曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
TASK 27-51-14-000-801
2. Inboard Aft Flap Actuating Mechanism Removal
(Figure 401)
A. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
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 27-51-14-860-001
(1) Extend the trailing edge flaps to the 40-unit position. To extend them, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-51-14-040-001
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-51-14-010-001
(3) Do this task: Inboard Flap Support Aft Fairing Removal, TASK 27-51-18-000-802.
SUBTASK 27-51-14-010-002
(4) Remove the upper skin panel [4] from the outboard end of the main flap [1]:
(a) Remove the bolts [3] that attach the upper skin panel [4] to the main flap [1].
(b) Remove the upper skin panel [4].
SUBTASK 27-51-14-010-003
(5) Remove the lower skin panel [58] from the inboard end of the main flap [1]:
(a) Remove the bolts [57] that attach the lower skin panel [58] to the main flap [1].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 401
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(b) Remove the lower skin panel [58].
SUBTASK 27-51-14-010-004
(6) Remove the leading edge panel [40] from the outboard end of the main flap [1]:
(a) Remove the bolts [42] that attach the leading edge panel [40] to the main flap [1].
(b) Remove the leading edge panel [40].
D. Inboard Aft Flap Mechanism Removal
SUBTASK 27-51-14-020-001
(1) Remove the aft flap drive rod assembly [43]:
(a) Remove the nuts [49], washers [48], bushings [47], washers [46] and bolts [45] that attach
the aft flap drive rod assembly [43] to the drive rod fitting [44] and the crankshaft
assembly [17].
(b) Remove the aft flap drive rod assembly [43].
SUBTASK 27-51-14-020-002
(2) Remove the interconnect push rod assembly [18]:
(a) Remove the nut [25], washer [24], washer [22], bolt [21] and bushing [23] that attach the
interconnect push rod assembly [18] to the crankshaft assembly [17].
(b) Remove the nut [15], washer [14], washer [12], bolt [11] and bushing [13] that attach the
interconnect push rod assembly [18] to the outboard bellcrank assembly [33].
(c) Remove the interconnect push rod assembly [18].
SUBTASK 27-51-14-020-003
(3) Remove the crankshaft assembly [17]:
(a) Remove the nut [55], washer [54], washer [52], bolt [51] and bushings [53] that attach the
crankshaft assembly [17] to the ribs [41].
(b) Remove the crankshaft assembly [17].
SUBTASK 27-51-14-020-004
(4) Remove the aft flap push rod assemblies [34]:
(a) Remove the nut [31], washer [30], washer [28], bolt [27] and bushing [29] that attach the
outboard aft flap push rod assembly [34] to the outboard bellcrank assembly [33].
(b) Remove the nut [31], washer [30], bushing [29], washer [28] and bolt [27] that attach the
inboard aft flap push rod assembly [34] to the inboard bellcrank assembly [67].
(c) Remove the nuts [79], washers [78], washers [76], bolts [75] and bushings [77] that attach
the aft flap push rod assemblies [34] to the aft flap [2].
(d) Remove the aft flap push rod assemblies [34].
SUBTASK 27-51-14-020-005
(5) Remove the cable assemblies [19] and cable assemblies [64]:
(a) Remove the locking clips [66] from the turnbuckles [65].
(b) Turn the turnbuckles [65] to loosen the cable assemblies [19] and cable assemblies [64].
(c) Remove the nuts [62], washers [61], washers [60] and bolts [59] that attach the cable
assemblies [64] to the inboard bellcrank assembly [67].
(d) Remove the nuts [38], washers [37], washers [36] and bolts [35] that attach the cable
assemblies [19] to the outboard bellcrank assembly [33].
(e) Remove the cable assemblies [19] and cable assemblies [64].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 402
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-14-020-006
(6) Remove the outboard bellcrank assembly [33]:
(a) Remove the nut [9], washer [8], washer [6], bolt [5] and bushings [7] that attach the
outboard bellcrank assembly [33] to the main flap [1].
(b) Remove the outboard bellcrank assembly [33].
SUBTASK 27-51-14-020-007
(7) Remove the inboard bellcrank assembly [67]:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(109)
