S 434-060

 (19)
 Install the strut door if it was removed (AMM 32-12-04/401).

 G.
Put the Airplane Back to Its Usual Condition

 S 494-049
 (1)  
Remove the axle jacks (AMM 07-11-03/201).

 (2)
Lubricate the truck at the grease fittings (AMM 12-21-14/301).

 (3)  
Lower the airplane and remove the jacks (AMM 07-11-01/201).

 S 714-041

 (4)  
Do the test of the truck tilt sensors with the deactuator test tool (AMM 32-09-07/201).

 S 644-050
 S 584-051
 

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757 MAINTENANCE MANUAL
 (5)  S 864-052Close these circuit breakers on the overhead circuit breaker panel, P11: (a) 11S18, LDG GEAR ANTISKID 1-5 (b) 11C31, ANTISKID 2-6 (Left Gear) (c) 11C32, ANTISKID 3-7 (Right Gear) (d) 11S22, ANTISKID 4-8 (Right Gear) (e) AIRPLANES WITH TEMPERATURE MONITORING SYSTEM; 11S16, BRAKE TEMP
 (6)  S 714-039Do the test of antiskid operation for the antiskid transducers that were disconnected (AMM 32-42-06/401).

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757 MAINTENANCE MANUAL
 MAIN GEAR TRUCK ASSEMBLY - INSPECTION/CHECK
___________________________________________
 1.  General_______
 A.  This procedure contains two tasks. The first task consists of only an illustration, and a wear limit table which shows the data for wear limits. There are no procedures for access removal or installation of the parts. Refer to the Main Gear Truck Assembly - Removal/Installation for the procedures to do these tasks. The second task gives instruction to inspect and clear the drain hole in the aft section of the truck beam.
 (1)  
The first task consists of only an illustration, and a wear limit table which shows the data for wear limits. There are no procedures for access removal or installation of the parts. Refer to the Main Gear Truck Assembly - Removal/Installation for the procedures to do these tasks.

 (2)  
The second task gives instruction to inspect and clear the drain hole in the aft section of the truck beam.

 TASK 32-11-17-206-002
 2.  Wear Limits for the Truck Assembly of the Main Landing Gear (Fig. 601)___________________________________________________________
 A.  Wear Limits for the Truck Assembly
 S 226-001
 (1)  Refer to Fig. 601 for the inspection points and the wear limits table.
 TASK 32-11-17-206-009
 3.  Inspect the Drain Hole in the Aft Section of the Truck Beam (Fig. 602)___________________________________________________________
 A.  Special Tools and Equipment
 (1)  
Wooden Rod 1/8 inch (0.3 cm) in diameter, more than 1 foot (30 cm) long. Commercially available.

 B.  
References

 (1)  
AMM 32-00-20/201 Landing Gear Downlocks

 C.  
Access

 (1)  
Location Zones
 731/741 Main Landing Gear (MLG)

 D.  
Prepare for the Inspection

 (1)  
Install the ground lockpins for the landing gear (AMM 32-00-20/201).

 (2)  
Put chocks around the wheels.

 S 486-005
 S 586-006
 

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MAINTENANCE MANUAL

FWD 
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1. BUSHING/PIN  SHOCK STRUT INNER CYLINDER  SHOCK STRUT INNER CYLINDER  1. BUSHING/PIN 
　
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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(116)