Garmin Software Version 0321.22 Manual de usuario descargar pdf (Pagina 31)

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

WITH GARMIN GFC 700 AUTOPILOT

DIAMOND MODEL DA 40

DIAMOND MODEL DA 40 F

190-00492-10 Rev 8 Diamond DA 40 / DA 40F

3-9

If smoke or fumes decrease:

9. Land at the nearest suitable airport as soon as possible

If smoke or fumes persist:

10. ALT (alternator) switch ................................................................................. ON

11. ESS BUS switch ........................................................................................... OFF

12. BATT and ESS TIE circuit breakers ......................................................... PULL

This removes power from the essential bus and restores power to the

main and avionics busses. See the table at the end of this section for

the equipment which will still be available.

13. Use standby instruments for attitude, airspeed and altitude

14. Refer to Section 3.7.2 (b) of this Supplement, Alternator Failure

15. Land at the nearest suitable airport as soon as possible

The equipment available on Essential Bus only (operating on battery only

and the Essential Bus switch selected) is:

Air Data Computer (airspeed, altitude, vertical speed, OAT, TAS)

Attitude and Heading Reference System (attitude, heading)

PFD (in composite mode)

Pitot Heat

Flaps

COM 1

GPS/NAV 1

Transponder

Landing light

Instrument flood lights

Engine instruments

Starter

Refer to the “Essential Bus” area of the circuit breaker panel for a quick

reference to equipment on the Essential Bus.

Equipment available on the Main and Avionics Busses only:

COM 2

GPS/NAV 2

MFD

Electric fuel pump

Instrument lights

Strobe lights

Position lights

Taxi light

Refer to the “Main Bus” and “Avionics Bus” areas of the circuit breaker panel

for a quick reference to equipment on those busses.

1 2 ... 26 27 28 29 30 31 32 33 34 35 36 ... 65 66

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Garmin Software Version 0321.22 Manual de usuario Pagina 31

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