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757 MAINTENANCE MANUAL
MAIN GEAR REACTION LINK - INSPECTION/CHECK
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1. General
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A. This procedure only has 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 Reaction Link - Removal/Installation for the procedures to these tasks.
TASK 32-11-10-206-002
2. Wear Limits for the Downlock Assembly of the Main Landing Gear (Fig 601)
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NOTE: Wear limits for components attached to the reaction link can be found
____
in the Maintenance Manual subject for the components.
A. Wear Limits for the Reaction Link
S 226-001
(1) Refer to Fig. 601 for the inspection points and the wear limit table.
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MAINTENANCE MANUAL
A LINK REACTION B B
A BOLT 1. BUSHING SUPPORT FWD TRUNNION LINK REACTION
BOLT 2. BEARING/
BOLT 1. BUSHING LINK REACTION
INBD
A-A
3. BUSHING/BUSHING 5. BUSHING/PIN
4. BUSHING/PIN UPPER SWIVEL
REACTION LINK
REACTION LINK
B-B
Main Landing Gear Reaction Link Wear Limits
Figure 601 (Sheet 1)
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MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR REPAIR
DIAMETER PER-MITTED WEAR DIM. MAX ANCE CLEAR-DIAM
MIN MAX
1 BUSHING ID 1.7500 1.7510 1.7541 0.0051 X
BOLT OD 1.7485 1.7490 1.7459 X 1
2 BEARING ID 1.7500 1.7510 1.7560 0.0070 X
BOLT OD 1.7485 1.7490 1.7459 X 1
3 BUSHING ID 2.7605 2.7615 2.7658 0.0068 X
BUSHING OD 2.7580 2.7590 2.7547 X
4 BUSHING ID 2.5000 2.5010 2.5052 0.0062 X
PIN OD 2.4980 2.4990 2.4948 X 1
5 BUSHING ID 2.8750 2.8760 2.8814 0.0064 X
PIN OD 2.8730 2.8740 2.8696 X 1
THE PART IS REPAIRABLE; REFER TO THE COMPONENT
MAINTENANCE MANUAL FOR THE REPAIR INSTRUCTIONS.
Main Landing Gear Reaction Link Wear Limits
Figure 601 (Sheet 2)
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757 MAINTENANCE MANUAL
MAIN GEAR DOWNLOCK ASSEMBLY - REMOVAL/INSTALLATION
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1. General
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A. This procedure contains two tasks. The first task removes the downlock assembly for the main landing gear. The second task installs the downlock assembly for the main landing gear.
TASK 32-11-12-004-001
2. Remove the Downlock Assembly for the Main Landing Gear (Fig. 401)
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A. Equipment
(1)
Thread Protector Set, MLG - B32011-14
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