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钻石42飞机飞行手册 DA 42 Airplane Flight Manual(58)

时间:2011-10-28 13:17来源:蓝天飞行翻译 作者:admin
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6. FUEL SELECTOR .................... ON (LH/RH)

CAUTION
When taxiing on a poor surface select the lowest possible RPM to avoid damage to the propeller from stones or similar items.
END OF CHECKLIST 4A.6.6 BEFORE TAKE-OFF
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 4A - 25 


1.
Position airplane into wind if possible.

2.
Parking brake ........................  set

 

% WARNING % For take-off the adjustable backrests (if installed) must be % fixed in the upright position.
% 3. Adjustable backrests (if installed) ......... verify upright position % and proper fixation
4.
Safety harnesses .....................  onand fastened


5.
Rear door ...........................  check closed and locked

 

CAUTION
When operating the canopy, pilots/operators must ensure that there are no obstructions between the canopy and the mating frame, for example seat belts, clothing, etc. When operating the locking handle do NOT apply undue force.
A slight downward pressure on the canopy may be required to ease the handle operation.
6.
Front canopy .........................  closedand locked


7.
Front baggage doors...................  closed (visual check)


8.
Door warning (DOOR)..................  check no indication


9.  
Annunciations / Engine / System Page ..... check OK / normal range (except pressure may be in the yellow range with a warm engine and power lever at IDLE)


CONTINUED
Page 4A - 26  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 


10.Circuit breakers ......................  check pressed in

11.Longitudinal Trim .....................  set T/O

12.FUEL SELECTOR ....................  check ON (LH/RH)

13.Directional Trim.......................  neutral

14.FLAPS  ............................. check function & indicator / set UP
15.Flight controls  ........................ unrestricted free movement, correct sense
NOTE
The following test sequence can be executed for both engines simultaneously, or in sequence.
FADEC test sequence:
CAUTION
If the .L/R ECU A/B FAIL“ do not illuminate and extinguish during the test sequence there is a malfunction in the engine control system. Terminate flight preparation.
The whole test procedure must be completed without any error. In case of an error terminate flight preparation, even when the engine seems to run smoothly after the test procedure.
1.
Power lever..........................  IDLE


2.
ECU TEST BUTTON ..................  pressand hold

 

CONTINUED
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 4A - 27 
 
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