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12.598 mm 12.675 mm 12.675 mm 0.0090 in
#1 BOLT O.D. 0.4900 in 0.4930 in 0.4900 in 0.2286 mm
12.446 mm 12.522 mm 12.446 mm
#2 BUSHING I.D. 0.6245 in 0.6252 in 0.6278 in
15.862 mm 15.880 mm 15.946 mm 0.0064 in
#2 BOLT O.D. 0.6230 in 0.6240 in 0.6214 in 0.1626 mm
15.824 mm 15.850 mm 15.784 mm
#3 FITTING I.D. 0.6250 in 0.6255 in 0.6255 in
15.875 mm 15.888 mm 15.888 mm 0.0025 in
#3 BOLT O.D. 0.6230 in 0.6240 in 0.6230 in 0.0635 mm
15.824 mm 15.850 mm 15.824 mm
#4 BUSHING I.D. 0.7500 in 0.7507 in 0.7507 in
19.050 mm 19.068 mm 19.068 mm 0.0027 in
#4 BOLT I.D. 0.7480 in 0.7490 in 0.7480 in 0.0686 mm
18.999 mm 19.025 mm 18.999 mm
SUBTASK 27-51-15-420-013
(4) Do this task: Inboard Flap Inboard Track Installation, TASK 27-51-15-400-802.
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Inboard Flap Inboard Flap Track Inspection
Figure 602 (Sheet 1 of 3)/27-51-15-990-804
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Inboard Flap Inboard Flap Track Inspection
Figure 602 (Sheet 2 of 3)/27-51-15-990-804
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Inboard Flap Inboard Flap Track Inspection
Figure 602 (Sheet 3 of 3)/27-51-15-990-804
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INBOARD AFT FLAP TRACKS - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the aft flap tracks for the inboard flap
(2) An installation of the aft flap tracks for the inboard flaps.
B. This procedure is applicable to the two aft flap tracks on the inboard flap.
TASK 27-51-16-000-801
2. Inboard Aft Flap Track Removal
(Figure 401)
A. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-12-000-801 Inboard Aft Flap Removal (P/B 401)
27-51-18-000-802 Inboard Flap Support Aft Fairing Removal (P/B 401)
B. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
C. Prepare for the Removal
SUBTASK 27-51-16-010-001
(1) Do this task: Inboard Flap Support Aft Fairing Removal, TASK 27-51-18-000-802.
SUBTASK 27-51-16-860-001
(2) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
Flaps, TASK 27-51-00-860-804.
SUBTASK 27-51-16-040-001
(3) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-51-16-020-001
(4) Do this task: Inboard Aft Flap Removal, TASK 27-51-12-000-801.
D. Inboard Aft Flap Track Removal
SUBTASK 27-51-16-020-002
(1) Remove aft flap track [2] from the main flap [1]:
(a) Remove the nuts [4] that attach the cartridge assemblies [3] and cartridge assemblies [5] to
the aft flap track support [6] on the main flap [1].
NOTE: There are two cartridge assemblies [3] and two cartridge assemblies [5] on the
inboard and the outboard aft flap track supports.
(b) Remove the cartridge assemblies [3] and cartridge assemblies [5] from the aft flap track
support [6].
(c) Carefully remove the aft flap track [2] from the aft flap track support [6].
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Inboard Aft Flap Track Installation
Figure 401 (Sheet 1 of 2)/27-51-16-990-801
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Inboard Aft Flap Track Installation
Figure 401 (Sheet 2 of 2)/27-51-16-990-801
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(121)
