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时间:2010-08-25 15:35来源:蓝天飞行翻译 作者:admin
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assembly [71]:
(a) Remove the bolts [101] that attach the leading edge skin panel [100].
(b) Remove the leading edge skin panel [100] from the main flap [2].
SUBTASK 27-51-23-020-012
(5) Remove the nut [75], washer [74], washer [73] and bolt [72] that attach the failsafe link [83] to the
carriage assembly [71].
(a) Move the failsafe link [83] away from the carriage assembly [71].
SUBTASK 27-51-23-020-013
(6) Remove the carriage assembly [71] from the main flap [2]:
(a) Remove the nut [120], washer [119], bushing [118], washer [117] and bolt [116] that attach
the aft link assembly [103] to the aft link fitting assembly [115].
(b) Remove the nut [104] and washer [105] that attach the aft link assembly [103] to the main
flap [2].
(c) Remove the aft link assembly [103] from the aft link fitting [116] and the main flap [2].
(d) Remove the nut [97] and washer [98] that attach the forward end of the carriage
assembly [71] to the main flap [2].
(e) Move the carriage assembly [71] forward, away from the main flap [2].
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SUBTASK 27-51-23-020-014
(7) If it is necessary, remove the nut [107], washer [108] and washer [109] that attach the failsafe
link [83] to the main flap [2].
SUBTASK 27-51-23-020-015
(8) If it is necessary, remove the aft link fitting assembly [115] from the carriage assembly [71]:
(a) Remove the nuts [113], washers [112] and bolts [111] that attach the aft link fitting
assembly [115] to the carriage assembly [71].
(b) Measure and record the thickness of the shims [114].
------------------------- END OF TASK ---------------------------
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Outboard Flap Inboard Carriage Installation
Figure 402 (Sheet 1 of 4)/27-51-23-990-802
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Outboard Flap Inboard Carriage Installation
Figure 402 (Sheet 2 of 4)/27-51-23-990-802
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Outboard Flap Inboard Carriage Installation
Figure 402 (Sheet 3 of 4)/27-51-23-990-802
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Outboard Flap Inboard Carriage Installation
Figure 402 (Sheet 4 of 4)/27-51-23-990-802
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TASK 27-51-23-400-802
5. Outboard Flap Inboard Carriage Installation
(Figure 402)
A. General
(1) This task is applicable to the flap carriages at flap supports No. 2 and 7.
B. References
Reference Title
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-21-400-801 Outboard Trailing Edge Flap Installation (P/B 401)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
C00528 Compound - Corrosion Preventive, Petroleum Hot
Application (Soft Film)
MIL-C-11796,
Class III
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00633 Grease - Aircraft General Purpose BMS3-33
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
71 Carriage assembly Not Specified
76 Pin Not Specified
82 Pin Not Specified
83 Link Not Specified
85 Bellcrank assembly Not Specified
86 Rubcap Not Specified
93 Pin Not Specified
99 Pin Not Specified
103 Link assembly Not Specified
106 Pin Not Specified
110 Pin Not Specified
115 Fitting assembly Not Specified
121 Pin Not Specified
E. Location Zones
Zone Area
543 Left Wing - Fairing Flap Support No. 2
567 Left Wing - Outboard Flap
643 Right Wing - Fairing Flap Support No. 7
 
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