Garmin Software Version 0321.22 Manual de usuario Pagina 41

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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-9
BEFORE TAXIING
1. Avionics master switch .................................................................................. ON
2. Electrical equipment ..................................................................... On as required
3. Flaps ............................................................................... UP – T/O – LDG – T/O
(indicator and visual check)
4. Flight instruments and avionics ............................. set, test function, as required
(set both altimeters)
5. Flood light ............................................................. ON, test function, as required
6. Ammeter ........................................................... check, if required increase RPM
7. Fuel tank selector ............................................................................ change tanks
confirm that engine also runs on other tank (at least 1 minute at 1500 RPM)
8. Pitot heating .............................................................................. ON, test function
(no yellow PITOT FAIL annunciation)
9. Pitot heating .......................................................................... OFF if not required
(yellow PITOT OFF annunciation)
10. Strobe lights (ACLs) .................................... check ON test function, as required
11. Position lights, landing and taxi lights .................. ON, test function, as required
CAUTION
When taxiing at close range to other aircraft, or during night flight in
clouds, fog or haze, the strobe lights should be switched OFF. The position
lights must always be switched ON during night flight.
12. Idle RPM ........................................................................ check, 600 to 800 RPM
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