INTERFERENCE FIT.
THE PART IS REPAIRABLE; REFER TO THE COMPONENT MAINTENANCE MANUAL FOR THE REPAIR INSTRUCTIONS.
Main Landing Gear Strut Door Wear Limits
Figure 601 (Sheet 5)
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MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR REPAIR
DIAMETER MITTED PER-WEAR DIM. MAX ANCE CLEAR-DIAM
MIN MAX
12 BEAM ASSEMBLY ID 1.4500 1.4508 1.4523 1 X 2
BUSHING OD 1.4515 1.4523 1.4500 X
13 BEAM ASSEMBLY ID 1.0010 1.0020 1.0100 0.0100 X 2
BEARING OD 0.9995 1.0000 0.9920 X
14 BEARING ID 0.4995 0.5000 0.5055 0.0060 X
BOLT OD 0.4985 0.4995 0.4940 X
15 LINK ID 0.5050 0.5150 0.5045 0.0050 X
BOLT OD 0.4985 0.4995 0.5100 X
16 FITTING ID 1.0010 1.0020 1.0100 0.0100 X 2
BEARING OD 0.9995 1.0000 0.9920 X
17 BUSHING ID 0.3752 0.3737 0.3795 0.0050 X
CLEVIS OD 0.3735 0.3745 0.3707 X
18 CLAMP ID 0.5002 0.5008 0.5016 1 X
BUSHING OD 0.5010 0.5016 0.5002 X
19 ROD END ID 0.3745 0.3750 0.3795 0.0050 X
CLEVIS OD 0.3735 0.3745 0.3700 X
20 EYEBOLT ID 0.3130 0.3160 0.3170 0.0050 X
BOLT OD 0.3110 0.3120 0.3110 X
21 CLEVIS ID 0.3130 0.3160 0.3170 0.0050 X
BOLT OD 0.3110 0.3120 0.3110 X
22 TURN BARREL ID 0.3130 0.3160 0.3170 0.0050 X
BOLT OD 0.3110 0.3120 0.3110 X
Main Landing Gear Strut Door Wear Limits
Figure 601 (Sheet 6)
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MAIN GEAR TRUNNION FAIRING DOOR - REMOVAL/INSTALLATION
______________________________________________________
1. General_______
A. This procedure contains two tasks. The first task removes the trunnion fairing door. The first task also includes steps to remove the pushrod if you do not need to remove the trunnion fairing door. The second task installs the trunnion fairing door and also includes steps for installation of the pushrod.
TASK 32-12-10-004-001
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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(161)
