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1. POWER lever ........................ performance as required
NOTE
The engine manufacturer recommends a cruise power setting of 70 %.
2.
Trim................................ asrequired
3.
Annunciations/Engine/System Page ....... monitor
END OF CHECKLIST
Use of the Auxiliary fuel tanks (if installed)
The auxiliary fuel tanks are optional equipment (O.M 42-056).
CAUTION
When operating the FUEL TRANSFER LH/RH switch, make sure not to exceed the fuel imbalance limitations given in Section 2.14.
To avoid additional imbalance in the auxiliary tanks both FUEL TRANSFER switches must be operated simultaneously.
1. Transfer the first half of the auxiliary fuel:
As soon as the fuel quantity in each main fuel tank is 17 US gal or less, set both FUEL TRANSFER switches to ON until the main tanks are full again.
CONTINUED
Page 4A - 34 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
% Monitor the fuel quantity indicator to verify that fuel is properly transferred to both main % fuel tanks (approx. 1 US gal per minute). If the fuel quantity in a main tank does not % increase during fuel transfer, proceed according to Section 4B.10 - L/R FUEL % TRANSFER FAIL.
2. Transfer the second half of the auxiliary fuel:
Repeat the procedure described above.
NOTE
Transfer the fuel from the auxiliary tanks to the main tanks as soon as possible. The fuel in the auxiliary tanks must be transferred to the main tanks to become available for the current flight mission.
END OF CHECKLIST
4A.6.10 DESCENT
1.
POWER lever ........................ as required
2.
Airspeed ............................ as required
3.
Trim ............................... as required
4.
Annunciations/Engine/System Page ....... monitor
END OF CHECKLIST 4A.6.11 APPROACH & LANDING
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 4A - 35
Approach:
% WARNING % For landing the adjustable backrests (if installed) must be % fixed in the upright position.
1. Adjustable backrests (if installed) ......... adjust to the upright position described by a placard on the roll-over bar and verify proper fixation
NOTE
If the landing mass exceeds 1700 kg (3748 lb), the landing constitutes an abnormal operating procedure. Refer to Section 4B.8.
2.
Safety harnesses ..................... check fastened and tightened
3.
Controls............................. no interference by foreign objects
4.
Landing light ......................... as required
5.
Gear warning horn .................... check function
6.
Fuel Selector......................... check ON
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本文链接地址：钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 3(14)
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