Garmin Software Version 0321.22 Manual de usuario Pagina 35

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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
4A-3
CAUTION
When the essential bus is switched ON, the battery will not be charged
unless the essential tie relay bypass (OAM 40-126) is installed.
21. BAT (battery) switch .................................................................................... ON
22. Fuel tank selector .......................................................................... on fullest tank
WARNING
Never move the propeller by hand while the ignition is switched on, as it
may result in serious personal injury.
Never try to start the engine by hand.
STARTING ENGINE (DA 40 only)
(a)
Cold engine
1. Strobe light (ACL) ......................................................................................... ON
2. Electrical fuel pump ........................................................... ON, note pump noise
(=functional check of pump)
3. Throttle ........................................................... 3 cm (1.2 in) forward from IDLE
(measured from rear of slot)
4. Mixture control lever ........................................ RICH for 3 – 5 sec, then LEAN
5. Throttle 1 cm (0.4 in) forward from .......................................................... IDLE
(measured from rear of slot)
WARNING
Before starting the engine, the pilot must ensure that the propeller area is
free, and no persons can be endangered.
CAUTION
Do not overheat the starter motor. Do not operate the starter motor for more
than 10 seconds. After operating the starter motor, let it cool off for 20
seconds. After 6 attempts to start the engine, let the starter cool for 30
minutes before further start attempts.
CAUTION
The use of an external pre-heater and external power source is
recommended whenever possible, in particular at ambient temperatures
below 0°C (32°F), to reduce wear and abuse to the engine and electrical
system. Pre-heat will thaw the oil trapped in the oil cooler, which can be
congealed in extremely cold temperatures. After a warm-up period of
approximately 2 to 5 minutes (depending on the ambient temperature) at
1500 RPM, the engine is ready for takeoff if it accelerates smoothly and the
oil pressure is normal and steady.
6. Ignition Switch ........................................................................................ START
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