g1000 Handout

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Handout

Garmin G1000

Flight Training Division

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Compiled by Peter Schmidleitner

Garmin G1000

Garmin 1000

Diamond DA 42 Twin Star

Vers. 3.3

Peter Schmidleitner


DA 42 Garmin 1000

MFD

Audio Panel

PFD

Peter Schmidleitner


G1000 Features

10 TFT LCD Displaysfor the PFD and MFD(1024 x 768 pixels)

Solid State Attitude-Heading-Reference-System (AHRS)

Digital Air DataComputer

Digital Audio Panel

Dual 16 Watt VHFCommunication Radios

Dual GPS Receivers

Dual VOR, LOC, GS

Terrain Awareness

TIS Traffic Avoidance

Extensive 3rd partyinterface capability

Peter Schmidleitner


G1000 Specifications

VHF COM Radio - 118.00 MHz to 136.975 MHz with25kHz or 8.33kHz spacing with either 10w or 16woutput

Non-precision GPS approach capable

ILS Receiver for precision approaches (Localizer andGlideslope)

VOR Receiver (108.0 MHz to 117.975 MHz)

256 Color, TFT moving map display


Garmin G1000

System Architecture

Peter Schmidleitner


System Architecture

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Peter Schmidleitner


Heading Information

Attention !

Magnetometer output routed throughAHRS

Therefore

AHRS fail = HDG fail

Peter Schmidleitner


G1000/Autopilot Interface

Attention !

G1000 Altitude Preselect does not workwith the KAP140 Autopilot

Use KAP140 Altitude Preselect control

Peter Schmidleitner


GIA 63

Communications hub for the systemPrimary communications path for AHRS and Air DatainformationInterfaces with GDL69 (Sattelite Data Link), StormscopeTM,SkyWatchTM , etc.

Peter Schmidleitner


GDC 74 Air Data Computer

RangeAltitude -1,400 ft to 55,000 ftIAS up to 430 ktsOperate -55oC to +70oC

Inputs include pitot, static and OAT

Accuracy supports RVSM

Peter Schmidleitner


GRS 77 AHRS and GMU 44 Magnetometer

Rapid alignment during taxi

Typically aligns in less than 1 min.!

In-Air Dynamic Restarts

Bank angles up to 20 degrees!

RobustOperates well in absence of GPS,Air Data, or Magnetometer!Inherent redundancy / integrity

Peter Schmidleitner


GTX 33 Transponder

Meets European Level 2Mode S Criteria

Solid State - no warm-up time and long life

Auto ALT Mode withGPS input

Auto Ground Mode

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Peter Schmidleitner


GEA 71 Engine/Airframe Interface

Extensive input capabilities

Engine load, RPM

Oil temp/pressure

Fuel flow/temp/quantity

Electrical system data

Coolant temp/Gearbox temp

Communicates with both GIA 63sBrings in not only engine data, butairframe data as well (e.g. Canopy Closedannunciation's)

Peter Schmidleitner


GMA 1347 Digital Audio Panel

Digital audio is used for the GarminNAVs and COMs

Emergency analog operation thatbypasses the GMA 1347

Voice Synthesis / Call-outs -eliminates need for additionalhardware

Reversionary Mode button


Garmin G1000

PFD Elements

Peter Schmidleitner


PFDAltitudeAttitudeAirspeed

Vertical speed

DG+CDI=HSIOAT Transponder, Time

Skid and Slip

Turn Rate

Peter Schmidleitner


Inset Map

Auxiliary window:Backlighting controlAnnunciationsADF/DME tuningTimer/Reference speeds

Nearest AirportsDirect-ToFlight PlanProcedures

PFD

Peter Schmidleitner


Supplemental flight data suchas the Inset Map, Alerts and

Annunciation Windowdisappear from the PFD whenpitch is more than +30 andless than -20 or when a 65bank angle is reached.

PFD

Extreme attitudes

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Garmin G1000

Controls onPFD and MFD

Peter Schmidleitner


Image reproduced with the permission of Garmin. Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserve

PFD and MFD Controls

COM tuningNAV tuning Navigation status bar

Peter Schmidleitner


Image reproduced with the permission of Garmin. Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved.

CRS select

BARO select

ALT select

HDG select

Range select


Peter Schmidleitner


Image reproduced with the permission of Garmin. Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserve

Softkeys FMS knobs

PFD / MFD keys



Garmin G1000

MFD Elements

Peter Schmidleitner


MFD

EIS / Engine Indication System Multi Function Display

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Peter Schmidleitner


Defaultpage

Display whenpushing the

SYSTEM button

Engine Indication SystemDisplay whenpushing theFUEL button

Peter Schmidleitner


Display whenpushing theFUEL button

Engine Indication System

Defaultpage

Display whenpushing the

SYSTEM button

LOAD is not measured, butcalculated from

common rail fuel pressure,ECU commanded injection time,

manifold pressure andProp RPM

Upper part always the same

Peter Schmidleitner


Engine Indication System

SYSTEM FUELDefault

Fuel Flow is notmeasured, butcalculated from fuel pressure andECU commanded injection time

Peter Schmidleitner


Ice protection system

Peter Schmidleitner


MFDCOM frequenciesCOM frequencies

Page Group and Page NamePage Group and Page Name

Waypoint Status BarWaypoint Status BarNAV frequenciesNAV frequencies

Page Group IconPage Group Icon

Peter Schmidleitner


MFDMap Page Group

3. Weather Map3. Weather Map

1. Navigation Map1. Navigation Map 2. Traffic Map2. Traffic Map

4. Terrain Proximity4. Terrain Proximity

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Peter Schmidleitner


MFDWaypoint (WPT) Page Group

1. Airport Information1. Airport Information 2. Intersection Information2. Intersection Information 3. NDB Information3. NDB Information

