Garmin Cessna Caravan G1000, Дополнение к руководству

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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3.7.2 FAILURES IN THE ELECTRICAL SYSTEM
(b) Alternator failure
An alternator failure is indicated by a red ALTERNATOR message and an
ammeter indication of 0 Amps.
1. Circuit breakers...................................................................................... Check in
2. ALT (alternator) switch ................................................................ OFF, then ON
If alternator does not come back on line (message extinguishes and
ammeter indication greater than zero):
3. ESS BUS switch ............................................................................................ ON
4. Switch off any non-essential electrical loads.
5. Land within 30 minutes
If PFD attitude information is lost prior to landing:
6. HORIZON EMERGENCY Switch................................................................ ON
CAUTION
The following items are available on the Essential Bus:
•
PFD in composite (backup) format
•
NAV/COM 1
•
GPS 1
•
Attitude and Heading Reference System (AHRS)
•
Air Data Computer
•
Pitot heat
•
Engine instruments
•
Transponder
•
Flood light
•
Landing light
Refer to the ESSENTIAL BUS area of the circuit breaker panel for a quick
reference to equipment on those busses. These items of equipment can be
supplied with power by the battery for at least 30 minutes. During this 30-
minute period, the airplane must be landed at a suitable airport. Economical use
of electrical equipment, in particular of pitot heat, and switching off equipment
that is not needed extends the time during which the other equipment remains
available.