Garmin Software Version 0321.22 Manual de usuario Pagina 27

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
WITH HONEYWELL KAP 140 AUTOPILOT
190-00492-12 Rev 6 Diamond DA 40 / DA 40F
3-5
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.
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