FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
WITH GARMIN GFC 700 AUTOPILOT
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 8 Diamond DA 40 / DA 40F
3-8
(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.
3.3.3 SMOKE AND FIRE IN FLIGHT
(b) Electrical fire with smoke in flight
1. Emergency switch ......................................................................... ON if installed
CAUTION
Switching OFF the master switch (ALT/BAT) will lead to total loss of all
electronic and electric equipment, including the AHRS and attitude display.
However, by switching the HORIZON EMERGENCY switch ON, the
emergency battery will supply power to the standby attitude gyro (artificial
horizon) and the flood light.
In case of extreme smoke development, the front canopy may be unlatched
during flight. This allows it to partially open, in order to improve ventilation.
The canopy will remain open in this position. Flight characteristics will not be
affected significantly.
2. Master switch (ALT/BAT) ........................................................................... OFF
3. Cabin heat ..................................................................................................... OFF
4. Emergency window(s) ............................................................................... OPEN
5. Use standby instruments for airspeed, altitude and attitude reference, if
necessary
6. Land at the nearest suitable airport as soon as possible
If electronic or avionics equipment is required for continued flight, the
following procedure may be used to isolate the source of the smoke or
fumes:
7. BAT (battery) switch ..................................................................................... ON
8. ESS BUS switch ............................................................................................ ON
NOTE
This removes power from the main and avionics busses, and does not allow
alternator operation. See the table at the end of this section for the equipment
which is still available.
(36 paginas)
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