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Introduction

Who am I?

- Peter Wheeler, GA Examiner since January 04- Simuflight CTC Aviation Training

-  A mixture of NZ instructor training & testing and

JAA training & testing

Why am I here?

- Operating DA42 since Nov 06

-  An interest in seeing glass technology move to GA

-  Asked to brief you on G1000

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The Garmin 1000

Introduction to the G1000 for Flight Examiners

Normal, Abnormal, Emergency procedures

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What we will cover: (questions at any time)

The system

- Definitions & Abbreviations- Description & Operation of the system

Flight Tests & the G1000

-  Abnormal Ops & Emergencies

- Simulating failures

Review

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Def initions & Abbr eviations

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Components of Garmin 1000 (see handout)

Transponder Modes A, C, S

Engine / Airframe unitEngine, Fuel sensors

 ADCOAT, Pitot & Static instr.

Magnetometer 

 AHRS Attitude & Heading

Rate sensors, Slip/Skid

Optional modules� KAP140 auto pilot 

�  ADF 

� DME 

�Stormsco

 pe

GPS / Com / Nav 1Similar to Garmin 430

GPS / Com / Nav 2Similar to Garmin 430

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The Primary Flight Display

125.60113.35SAM 

Expanded pitch scale:

Can set attitudes ±1° (really!)

Slip bar:

� ¼ bar = ¼ ball imbalance

� Heavily damped ³lag´

SAM 113.35

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The Primary Flight Display

125.60113.35SAM 

 Air Data Computer:� IAS and TAS

� Digits distracting?

� Digits moving

means speed

SAM 113.35

 Air Data Computer:� ALT and VSI

� Digits distracting?

� Digits moving

means altitude

� Scan bug not digits

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The Primary Flight Display

125.60113.35

 ADC and AHRS trend vectors:� 6 seconds

� ASI, Alt, HSI (turn rate)

SAM 

SAM 113.35

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The Primary Flight Display

125.60113.35SAM 

SAM 

Tuning Nav/Coms:� Standby (outside), active (inside)

� Green means in-use

� VOR/LOC visual (not aural) ident.

�Freq toggle, changing boxes, tuning«

113.35

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The Primary Flight Display

125.60113.35SAM 

SAM 

Displaying navaids:

� HSI display: Nav 1, Nav 2, GPS

�CDI disappears if no signal� RMI: VOR 1, 2, GPS, ADF

113.35

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The Primary Flight Display

125.60113.35SAM 

SAM 

DME conventional

RMI distance is GPS-based

113.35

DME Nav 1

Nav 2

Hold

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The Primary Flight Display

125.60113.35SAM 

SAM 

Transponder Status Bar:

� Mode S

� Auto, Manual

� Codes, squawk etc

113.35

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The Primary Flight Display

125.60113.35SAM 

SAM 113.35

Softkeys:

� Context-sensitive:

look before you leap!

� Sub-menus & the ³Back´ button

� ³Alerts´ button always on the far 

right to acknowledge alerts

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The Primary Flight Display

125.60113.35SAM 

GPS:

� Waypoint Status Bar � Cannot disable but can cover«

� Next waypoint, distance to go,

desired (planned) track,

instantaneous track (°M)

SAM 113.35

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The Primary Flight Display

125.60113.35SAM 

SAM 113.35

Using the FMS knobs: tuning the ADF or DME� Bring up the ADF window;

� Use the outer & inner knobs to select fields and change digits;

� IMPORTANT: Press ENTER, not the FMS knob itself , to accept the

new value. Pressing the FMS knob simply cancels the change.

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The Multi-Function Display

113.35 120.750SAM 

IBMH 

Nav/Com displays: as per PFD

GPS:� Navigation Status bar:

� Operator can change

� Instantaneous GS, Cross-track error,

Distance and ETA for example.

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The Multi-Function Display

113.35 120.750SAM 

IBMH 

Useful features:

� Change map appearance / defaults using MENU

� Use MAP softkey to overlay information

�Topography, Terrain Awareness, Stormscope etc

� GPS flight plan will always be overlaid

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The Multi-Function Display

113.35 120.750SAM 

IBMH 

Changing map scale:

� Rotate RANGE knob

Press the range knob to generate a map panning arrow

� Range knob acts as a joystick to pan cursor on map

� More information displayed at top of screen

300° 9.8NM ± Elev 357FT ± N45°W001°

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The Audio Selector Panel

Similar functions to other Garmin audio panels

- ³COM1 MIC´ listen & talk- ³COM1´ just listen

 Audio identification of DME / ADF

Volumes

- Coms, Navaids (not DME) have own volume

- Intercom volume for pilot, one other for all pax

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Failur es affecting the G1000

GPS / Com / Nav 1Similar to Garmin 430

GPS / Com / Nav 2Similar to Garmin 430

Transponder Modes A, C, S

Engine / Airframe unitEngine, Fuel sensors

 ADCOAT, Pitot & Static instr.

Magnetometer 

 AHRS Attitude & Heading

Rate sensors, Slip/Skid

Optional modules� KAP140 auto pilot 

�  ADF 

� DME 

� Stormsco pe

NO D ATA

N  AV2 

V OR 1

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Reversionary Modes

GPS / Com / Nav 1Similar to Garmin 430

GPS / Com / Nav 2Similar to Garmin 430

 ADCOAT, Pitot & Static instr.

Magnetometer 

 AHRS Attitude & Heading

Rate sensors, Slip/Skid

Optional modules� KAP140 auto pilot 

�  ADF 

� DME 

� Stormsco pe

� Note: even though GPS / Com / Nav 2 work,

the data may not be accessible.

� You may also lose the use of  ADF, DME etc!

� Limited navigation available Nav 1, NRST

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Manual Reversionary Mode

GPS / Com / Nav 1Similar to Garmin 430

GPS / Com / Nav 2Similar to Garmin 430

 ADCOAT, Pitot & Static instr.

Magnetometer 

 AHRS Attitude & Heading

Rate sensors, Slip/Skid

Optional modules� KAP140 auto pilot 

�  ADF 

� DME 

� Stormsco pe

� Reversion should be automatic.

� If it does not occur, it can be done manually.

� If this is simulated (i.e. no real failure), all

navaids will remain useable.

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What we have cover ed:

The system

- Definitions & Abbreviations- Description & Operation of the system

Flight Tests & the G1000

-  Abnormal Ops & Emergencies

- Simulating failures

Review: Questions or comments?