Garmin Software Version 0321.19 Manual de usuario descargar pdf (Pagina 32)

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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FAILURE OF THE PREFLIGHT TEST (Red boxed PFT on PFD)

1. AFCS Circuit Breaker.........................................................................PULL

WARNING

DO NOT ATTEMPT TO ENGAGE THE AUTOPILOT OR OPERATE

THE MANUAL ELECTRIC TRIM UNTIL THE CAUSE OF THE

MALFUNCTION HAS BEEN CORRECTED.

NOTE

When the AFCS circuit breaker is pulled, the PFT FAIL annunciation will be

removed and the autopilot and manual electric trim will be unavailable. Do not

reset the circuit breaker unless the airplane is on the ground.

MAXIMUM ALTITUDE LOSS DUE TO AUTOPILOT, FLIGHT

DIRECTOR OR AHRS MALFUNCTIONS:

MANEUVER ALTITUDE LOSS

Climb, Cruise, Descent 200 feet

Maneuvering 115 feet

Approach 130 feet

3.2.3 ENGINE PROBLEMS IN FLIGHT

(h) High Fuel Flow

– (DA 40 only)

Fuel flow in red sector

1. Fuel pressure .................................check for red FUEL PRESS LO message

• If fuel pressure is low (FUEL PRESS LO message), there is possibly a

leak (between the injection system and the injectors). Land at the

nearest available airport.

• If there is no FUEL PRESS LO message, there is no leak; the likely

cause is a defective fuel flow indication, which should thus be ignored

(the airplane should be serviced). Fuel flow data should be taken from

the engine performance table in Chapter 5 of the AFM.

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Garmin Software Version 0321.19 Manual de usuario Pagina 32