NOTE: This is an interference fit and it may be necessary to use a
____
 vise.

 S 844-015
 (3)  
Hold the strut door.

 S 414-016

 (4)  
Install the parts that follow to connect the support beam for the door to the door:

 (a)  
Attach bolts for the lever arm (14)

 (b)  
Washers (15)

 (c)  
Nuts (17)
 1) Tighten the nuts to 160-240 pound-inches

 (d)  
Attach bolts for the beam (18, 25, 28, 32, 35, 39, 43, 47)

 (e)  
Washers (19, 20, 26, 29, 30, 33, 36, 37, 40, 44, 45, 48)

 (f)  
Nuts (21, 27, 31, 34, 38, 42, 46, 49) 1) Tighten the nuts (21) to 290-510 pound-inches 2) Tighten the nuts (27, 31, 34, 38, 42, 46, 49) to the

 standard torque.
 S 414-017
 (5)  
Install the parts that follow to connect the strut door to the upper support fitting at the trunnion link (Detail C):

 (a)  
Attach bolt (10)

 (b)  
Washers (11, 12)

 (c)  
Nut (13) 1) Install the washers under the bolthead and the nut 2) Tighten the nut to 660-980 pound-inches

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757 MAINTENANCE MANUAL
 S 414-018
 (6)  
Install the parts that follow to connect the strut door to the lower adjustable link on the lower fitting of the strut door:

 (a)  
Bolt (6)

 (b)  
Washers (7, 8)

 (c)  
Nut (9)
 1) Tighten the nut to 660-980 pound-inches

 E.
Put the Airplane Back to Its Usual Condition

 S 824-027
 (1) Adjust the strut door for the main landing gear (AMM 32-12-00/501).
 NOTE: Adjustment of the strut door is not necessary if the same
____ door, attaching hardware and adjustment rods that were removed are reinstalled and the jamnuts on the adjustment rods are not loosened.
 S 094-022
 WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  Remove the door locks for the landing gear and close the doors (AMM 32-00-15/201).
 

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757 MAINTENANCE MANUAL
 MAIN GEAR STRUT DOOR - INSPECTION/CHECK
_______________________________________
 1.  General_______
 A.  This procedure only has illustrations, and wear limit tables which show the data for wear limits. There are no procedures for access, removal, or installation of the parts. Refer to the Main Gear Strut Door -Removal/Installation for procedures to do these tasks.
 TASK 32-12-04-206-001
 2.  Wear Limits for the Strut Door of the Main Landing Gear (Fig. 601)_______________________________________________________
 A.  Wear Limits for the Strut Door
 S 226-002
 (1)  Refer to Fig. 601 for the inspection points and the wear limits tables.
 

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MAINTENANCE MANUAL

TRUNNION 
LINK 
STRUT 
DOOR  FITTING FOR THE 
CENTER SUPPORT 
SEE  C  SEE  D  B  B  EQUALIZER 
SHOCK 
STRUT  A 
STRUT DRAG  A  A  A  (2 LOCATIONS) FITTING CENTER DOOR 
SEE  A  A  A  A  A 
　
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 1(159)