4. VOR Information4. VOR Information 5. User WPT Information5. User WPT Information

Peter Schmidleitner


MFDAux Page Group

1. Trip Planning1. Trip Planning 2. Utility2. Utility 3. GPS Status3. GPS Status

4. System Setup4. System Setup 5. System Status5. System Status

Peter Schmidleitner


MFDNearest Page Group

NearestNearest

AirportsAirports

IntersectionsIntersections

NDBsNDBs

VORsVORs

User WaypointsUser Waypoints

ARTCC/FSS/WXARTCC/FSS/WX

AirspacesAirspaces

Peter Schmidleitner


MFD

1. Active Flight Plan1. Active Flight Plan 2. Flight Plan Catalog2. Flight Plan Catalog

Flight Plan Page Group

3. Vertical Navigation3. Vertical Navigation


Garmin G1000

COM Tuning

Peter Schmidleitner


NAV and COM Tuning

LH identical RH

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Peter Schmidleitner


NAV COM

NAV and COM Tuning

Peter Schmidleitner


MHz tuning

Active: inside Standby: outside

Active: green Standby cursor: boxed

COMvolume/squelch

COM

KHz tuning

COM flip-flop

Cursor toggleActive (green) is selectedon AUDIO panel

COM Tuning


Garmin G1000

Audio Panel

Peter Schmidleitner


Audio panel

COM Split Switch

Intercom Isolation

MIC selector; automatically selectscorresponding Audio to headphone

GMA 1347

Peter Schmidleitner


Audio panel

Marker

Audio selectors

Audio selectors

Peter Schmidleitner


Audio panel

Clearance recorder playback

Intercom volume andsquelch control

Last 2,5 minutes of communication

MAN Squelch key

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Garmin G1000

NAV TuningADF/DME Tuning

RMI

Peter Schmidleitner


NAV

Active: insideStandby: outside

Active: greenStandby cursor: boxed

NAV volumeident filter

MHz tuning

KHz tuning

NAV flip-flop

Cursor toggle Active (green) is on HSI,selected by CDI key

NAV Tuning

Peter Schmidleitner


ADF - DME Tuning

Press ADF/DME

This brings up theADF/DME tuning

window

Note!For the ADF the ENTER key

flip/flops standby and active !

Peter Schmidleitner


RMI Needles

Press PFD

Now BRG1 andBRG2 toggle the

arrows betweenGPS, NAV and ADF


Garmin G1000

CDI

Peter Schmidleitner


CDI Softkey

CDI softkey togglesbetween

GPS (magenta)

NAV1(single green)

NAV2 (double green)

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Peter Schmidleitner


CDI Softkey


GPS (magenta)

NAV1(single green)

NAV2 (double green)

Peter Schmidleitner


CDI Softkey


GPS (magenta)

NAV1(single green)

NAV2 (double green)

Peter Schmidleitner


GPS CDI Modes

The mode isindicated here

Peter Schmidleitner


GPS CDI Modes

Possible modes are:

AUTO SEQUENCING

OBSOmni Bearing Select

SUSPSuspend

Peter Schmidleitner


GPS CDI Modes

AUTO SEQUENCING

blank

not active (black)

Peter Schmidleitner


GPS CDI Modes

Omni Bearing Select

OBS

active (grey)

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Peter Schmidleitner


GPS CDI Modes

SUSPEND

SUSP

active (grey)

to deactivate SUSPEND


Garmin G1000

EmergencyProcedures

Peter Schmidleitner


Normal Mode Display

Emergency Procedures

Peter Schmidleitner



PFD Failure

Peter Schmidleitner



MFD Failure

Peter Schmidleitner



Reversionary Mode

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Peter Schmidleitner



Failure indicatedwith a red cross

Flashes as WARNING,CAUTION or ADVISORY

Displays abbreviatedannunciation text

Displays alert textmessages

AlertingSystem

Peter Schmidleitner



Air Data Computer Fail

Peter Schmidleitner



AHRS Fail

Peter Schmidleitner



Magnetometer Fail

Peter Schmidleitner


Automatic backup to analogmode of COM 1, no intercom

Audio panel

Use other NAV / COMNAV / COM

Refer to SBY ASI, AltimeterADC

Refer to SBY horizon, attemptAHRS reset

AHRS

ActionFailed System



Garmin G1000

Terrain Awareness

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Peter Schmidleitner


Terrain Awareness

For situational awareness only

No voice callout

Yellow = aircraft within 1000 AGL ofterrain

Red = aircraft below elevation of

terrain does not account for trees, power-

lines, etc.

Peter Schmidleitner


Terrain Awareness


Garmin G1000

Stormscope

Peter Schmidleitner


Stormscope WX 500

Peter Schmidleitner

Always operating

Overlay on Map, or dedicated page witheither 360 or 120 arc view modes

Strike or Cell mode selected by soft key

Range by use of Zoom/Pan joystick

Data clear by soft key

Strike aging New strike is bold for 6 seconds

Normal lightning bolt for 1 minute

+ 1 additional minute after strike

Smaller + for last minute

Stormscope WX 500

Peter Schmidleitner

Stormscope WX 500

Weather MapWeather Map

g1000 Handout

Documents

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