S 974-049

 (12)
 Measure and write the run-on torque value.

 S 434-050

 (13)
 Tighten the nut to 400 | 25 pound-inches lube torque plus run-on torque.

 S 434-035

 (14)
 Install the washer on the T-bolt against the lower drag strut.

 S 434-036

 (15)
 Add the nut and tighten to a torque of 1200-1500 pound-inches.

 S 434-037

 (16)
 Put the upper drag strut in the lower drag strut and align the holes.

 S 434-038

 (17)
 Install the bolt with the head end on the same side of the lower drag strut as the anti-rotation lug.

 S 434-039

 (18)
 Add the washer and the nut.

 S 434-040

 (19)
 Tighten the nut hand-tight.

 S 434-041

 (20)
 If it is necessary, loosen the nut to align the nearest slot and install the cotter pin.

 S 424-042

 (21)
 Connect the lower side strut to the universal assembly.

 (a)  
Put the lower side strut in the clevis on the universal assembly.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-42
 ALL  ú ú 01 Page 405 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)
Install the attachment bolt with the head end outboard.

 (c)
Add the washer and the nut.

 (d)
Tighten the nut to a torque of 400 pound-inches.

 S 094-043
 (22)
 Remove the axle jack below the inner cyliner.

 S 584-044

 (23)
 Lower the airplane and remove the jacks (Ref 7-11-11).

 S 424-045

 (24)
 Put the inner door of the shock strut in its position and connect the control rod assembly.

 S 434-046

 (25)
 Install the bracket clamp for the electrical harness on the lower drag strut.

 (26)
 Install the hydraulic line support on the lower drag strut.

 S 434-047
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-42
 ALL  ú ú 01 Page 406 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 MAIN GEAR TORSION LINKS - REMOVAL/INSTALLATION
______________________________________________
 1.  General_______
 A.  This procedure removes and installs the main gear torsion links.
 B.  The main gear torsion links are removed after damage, or when bushings are worn beyond service limits. Removal of the upper torsion link also disconnects the bottom end of the lower drag strut. On the right gear, the upper torsion link is connected to a spoiler lockout mechanism. The main tires should be removed and the shock strut partially extended to provide clearance for the upper torsion link pin when replacing the upper torsion link. The main gear brakes also should be removed to provide clearance for the lower torsion link pin when replacing the lower torsion link.
 TASK 32-11-51-004-001
 2.  Remove the Main Gear Torsion Links (Fig. 401)__________________________________
 A.  Standard Tools and Equipment
 (1)  
Pins - Ground Lock

 B.  
References

 (1)  
AMM 7-11-11/201, Airplane Jacking

 (2)  
AMM 32-00-01/201, Gound Lock Pins

 (3)  
AMM 32-41-41/401, Main Gear Brakes

 (4)  
AMM 32-45-11/401, Main Gear Wheels

 C.  
Access

 (1)  
Location Zones
 310 Left Main Landing Gear
 410 Right Main Landing Gear

 D.  
Remove Main Gear Torsion Links (Fig. 401)

 S 844-002
 (1)  
Make sure that all the ground lockpins are installed (AMM 32-00-01/201).

 S 844-016

 (2)  
If the upper torsion link will be replaced, do the steps that follow:

 (a)  
Remove the main gear wheels (AMM 32-45-11/401).

 (b)  
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 1(90)