曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

------------------------- END OF TASK ---------------------------
TASK 27-59-02-000-803
6. Inboard Flap Outboard Skew Mechanism Removal
(Figure 203)
A. General
(1) This task is applicable to the flap skew mechanisms installed on flap supports No. 3 and 6.
(2) You can remove the flap skew mechanism with the flap skew sensor [83] either removed or
installed. This task shows the removal with the flap skew sensor [83] installed.
B. 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)
C. Location Zones
Zone Area
542 Left Wing - Fairing Flap Support No. 3
642 Right Wing - Fairing Flap Support No. 6
D. Procedure
SUBTASK 27-59-02-860-011
(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 27-59-02-040-003
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-59-02-860-012
(3) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 11 C01443 FC TE FLAP POS/SKEW SNSR & IND RIGHT
A 12 C00213 FC TE FLAP POS/SKEW SNSR & IND LEFT
SUBTASK 27-59-02-020-007
(4) Disconnect the electrical connector [82] from the flap skew sensor [83].
SUBTASK 27-59-02-020-008
(5) Remove the nuts [97], washers [96], bushings [95], washers [94] and bolts [93] that attach the
control rod [92] to the crank arm [98] and to the carriage [91].
SUBTASK 27-59-02-020-009
(6) Remove the sensor input assembly [81]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-02
Page 213
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Remove the nut [89], washer [88], washer [87], washer [86] and bolt [85] that attach the
sensor input assembly [81] and the jumper wire [84] to the flap track [90].
(b) Remove the nuts [102], washers [101], washers [100] and bolts [99] that attach the sensor
input assembly [81] to the flap track [90].
(c) Remove the sensor input assembly [81] from the flap track [90].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-02
Page 214
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Flap Outboard Skew Mechanism Installation
Figure 203 (Sheet 1 of 2)/27-59-02-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-02
Page 215
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Flap Outboard Skew Mechanism Installation
Figure 203 (Sheet 2 of 2)/27-59-02-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-59-02
Page 216
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-59-02-400-803
7. Inboard Flap Outboard Skew Mechanism Installation
(Figure 203)
A. General
(1) This task is applicable to the flap skew mechanisms installed on flap supports No. 3 and 6.
B. References
Reference Title
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-59-00-730-801 Flap Skew Detection System Functional Test (P/B 501)
27-59-00-820-801 Flap Skew Detection System Adjustment (P/B 501)
27-59-01-400-803 Inboard Flap Outboard Skew Sensor Installation (P/B 201)
SWPM 20-60-03 Standard Wiring Practices Manual
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
A02315 Sealant - Low Density, Synthetic Rubber. 2 Part BMS5-142
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
81 Input assembly 27-59-00-02-060 GUN ALL
27-59-00-02-065 GUN ALL
E. Location Zones
Zone Area
542 Left Wing - Fairing Flap Support No. 3
642 Right Wing - Fairing Flap Support No. 6
F. Procedure
SUBTASK 27-59-02-860-013
(1) Make sure that these circuit breakers are open:
F/O Electrical System Panel, P6-2
Row Col Number Name
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 飛機維護手冊5 AIRCRAFT MAINTENANCE MANUA(139)