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时间:2011-04-10 10:19来源:蓝天飞行翻译 作者:航空
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 (e)  
Attach the retainer with the bolts (15) and the washers (14).

 (f)  
Tighten the bolts to 36-44 pound-inches (4-5 N-m).

 (g)  
Install the lockwire on the bolts.


 S 834-067
 (7)  If you replaced the pushrod or the actuator rod, or changed their length, do this task: "Aftflap Drive Mechanism Adjustment" (Ref Paragraph 16)
 NOTE: If you only replaced the midflap crank, do the aftflap
____
 adjustment check.

 F. Aftflap Adjustment Check
 S 864-068
 (1)  
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).

 S 834-069

 (2)  
Examine the adjustment of the aftflap drive mechanism:

 (a)  
Push the ALTN FLAPS ARM switch to put the flaps in alternate control.


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747-400
MAINTENANCE MANUAL

 (b)  
Make sure the hooks on the geneva cams (35) are in the released position (Detail E, Fig. 401).

 CAUTION:_______MONITOR THE FLAP MOVEMENT CAREFULLY. THE FLAPS CAN BE DAMAGED BY INCORRECTLY ADJUSTED COMPONENTS.

 (c)  
Turn the ALTN FLAPS switch to move the ball screw nut to the position shown in Fig. 402.

 (d)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 1)  P415 Power Distribution Center - Right
 a) 415M24 ALT OUTBD TE FLAPS


 (e)  
Make sure the aftflap is in the position shown in Section B-B, Fig. 401.


 S 834-070
 (3)  
If the dimension is not in the tolerance, do this task: "Aftflap Drive Mechanism Adjustment" (Ref Paragraph 16).

 S 864-071

 (4)  
If the dimension is in the tolerance, move the flap control lever to the position of the flaps.

 S 864-072

 (5)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P415 Power Distribution Center - Right
 1) 415M24 ALT OUTBD TE FLAPS

 

 S 864-073
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
 (6)  
Push the ALTN FLAPS ARM switch to disarm the alternate control.

 S 864-074

 (7)  
Do this task to pressurize hydraulic system No. 4: "Hydraulic System Pressurization" (AMM 29-11-00/201).


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A
747-400 MAINTENANCE MANUAL
 S 714-102
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
 (8)  
Extend and retract the flaps slowly.

 (a)  
Make sure the flaps move smoothly.


 S 644-076
 (9)  
Do this task to lubricate the aftflap drive mechanism: "Trailing Edge Flap System Lubrication" (AMM 12-21-20/301).

 G.
Put the Airplane Back to Its Usual Condition


 S 864-077
 (1)
Put the flap control lever in the UP detent to retract the flaps.

 S 864-078

 (2)  
Do this task to depressurize hydraulic system No.4: "Hydraulic System Depressurization" (AMM 29-11-00/201).

 (3)  
Do this task: "Remove Electrical Power" (AMM 24-22-00/201).


 S 864-079
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