Garmin Software Version 0321.22 Manual de usuario Pagina 43
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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-11
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. G1000 and autopilot altitude preselectors ..................................................... 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
Missed Approach
(See KAP 140 flight manual supplement for additional information)
a. ... AP DISC Button ........................................... PRESS to disengage AP
b. ... MISSED APPROACH ....................................................... EXECUTE
c. ... AP Button – After airplane is in trim and climb established .... PRESS
(for autopilot operation if desired).
d. ... G1000 HDG bug ............................... Set to missed approach heading
e. ... Autopilot HDG button .............................................................. PRESS
f. .... G1000 Missed Approach ............................................... ACTIVATED
g. ... Autopilot NAV button .............................................................. PRESS
(After missed approach path has been verified)
NOTE
If engaged, the autopilot must be operated in HDG mode
until the pilot has verified that the autopilot programming
will result in the required climb and tracking of the missed
approach path. If tracking the ILS course outbound as part
- Table of Contents 5
- (DA 40 only) 25
- (DA 40 F only) 25
- CAUTION 26
- WARNING 35
- NOTE (DA 40 F only) 43
- 7.10 FUEL SYSTEM 54
- Part Information 55
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