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A
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MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER DIM. ALLOWED WEAR ANCE CLEAR-MAX DIAM
MIN MAX
1 HINGE ID 0.5625 0.5655 0.5675 0.014 X
PIN OD 0.5555 0.5560 0.5360 X
2 HINGE ID 0.4375 0.4405 0.4425 0.014 X
PIN OD 0.4305 0.4310 0.429 X
3 HINGE ID 0.3750 0.3780 0.3800 0.014 X
PIN OD 0.3680 0.3685 0.3660 X
4 LATCH CAM ID 1.084 1.104 1.1240 0.173 X
LATCH PIN OD 3 3 4 X
5 LATCH CAM ID 1.3750 1.3850 1 0.111 5
LATCH PIN OD 1.3340 1.3350 1.3240
6 BUSHING ID 0.8766 0.8776 2 2 X
SHAFT OD 0.8733 0.8743 0.8710 X
7 BUSHING ID 0.8780 0.8790 2 2 X
SHAFT OD 0.8733 0.8743 0.8710 X
8 HOUSING ID 0.3281 0.3321 0.3380 0.040 X
PUSHROD OD 0.3080 0.3100 0.2980 X
9 HOUSING ID 0.2570 0.2610 0.2750 0.035 X
PUSHROD OD 0.2500 0.2550 0.2400 X
10 HOUSING ID 0.3281 0.3321 0.3380 0.040 X
PUSHROD OD 0.3070 0.3100 0.2980 X
Side Cargo Door Wear Limits
Figure 601 (Sheet 5)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER DIM. ALLOWED WEAR ANCE CLEAR-MAX DIAM
MIN MAX
11 BUSHING ID 1.6030 1.6050 1.6080 0.0115 5
SHAFT OD 1.5985 1.5990 1.5965 X
12 SPACER ID 1.6030 1.6050 1.6080 0.0115 5
SHAFT OD 1.5985 1.5990 1.5965 X
13 HOOK ID 1.135 1.175 6 0.155 5
PIN OD 1.110 1.130 1.070 X
SEE DETAIL F FOR SATISFACTORY DIMENSION OF LATCH CAM REPLACE IF THE TEFLON LAYER IS NOT SATISFACTORY SMALL DIAMETER: MIN = 0.681 INCH
MAX = 0.702 INCH LARGE DIAMETER: MIN = 0.991 INCH
MAX = 1.002 INCHES MAXIMUM DAMAGE 0.040 INCH AT ANY LOCATION AROUND THE EDGE OF THE PIN. ONLY ONE DAMAGED LOCATION PERMITTED FOR EACH PIN REPAIR THE PART. REFER TO OVERHAUL MANUAL NOT TO BE DECREASED MORE THAN 0.025 INCH
Side Cargo Door Wear Limits
Figure 601 (Sheet 6)
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MAINTENANCE MANUAL
FWD
LATCH FITTING SEE A
Side Cargo Door Mechanism Adjustment
Figure 602 (Sheet 1)
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