Garmin Cessna Caravan G1000 Aanvullend vlieghandboek - Pagina 16

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AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

7. In an in--flight emergency, depressing and holding the Comm trans-

fer button for 2 seconds will select the emergency frequency of

121.500 MHz, and will show it in the "Active" frequency window.

8. The Attitude, Heading and Reference System (AHRS) requires at

least one GPS or air data input to function properly. In the unlikely

event that both GPS position sources fail, and the air data computer

fails, the AHRS will subsequently lose attitude and heading and the

pilot will be required to use the standby instrumentation. In this

instance, the PFD will not provide altitude, airspeed, attitude, or nav-

igation information

3.1 - - EMERGENCY PROCEDURE CHECKLISTS

Use the electrical fire checklists found in the M20R POH and appropri-

ate AFM supplements.

Electrical System Failures

Alternator Failure

If the Main Alternator fails, indicated by the Master Warning "ALT

VOLTS" is flashing:

Perform the Standby Alternator Emergency Checklist (repeated below)

1. Push the "Stdby Alt/Emergency Bus" switch ON. (This activates the

emergency bus circuitry & Standby Alternator system) Verify:

(a) The AMBER "EMERG BUS" annunciator illuminates, and

(b) The RED "ALT VOLTS" flashing annunciator extinguishes.

The most efficient operating RPM is 2500 RPM when operat-

ing on the Standby Alternator System.

2. All electrical systems will remain powered and functional.

3. If the RED "ALT VOLTS" annunciator remains illuminated, then:

If the RED "ALT VOLTS" annunciation remains illuminated, then

the standby alternator has failed, and only main battery power re-

mains.

4. Reduce the electrical load by pulling the "BAT" circuit breaker. This

load sheds the non--essential bus. The following systems remain

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FAA APPROVED

NOTE:

-CAUTION-

MOONEY

M20R

ISSUED 11 - 2004

REVISION A 06--2005

REVISION B 03--2006