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时间:2011-03-25 17:55来源:蓝天飞行翻译 作者:admin
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 4. Procedure
_________
 Subtask 32-31-00-720-052
 A. Functional Test of the Normal Extension and Retraction of the Landing Gear
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
 NOTE : During the test procedure, monitor the retraction and extension
____
 times:

 -
the retraction cycle (from the first door-uplock open to the last door-uplock closed) is between 10 and 15 seconds

 -
the extension cycle (from the first door-uplock open to the last door-uplock closed) is between 15 and 21 seconds

 -
the minimum flow capacity necessary from the ground hydraulic cart is 140 l.min (36.9837 USgal.mn).


 1EFF : ALL 1 32-31-00Page 579 1 1 Aug 01/05 1 1 1CES 1 (1) Do this test:


 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the panel 402VU, make sure that the LDG GEAR down and locked lights are on (green).

 2.
 On the ECAM CP:

-push (in) the WHEELS pushbutton switch (P/BSW).

3.
 On the panel 400VU:


-move the landing-gear control-lever 6GA to the UP position.
On the ECAM lower DU:
-
the door symbols show the closed andlocked position (green)

 -
the landing gear systems 1 and 2 symbols show the down and locked position (green).

On the panel 402VU:

-
the LDG GEAR UNLK lights come on(red).

 On the ECAM lower DU:

 -
the door symbols show the closed and locked position (green)

 -
the L/G CTL caption comes into view (amber).

 On the aircraft:

 -
the doors start to open.

 On the ECAM lower DU:

 -
the door symbols move to the open position (amber).

 On the aircraft:

 -
the doors are fully open

 -
the L/G starts to retract.

 On the panel 402VU:

 -
the LDG GEAR down and locked lights go off.

 On the ECAM lower DU:

 -
the landing gear systems 1 and 2 symbols change color (red).


 1EFF : ALL 1 32-31-00Page 580 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------On the aircraft:
 -
the L/G is retracted and locked up.

 On the panel 402VU:

 -
the LDG GEAR down and locked lights go off

 -
the LDG GEAR UNLK lights go off.

 On the ECAM lower DU:

 -
the L/G CTL caption goes out of view

 -
the landing gear systems 1 and 2 symbols go out of view.

 On the aircraft:

 -
the doors start to close.

 On the ECAM lower DU:

 -
the door symbols move to the closed position (amber).

 On the aircraft:

 -
the doors are closed and locked up.

 On the ECAM lower DU:

 -
the door symbols show the closed and locked position (green).


 4. On the panel 400VU:  On the panel 402VU:
 -move the landing-gear  - the LDG GEAR UNLK lights come on
 control-lever 6GA to the DOWN (red).
 position.

 On the ECAM lower DU:
 -
the L/G CTL caption comes into view (amber).

 -
the doors start to open.

 On the ECAM lower DU:

 -
the door symbols move to the open position (amber).


 On the aircraft:
 On the aircraft:
 1EFF : ALL 1 32-31-00Page 581 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-
the doors are fully open

 -
the L/G starts to extend.

 On the ECAM lower DU:

 -
the door symbols show the open position (amber)

 -
the landing gear systems 1 and 2 symbols come into view (red).

 On the aircraft:

 -
the L/G gear is down and locked.

 On the panel 402VU:

 -
the LDG GEAR UNLK lights go off (red)

 -
the LDG GEAR down and locked lights come on (green).

 On the ECAM lower DU:

 -
the L/G CTL caption goes out of view

 -
the landing gear systems 1 and 2 symbols change color (green).

 On the aircraft:

 -
 
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