C.
Access
(1)
Location Zone
522 Variable Camber Flap, LH
523 Variable Camber Flap, LH
524 Variable Camber Flap, LH
525 Variable Camber Flap, LH
526 Variable Camber Flap, LH
532 Variable Camber Flap, LH
533 Variable Camber Flap, LH
534 Variable Camber Flap, LH
535 Variable Camber Flap, LH
536 Variable Camber Flap, LH
537 Variable Camber Flap, LH
622 Variable Camber Flap, RH
623 Variable Camber Flap, RH
624 Variable Camber Flap, RH
625 Variable Camber Flap, RH
626 Variable Camber Flap, RH
632 Variable Camber Flap, RH
633 Variable Camber Flap, RH
634 Variable Camber Flap, RH
635 Variable Camber Flap, RH
636 Variable Camber Flap, RH
637 Variable Camber Flap, RH
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A
747-400
MAINTENANCE MANUAL
B
A
B
A
VARIABLE CAMBER FLAP
Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 1)
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A 747-400 MAINTENANCE MANUAL
1. BEARING/TORQUE TUBE
B-B
Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 2)
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MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE WORN PART REPAIR WORN PART REPAIR INSTR
DIAMETER DIM. WEAR MITTED PER- DIA MAX CLEAR-ANCE
MIN MAX
1 BEARING ID 2.6239 2.6250 2.6279 0.0045 X
TORQUE TUBE OD 2.6229 2.6334 2.6194 X
1 2 BUSHING ID 0.7725 0.7735 0.7780 0.0055 X
SPACER OD 0.7710 0.7725 0.7670 X
2 2 BUSHING ID 0.7495 0.7505 0.7550 0.0055 X
SPACER OD 0.7480 0.7495 0.7440 X
3 BEARING ID 0.5620 0.5625 0.5680 0.0065 X
BOLT OD 0.5610 0.5615 0.5555 X
4 BUSHING ID 0.5625 0.5640 0.5665 0.0050 X
BOLT OD 0.5610 0.5615 0.5575 X
5 SPACER ID 0.5620 0.5650 0.5680 0.0065 X
BOLT OD 0.5610 0.5615 0.5555 X
FLAPS NO. 1E-5 AND 22-26E
FLAPS NO. 6-10 AND 17-21
Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 3)
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MAINTENANCE MANUAL
D. Do a Check of the Variable Camber Flap Actuating Linkage
S 026-005
(1)
Do this task: "Variable Camber Flap Actuating Linkage Removal" (AMM 27-81-08/401).
S 226-003
(2)
Do a check of the actuating linkage (Fig. 601):
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本文链接地址：747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 7(142)
