FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-11 Rev 8 Diamond DA 40 / DA 40F
4A-12
18. RPM lever (DA 40 only) ................................. pull back until a drop of max.
500 RPM is reached – HIGH RPM;
Cycle 3 times
18a Carburetor Heat (DA 40 F only) .............................................. check function
18b Throttle (DA 40 F only) ............................ MAX PWR, minimum 2200 RPM
NOTE (DA 40 F only)
The result of the ground check at full throttle depends on a
number of environmental factors, e.g. temperature, ambient air
pressure and in particular head or tailwind components.
Headwind will cause a higher RPM than tailwind.
19. Throttle .................................................................................. set 1000 RPM
20. Carburetor Heat (DA 40 F only) ............................................. check COLD
21. Alternate Air (DA 40 only) ................................................ check CLOSED
22. Flight Plan .........................................................................................entered
23. Altimeter setting ......................................................................... checked/set
(G1000 and standby altimeter)
24. Altitude preselector .................................................................................. set
25. Radios ................................................................................. set and checked
26. Transponder .................................................................................... code set
27. Standby attitude gyro ......................................................... erect and no flag
28. Parking brake .................................................................................... release
29. Landing light ........................................................................ ON as required
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