DA 40 NG AFM
Normal Operating
Procedures
4A.5.10 FUEL TRANSFER
CAUTION
During normal operation fuel is taken from the main tank only.
Therefore fuel must be transferred from the auxiliary tank to the main tank by activating the fuel transfer pump. The transfer rate is approximately 60 US gal/h (227 liter/h).
1. Fuel transfer switch . . . . . . . . . . . . . . . . . . . . |
ON |
NOTE
The transfer pump turns off automatically to avoid overfilling the main tank. The switch remains in its position. If the pump is not turned off, it will continue pumping each time the fuel level in the main tank drops, but only as long as there is fuel in the auxiliary tank. The fuel transfer status light is illuminated only while the pump is running.
2. Fuel transfer switch . . . . . . . . . . . . . . . . . . . . |
OFF, if required |
NOTE
If the fuel transfer status light starts to blink, the fuel transfer pump must be switched off.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 29 |
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Normal Operating |
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DA 40 NG AFM |
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Procedures |
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4A.5.11 DESCENT |
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1. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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2. |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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3. |
Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
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% 4. |
Annunciations / engine indications . . . . . . . . |
monitor |
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END OF CHECKLIST
Page 4A - 30 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM
Normal Operating
Procedures
4A.5.12 APPROACH & LANDING
Approach:
NOTE
If the landing mass exceeds 1216 kg (2681 lb), the landing constitutes an abnormal operating procedure. Refer to Section
4B.7 - LANDING WITH HIGH LANDING MASS.
1. |
Safety harnesses . . . . . . . . . . . . . . . . . . . . . . |
check fastened and tightened |
2. |
Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
no interference by foreign objects |
3. |
Landing light . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
4. |
Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . |
ON |
5. |
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . |
check released |
6. |
Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
Before Landing:
7. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . see table below:
Flaps |
940 kg |
1000 kg |
1080 kg |
1160 kg |
1216 kg |
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(2072 lb) |
(2205 lb) |
(2381 lb) |
(2557 lb) |
(2681 lb) |
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T/O |
68 KIAS |
70 KIAS |
73 KIAS |
76 KIAS |
77 KIAS |
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LDG |
66 KIAS |
69 KIAS |
72 KIAS |
74 KIAS |
76 KIAS |
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8. |
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
9. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
10. |
Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as required |
CONTINUED
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 31 |
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Normal Operating
DA 40 NG AFM
Procedures
11. Final approach speed . . |
. . . . . . . . . . |
. . . . . . see table below: |
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Flaps |
940 kg |
1000 kg |
1080 kg |
1160 kg |
1216 kg |
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(2072 lb) |
(2205 lb) |
(2381 lb) |
(2557 lb) |
(2681 lb) |
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LDG |
66 KIAS |
69 KIAS |
72 KIAS |
74 KIAS |
76 KIAS |
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NOTE
Higher approach speeds result in a significantly longer landing distance during flare.
CAUTION
In conditions such as (e.g.) strong wind, danger of wind shear or turbulence a higher approach speed should be selected.
END OF CHECKLIST
Page 4A - 32 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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