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时间:2011-04-17 09:16来源:蓝天飞行翻译 作者:航空
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 S 864-039-N00
 (5)  Remove the DO-NOT-OPERATE tags from the thrust levers.
 S 714-016-N00
 (6)  Operate the thrust reverser, manual or power method
 (AMM 78-31-00/201).
 NOTE:____ Operate the thrust reverser a minimum of three full cycles
 to make sure it is serviceable.

 S 044-040-N00
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE SPEED BRAKE CONTROL
_______ SYSTEM. IF YOU DO NOT DO THIS, THE SPOILERS CAN MOVE QUICKLY WHEN YOU MOVE THE THRUST LEVERS. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (7)  
Do the deactivation procedure for the speed brake control system (AMM 27-62-00/201).

 S 864-041-N00

 (8)  
Make sure the forward thrust levers are in the idle position and attach the DO-NOT-OPERATE tags.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-31-15
 ALL  ú ú N01 Page 408 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 864-042-N00
 (9)  Make sure the reverse thrust levers are in the fully stowed position and attach the DO-NOT-OPERATE tags.
 S 044-043-N00
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE THRUST REVERSER TO
_______ PREVENT THE OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
 (10)
 Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).

 S 214-037-N00

 (11)
 Make sure each blocker door makes a continuous surface with (is at the same level as) the adjacent structure (AMM 78-31-14/601).


 NOTE: The blocker doors must not extend above the surface of the
____ fan cowl when the thrust reverser is fully retracted.
 E. Put the Airplane Back to Its Usual Condition.
 S 444-044-N00
 (1)  
Do the activation procedure for the thrust reverser
 (AMM 78-31-00/201).


 S 444-045-N00

 (2)  
Do the activation procedure for the speed brake control system (AMM 27-62-00/201).

 (3)  
Remove the DO-NOT-OPERATE tags from the thrust levers.


 S 864-046-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-31-15
 ALL  ú ú N01 Page 409 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
THRUST REVERSER BLOCKER DOOR DRAG LINKS - INSPECTION/CHECK
__________________________________________________________
 1.  General
_______
 A.  The thrust reverser blocker door drag links are referred to as the drag links in this procedure.
 B.  This procedure gives instructions to examine the drag links for damage without opening the thrust reverser.
 TASK 78-31-15-206-001-N00
 2.  Do a Check of the Thrust Reverser Blocker Door Drag Links
_________________________________________________________
 A.  References
 (1)  
AMM 27-62-00/201, Speed Brake Control System

 (2)  
AMM 78-31-00/201, Thrust Reverser System

 (3)  
AMM 78-31-15/401, Thrust Reverser Blocker Door Drag Links

 B.  
Access

 (1)  
Location Zones
 410 Engine 1 Nacelles
 420 Engine 2 Nacelles
 430 Engine 3 Nacelles
 440 Engine 4 Nacelles


 (2)  
Access Panels 415 and 416 Engine 1 - Thrust Reverser Halves 425 and 426 Engine 2 - Thrust Reverser Halves 435 and 436 Engine 3 - Thrust Reverser Halves 445 and 446 Engine 4 - Thrust Reverser Halves

 C.  
Prepare to Do a Check of the Drag Links.


 S 046-016-N00
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE SPEED BRAKE CONTROL
_______ SYSTEM. IF YOU DO NOT DO THIS, THE SPOILERS CAN MOVE QUICKLY WHEN YOU MOVE THE THRUST LEVERS. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  Do the deactivation procedure for the speed brake control system (AMM 27-62-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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