Garmin Software Version 0321.19 Manual de usuario descargar pdf (Pagina 36)

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

Page 36 of 65

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.

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Garmin Software Version 0321.19 Manual de usuario Pagina 36