the BACK Softkey to return

to the top-level softkeys.

MSG

Select the BACK Softkey to return

to the top-level softkeys.

Transponder Softkeys

Level 1

ADF/DME

XPDR

Level 2 Level 3

Description

Displays the ADF/DME Tuning Window

Displays transponder mode selection

softkeys

STBY

Selects Standby Mode (transponder does

not reply to any interrogations)

Selects Mode A (transponder replies to

interrogations)

ALT

Selects Mode C – Altitude Reporting Mode

(transponder replies to identiﬁcation and

altitude interrogations)

GND

Manually selects Ground Mode, the

transponder does not allow Mode A

and Mode C replies, but it does permit

acquisition squitter and replies to discretely

addressed Mode S interrogations.

VFR

Automatically enters the VFR code (1200 in

the U.S.A. only)

CODE

Displays transponder code selection

softkeys 0-7

0 — 7 Use numbers to enter code

Removes numbers entered, one at a time

BKSP

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Appendix

Level 1

IDENT

Level 2 Level 3

Description

Activates the Special Position Identiﬁcation

(SPI) pulse for 18 seconds, identifying the

transponder return on the ATC screen

TMR/REF

NRST

Displays Timer/References Window

Displays Nearest Airports Window

Displays Message Window

MSG

mFd soFtkeY mAp

(optional) (optional)

DCLTR

SHW CHRT

CAS ↑

MAP

CAS ↓

CHKLIST

DCLTR-1

DCLTR-2

DCLTR-3

Select the BACK Softkey on this level to

return to the top softkey level.

(optional) (optional)

XM LTNG

TRAFFIC

TOPO

TERRAIN

AIRWAYS

BACK

NEXRAD

AIRWY ON

AIRWY LO

AIRWAY HI

MFD Softkeys

Description

Level 1

Level 2

CAS ↑

CAS ↓

MAP

Scroll up (Displayed only when a sufﬁcient

number of items are displayed in the Crew

Alerting System Display to warrant scrolling)

Scroll down (Displayed only when a sufﬁcient

number of items are displayed in the Crew Alert-

ing System Display to warrant scrolling)

Enables second-level Navigation Map softkeys

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Appendix

Level 1

Level 2

Description

TRAFFIC Displays trafﬁc information on Navigation Map

TOPO

Displays topographical data (e.g., coastlines,

terrain, rivers, lakes) and elevation scale on

Navigation Map

TERRAIN Displays terrain information on Navigation Map

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

NEXRAD Displays NEXRAD weather and coverage

information on Navigation Map (optional feature)

XM LTNG Displays XM lightning information on Navigation

Map (optional feature)

BACK

Returns to top-level softkeys

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

SHW CHRT

CHKLIST

When available, displays optional airport and

terminal procedure charts

When available, displays optional checklists

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Appendix

Blank Page

100

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index

ChartView 56, 57

Code selection softkeys 12

COM 12, 61

Activate a ﬂight plan 20

Active Channel 59

ADF 11, 12, 62

AHRS 83, 84, 85, 87

Airport Signs 55, 56

Airways 99

Air Data Computer 68

Alert messages 86

ALT 46

Altimeter setting 1, 62

Altitude mode 46

Altitude volume 46

Antenna stabilization 53

Antenna tilt 51

DCLTR Softkey 56

Dead Reckoning 63

Declutter 62, 93, 99

Designated altitudes 22

Differential cabin pressure 5

Warning 65

Direct-to 19

DME 11, 12

Door status 9

DR mode 63, 64

Attitude & Heading Reference System

Audio panel controls

NAV1, NAV2 12

Edit a ﬂight plan 34

Enable Terrain 48

Engine display 5

Essential bus voltage 5

Barometric Altitude Minimums 3

Battery

Alerts 66

Flap position 5

Asymmetrical deﬂection warning 65

Flight Director 15

Flight ID 11

Flight path marker 55

FliteCharts® 56, 57

Frequency Transfer 12

Fuel

Alerts 65–66

Flow 5

Pressure 5

Quantity 5

Current 5

Overheat warning 65

Voltage 5

Bearing line 51, 52, 53

Cabin pressure altitude 5

Warning 65

CDI 1, 2, 12, 89

Cell 41, 42

Cell mode 42

Channel Presets 60

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Index-1

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index

Gain 52

Generator

Current 5

Speed 5

NACO 57

NAV 12

NAV1 2, 12

NAV2 2, 12

Navigation database 21, 22

NEXRAD 43, 44, 94, 99

Horizontal scan 52

Horizon heading 55

OBS 2

Obstacles 78, 80

Oil, engine

Alerts 65

Pressure 5

Temperature 5

Overspeed Protection 16

Oxygen

Pressure 5

Warning 65

Inhibit 48, 50

Inhibit TAWS 50

Inhibit Terrain 48

Inset Map 93, 94

Interturbine Temperature (ITT) 5

Warning 65

IOI 70, 72

Jeppesen 57

Pathways 55, 56

PIT 68

Propeller speed 5

Lightning 41, 42

Reversionary Mode

EICAS 5

Reversionary mode 61

ROC 70, 71, 72

Map panning 43

Message advisories 74–79, 81–85,

87–91

METAR 43

Minimums 73

MISCOMP 68

SafeTaxi® 56

Sector scan 53

Sensor 68

STAB 53

Standby 51

Mode S 97

Mode selection softkeys 12

Multi Function Display (MFD)

Softkeys 98

Index-2

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index

Store Flight Plan 34

Stormscope lightning data 41, 42

Strike 41

Weather data link page 43

Weather radar 50

Wind data 96

Strike mode 42

SVS 55, 91

Synthetic Vision System 55

XM lightning 94, 99

XM weather 43

TA 73

TAF 43

TAS 45, 46, 73, 83

TAWS 49, 50, 71, 73

TAWS-B 49

Terrain 46, 47, 49, 78, 94, 99

Terrain-SVS 47, 48

Tilt line 51

Timer 2, 88

Topographical data 94, 99

Torque 5

Warning 65

Trafﬁc 41, 45, 99

Trafﬁc advisory 45

Trafﬁc Advisory 73

Trafﬁc map page 45, 46, 47

Transponder 11, 12, 97, 98

Trim 5

Vertical speed guidance 22

Vertical track 73

VNV 19, 62, 90

Vspeed 2

WAAS 80

WATCH® 53

Weather Attenuated Color Highlight 53

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Index-3

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index

Blank Page

Index-4

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-02 Rev. A

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Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

p: 913.397.8200 f: 913.397.8282

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

p: 503.391.3411 f: 503.364.2138

Garmin (Europe) Ltd

Liberty House, Bulls Copse Road

Hounsdown Business Park

Southampton, SO40 9RB, U.K.

p: 44/0870.8501241 f: 44/0870.8501251

Garmin Corporation

No. 68, Jangshu 2nd Road

Shijr, Taipei County, Taiwan

p: 886/2.2642.9199 f: 886/2.2642.9099

www.garmin.com

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