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钻石40飞机飞行手册 DA 40 Airplane Flight Manual(34)

时间:2011-10-28 12:56来源:蓝天飞行翻译 作者:admin
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2.
Power lever .........................  performance as required


3.
Trim ...............................  as required


4.  
Fuel transfer......................... repeat as required (in accordance with 4A.3.10 - FUEL TRANSFER)


%  NOTE
% The engine manufacturer recommends a cruise power setting % of 70 %.
NOTE
Proper operation of the transfer pump must be checked by monitoring the fuel quantities (increasing in the MAIN tank, decreasing in the AUX tank).
4A.3.10 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 liters/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.
%

Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 4A - 19 


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.
4A.3.11 DESCENT
1. Power lever .........................  as required

4A.3.12 LANDING APPROACH
1.
Safety harnesses .....................  check fastened & tightened


2.
Airspeed............................  reduce to operate flaps (108 KIAS)


3.
Flaps ..............................  T/O


4.
Trim ...............................  as required


5.
Landing light.........................  as required

 

before landing:
6.
Power lever .........................  as required


7.
Airspeed............................  reduce to operate flaps (91 KIAS)


8.
Flaps ..............................  LDG


9.  
Approach speed...................... 67 KIAS (1092 kg, 2407 lb)
63 KIAS (1000 kg, 2205 lb)
58 KIAS (850 kg, 1874 lb)

 

NOTE
Higher approach speeds result in a significant longer landing distance during flare.
%

Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 4A - 20 


CAUTION
In conditions such as (e.g.) strong wind, danger of wind shear or turbulence a higher approach speed should be selected.
4A.3.13 GO-AROUND
1.
Power lever .........................  MAX
 
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