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Table 601/27-51-12-993-805
NAME OF THE PARTS
THAT ARE IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
CLEARANCE
inches/mm
#1 BUSHING I.D. 0.2500 in 0.2505 in 0.2545 in
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(Continued)
NAME OF THE PARTS
THAT ARE IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
CLEARANCE
inches/mm
6.3500 mm 6.3627 mm 6.4643 mm 0.0050 in
#1 BOLT O.D. 0.2485 in 0.2495 in 0.2455 in 0.1270 mm
6.3119 mm 6.3373 mm 6.2357 mm
#2 ROD END I.D. 0.2500 in 0.2500 in 0.2500 in
6.3500 mm 6.3500 mm 6.3500 mm 0.0015 in
#2 BOLT O.D. 0.2485 in 0.2495 in 0.2485 in 0.0381 mm
6.3119 mm 9.3373 mm 6.3119 mm
#3 BUSHING I.D. 0.3750 in 0.3756 in 0.3756 in
9.5250 mm 9.6502 mm 9.5402 mm 0.0016 in
#3 BUSHING O.D. 0.3740 in 0.3745 in 0.3740 in 0.0406 mm
9.4993 mm 9.5123 mm 9.4996 mm
#4 BUSHING I.D. 0.2500 in 0.2505 in 0.2545 in
6.3500 mm 6.3627 mm 6.4643 mm 0.0050 in
#4 BOLT O.D. 0.2485 in 0.2495 in 0.2455 in 0.1270 mm
6.3119 mm 6.3373 mm 6.2357 mm
#5 BUSHING I.D. 0.3125 in 0.3130 in 0.3170 in
7.9375 mm 7.9505 mm 8.0518 mm 0.0050 in
#5 BOLT O.D. 0.3110 in 0.3120 in 0.3080 in 0.1270 mm
7.8994 mm 7.9248 mm 7.8232 mm
#6 BUSHING I.D. 0.4375 in 0.4382 in 0.4382 in
11.113 mm 11.130 mm 11.130 mm 0.0017 in
#6 BUSHING O.D. 0.4365 in 0.4370 in 0.4365 in 0.0431 mm
11.087 mm 11.100 mm 11.087 mm
#7 TRACK I.D. 0.3125 in 0.3130 in 0.3170 in
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(Continued)
NAME OF THE PARTS
THAT ARE IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
CLEARANCE
inches/mm
7.9375 mm 7.9505 mm 8.0518 mm 0.0050 in
#7 BOLT O.D. 0.3110 in 0.3120 in 0.3080 in 0.1270 mm
7.8994 mm 7.9248 mm 7.8232 mm
#8 BUSHING I.D. 0.3125 in 0.3131 in 0.3170 in
7.9375 mm 7.9527 mm 8.0518 mm 0.0050 in
#8 BOLT O.D. 0.3110 in 0.3120 in 0.3081 in 0.1270 mm
7.8994 mm 7.9248 mm 7.8257 mm
SUBTASK 27-51-12-420-004
(4) Do this task: Inboard Aft Flap Installation, TASK 27-51-12-400-801.
------------------------- END OF TASK ---------------------------
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Inboard Aft Flap Inspection
Figure 601 (Sheet 1 of 4)/27-51-12-990-804
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Inboard Aft Flap Inspection
Figure 601 (Sheet 2 of 4)/27-51-12-990-804
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Inboard Aft Flap Inspection
Figure 601 (Sheet 3 of 4)/27-51-12-990-804
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Inboard Aft Flap Inspection
Figure 601 (Sheet 4 of 4)/27-51-12-990-804
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INBOARD FLAP CARRIAGES - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the outboard carriage for the inboard flap
(2) An installation of the outboard carriage for the inboard flap
(3) A removal of the inboard carriage for the inboard flap
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(103)
