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E56587
A
737-300/400/500MAINTENANCE MANUAL
 MAIN LANDING GEAR SIDE STRUT - INSPECTION/CHECK
_______________________________________________
 1.  General
_______
 A.  This procedure only has illustration and a wear limits table which shows the data for wear limits. There are no procedures for the access, the removal, or the installation of the parts. Refer to the Main Landing Gear Side Strut - Removal/Installation for procedures to do these tasks.
 TASK 32-11-61-206-001
 2.  Wear Limits for the Side Strut of the Main Landing Gear (Fig. 601)
_______________________________________________________
 A.  Wear Limits for the Side Strut
 S 226-002
 (1)  Refer to Fig. 601 for the inspection points and the wear limits table.
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 32-11-61
 ALL  ú ú 01 Page 605 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 MAIN GEAR REACTION LINK - REMOVAL/INSTALLATION
______________________________________________
 1. General
 A. This procedure removes and installs the main gear reaction link.
 TASK 32-11-71-004-001
 2.  Remove Main Gear Reaction Link (Fig. 401)______________________________
 A. Special Tools and Equipment
 (1)  Thread Protector and Alignment Tool:
 F80115-13 (F80115-4, Optional)
 Use on 737-400 airplanes to protect the threads of the bolts which
 connect the reaction link to the universal, and the uplock crank.

 Use on 737-300/-500 airplanes to protect the threads of the bolt
 which connects the reaction link to the side strut.

 (2)  Thread Protector and Alignment Tool:
 F80115-17 (F80115-9, Optional) - Use on 737-400 airplanes to protect the threads of the bolt which connects the reaction link to the side strut.
 F80115-12 (F80115-3, Optional) - Use on 737-300/-500 airplanes to protect the threads of the bolts which connect the reaction link to the universal, and the uplock crank.
 (3)  
Thread Protector and Alignment Tool- F80115-14 (F80115-5, Optional) Use on 737-300/-400/-500 airplanes to protect the threads of the bolt which connects the reaction link to the lock strut.

 B.
Standard Tools and Equipment

 (1)  
Pins - Ground Lock

 C.
References

 (1)  
AMM 07-11-11/201, Airplane Jacking

 (2)  
AMM 32-00-01/201, Ground Lockpins

 (3)  
AMM 32-32-91/401, Downlock Springs

 D.
Access

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

 E.
Remove the Main Gear Reaction Link

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

 S 584-003

 (2)  
Lift the airplane on jacks until the wheels almost touch the ground (AMM 07-11-11/201).

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 32-11-71
 ALL  ú ú 01 Page 401 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE  SEE SEE SEE B A E  C 
SEE  D 
FWD  INBD 
1.  DOWNLOCK ACTUATOR 
2.  DOWNLOCK SPRING 
LOCK STRUT 3. 4. LINK REACTION 
Main Gear Reaction Link Installation Figure 401 (Sheet 1) A 

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 32-11-71
 ALL  ú ú 01 Page 402 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FWD INBD
14.  KEEPER 4. REACTION LINK
1. DOWNLOCK ACTUATOR
3. LOCK
STRUT6. UPLOCK
　
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