DA 40 NG AFM
Normal Operating
Procedures
4A.5.13 GO-AROUND |
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1. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . |
MAX |
2. |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
72 KIAS |
3. |
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
T/O |
Above a Safe Height:
4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 KIAS
5. Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 33 |
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Normal Operating |
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DA 40 NG AFM |
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Procedures |
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4A.5.14 AFTER LANDING |
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1. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . |
IDLE |
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2. |
Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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3. |
Transponder . . . . . . . . . . . . . . . . . . . . . . . . . |
OFF / STBY |
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4. |
Pitot heating . . . . . . . . . . . . . . . . . . . . . . . . . |
OFF |
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5. |
Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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6. |
Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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7. |
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
UP |
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8. |
Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . |
OFF |
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END OF CHECKLIST
Page 4A - 34 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
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Normal Operating |
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Procedures |
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4A.5.15 ENGINE SHUT-DOWN |
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1. |
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . |
set |
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2. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . |
up to 10 % load for 1 minute |
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% 3. |
Engine indications . . . . . . . . . . . . . . . . . . . . . |
check |
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4. |
ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
check not transmitting on |
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121.5 MHz |
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5. |
AVIONIC MASTER . . . . . . . . . . . . . . . . . . . . |
OFF |
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6. |
Electrical consumers . . . . . . . . . . . . . . . . . . . |
OFF |
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7. |
ENGINE MASTER . . . . . . . . . . . . . . . . . . . . . |
OFF |
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8. |
Strobe . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
OFF |
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CAUTION
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After turning the ENGINE MASTER OFF, wait until the engine |
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indications on the G1000 |
MFD (if installed) or MED (if |
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installed) disappear prior |
to switching the ELECTRIC |
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MASTER OFF. This ensures that engine and flight data can |
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be written to non-volatile memory before removing electrical |
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power. |
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9. ELECTRIC MASTER . . . . . . . . . . . . |
. . . . . . . OFF |
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CAUTION |
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Do not shut down an engine by placing the FUEL VALVE in the OFF position. The high pressure fuel pump can otherwise be damaged.
NOTE
Before shut-down the engine must run for at least 1 minute with the POWER lever set up to 10% load to avoid heat damage of the turbo charger.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 35 |
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Normal Operating
DA 40 NG AFM
Procedures
4A.5.16 POST FLIGHT INSPECTION
1.Record any problem found in flight and during the post-flight check in the log book.
2.Park the airplane.
3.If necessary, moor the airplane.
END OF CHECKLIST |
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4A.5.17 PARKING |
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1. |
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . |
release, use chocks |
2. |
Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
moor, if unsupervised for |
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extended period |
3. |
Pitot probe . . . . . . . . . . . . . . . . . . . . . . . . . . . |
cover |
END OF CHECKLIST
Page 4A - 36 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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