Garmin Software Version 0321.22 Manual de usuario Pagina 25

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
WITH HONEYWELL KAP 140 AUTOPILOT
190-00492-12 Rev 6 Diamond DA 40 / DA 40F
3-3
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.
(g) High Fuel Flow –
(DA 40 F only)
1. Fuel Quantity .................................................................. Check and Monitor
2. Power Setting ...................................................................................... Check
Land as soon as practical. Consider the reduced range and endurance due to
possible loss of fuel.
NOTE
Have the airplane inspected before next flight.
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