FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-11 Rev 8 Diamond DA 40 / DA 40F
3-4
2. Master switch (ALT/BAT) ...................................................................... OFF
3. Cabin heat ................................................................................................ OFF
4. Emergency window(s) .......................................................................... OPEN
5. Use standby instruments for airspeed, altitude and attitude reference, if
necessary
6. Land at the nearest suitable airport as soon as possible
If electronic or avionics equipment is required for continued flight, the
following procedure may be used to isolate the source of the smoke or
fumes:
7. BAT (battery) switch ................................................................................ ON
8. ESS BUS switch ....................................................................................... ON
NOTE
This removes power from the main and avionics busses, but does not allow
alternator operation. See the table at the end of this section for the
equipment which is still available.
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
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