Garmin Cessna Caravan G1000 Airplane Flight Manual Supplement - Page 18

Browse online or download pdf Airplane Flight Manual Supplement for Avionics Display Garmin Cessna Caravan G1000. Garmin Cessna Caravan G1000 33 pages. Integrated flight deck
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Garmin Cessna Caravan G1000 Airplane Flight Manual Supplement

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

5. Terminate flight as soon as practical.

6. On approach, the pilot may engage the "BAT" circuit breaker to rees-

tablish power to all systems if necessary.

7. If using battery power only and the primary battery has been de-

pleted (minimum of 18 VDC), the pilot may select the alternate bat-

tery using the main battery selection switch. There will be no change

in available equipment when changing battery sources. All equip-

ment powered previously will remain powered

AVIONICS EMERGENCIES

a) PFD OR MFD DISPLAY FAILURE

1. DISPLAY BACKUP button on audio panel

b) AHRS FAILURE

Failure of the Attitude and Heading Reference System (AHRS)

is indicated by a removal of the sky/ground presentation and

a red X and a yellow "AHRS FAILURE" shown on the PFD. The

digital heading presentation will be replaced with a yellow

"HDG" and the compass rose digits will be removed. The

course pointer will indicate straight up and course may be set

using the digital window.

1. Use Standby Attitude Indicator and Magnetic compass.

2. Course Set using digital window

3. Land as soon as practical.

c) AIR DATA COMPUTER (ADC) FAILURE

Complete loss of the Air Data Computer is indicated by a red X

and yellow text over the airspeed, altimeter, vertical speed,

TAS and OAT displays. Some FMS functions, such as true air-

speed and wind calculations, will also be lost.

1. Use Standby Airspeed Indicator and Altimeter

2. Land as soon as practical at a suitable airport

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FAA APPROVED

. . . . .

NOTE:

MOONEY

M20R

PUSH

ISSUED 11 - 2004

REVISION A 06--2005

REVISION B 03--2006