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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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.