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时间:2011-04-12 10:20来源:蓝天飞行翻译 作者:航空
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 (2)  
Do this task: "Installation of the Door locks on the Wing Landing Gear" (Ref 32-00-30/201).

 S 492-127

 (3)  
Do this task: "Installation of the Door locks on the Body Landing Gear" (Ref 32-00-30/201).

 F.  
Procedure - Perform the two subsequent quick checks of the scraper ring on the landing gear:


 S 212-122
 (1)  Visually examine the chrome surface of the inner cylinder before you clean it.
 NOTE: If you find vertical streaks of fluid or accumulated debris
____ on the chrome surface, it means that part of the scraper ring do not perform well.
 S 212-123
 (2)  Use a mirror and a flashlight to examine the scraper ring.
 NOTE: Put the mirror below the outer cylinder and against the inner
____ cylinder to examine the condition of the scraper ring.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-02
 ALL  ú ú 01 Page 220 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 362-124
 (3)  
If one of the above checks finds a fault on the scraper ring, use the optional split scraper ring to replace the damaged scraper ring.

 (a)  
Release the pressure from the shock strut (Ref 32-13-02/801).

 (b)  
Lower the gland nut.

 (c)  
Cut the damaged scraper ring from the inner cylinder.


 NOTE: Do not scratch the surface of the inner cylinder.
____
 (d)  
Install the split scraper ring.

 (e)  
Tighten the gland nut 2100-2400 inch-pound torque (Ref 32-13-02/801).

 (f)  
Do this task: Body Landing Gear Shock Strut Servicing (12-15-04/301).

 G.
Put the Airplane Back to its Usual Condition.


 S 842-143
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Do this task: "Removal of the Door Locks from the Wing Landing Gear" (Ref 32-00-30/201).

 S 842-144

 (2)  
Do this task: "Removal of the Door Locks from the Body Landing Gear" (Ref 32-00-30/201).


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 32-13-02
 ALL  ú ú 01 Page 221 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 BODY LANDING GEAR SHOCK STRUT - FLUID REPLACEMENT
_________________________________________________
 1.  General
_______
 A.  This procedure has instructions to drain all fluid from the shock strut of the body landing gear. The fluid capacity for each strut is approximately 12.5 gallons. Refer to AMM 12-15-04/301 for filling and pressurization procedures.
 TASK 32-13-02-613-001
 2.  Body Landing Gear Shock Strut Servicing
_______________________________________
 A.  Standard Tools and Equipment
 (1)  
Container - At least 15 gallon capacity

 (2)  
Plastic Tubing - 1/4 or 3/8 inch OD, approximately 7 feet long

 B.  
References

 (1)  
09-11-00/201, Towing

 (2)  
12-15-04/301, Body Landing Gear Shock Strut

 (3)  
32-00-30/201, Landing Gear Door Locks

 (4)  
32-13-02/201, Body Gear Shock Strut

 (5)  
IPC 32-15-01 Fig. 5

 C.  
Access

 (1)  
Location Zone
 755 Body Landing Gear, LH
 765 Body Landing Gear, RH


 D.  
Procedure


 S 863-012
 WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1) Install the ground locks in all landing gear (AMM 09-11-00/201).
 S 493-013
 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 2(141)