曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

NOTE: It is not necessary to disconnect the wires for the flap limit switches [39].
(a) Remove the screws [40] and washers [56] and the switch cover [31] from the flap control
unit assembly [9].
(b) For the Flap UP limit switch, S245, Flap Up limit switch, S1051 and the Flap DOWN limit
switch, S246, do this task: Flap Limit Switch Removal, TASK 27-51-63-000-801.
(c) For the Landing Warning Switch, S138, do this task: Flap Landing Warning Switch
Removal, TASK 31-51-01-000-801.
SUBTASK 27-51-61-020-004
(4) Disconnect the cables [48], WFFA and WFFB at the turnbuckles [50]:
NOTE: It is necessary to remove the cables [49] with the flap control unit assembly [9].
(a) Remove the locking clips [49] and disconnect the turnbuckles [50] on the cables [48].
(b) Put a label on the cables [48] to identify them.
SUBTASK 27-51-61-020-005
(5) Disconnect the electrical connector [33] from the trailing edge flap control valve [34].
SUBTASK 27-51-61-020-006
(6) Disconnect the hydraulic lines [32]:
(a) Disconnect the hydraulic lines [32] from the trailing edge flap control valve [34].
(b) Disconnect the hydraulic lines [32] from the leading edge control valve [35].
SUBTASK 27-51-61-020-007
(7) Remove the flap control unit assembly [9]:
(a) Remove the bolts [15] and washers [14] from above the flap control unit assembly [9]
(Figure 401).
(b) Remove the bolts [41] and washers [42] from below the flap control unit assembly [9]
(Figure 402).
(c) Remove the flap control unit assembly [9].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 403
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Quadrant Installation
Figure 401 (Sheet 1 of 4)/27-51-61-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 404
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Quadrant Installation
Figure 401 (Sheet 2 of 4)/27-51-61-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 405
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Quadrant Installation
Figure 401 (Sheet 3 of 4)/27-51-61-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 406
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Quadrant Installation
Figure 401 (Sheet 4 of 4)/27-51-61-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 407
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Installation
Figure 402 (Sheet 1 of 4)/27-51-61-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 408
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Installation
Figure 402 (Sheet 2 of 4)/27-51-61-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 409
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Installation
Figure 402 (Sheet 3 of 4)/27-51-61-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 410
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Control Unit Installation
Figure 402 (Sheet 4 of 4)/27-51-61-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-61
Page 411
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-61-400-801
3. Flap Control Unit Installation
A. References
Reference Title
27-51-00-730-801 Trailing Edge Flap System Test (P/B 501)
27-51-00-820-801 Trailing Edge Flap Control System Adjustment (P/B 501)
27-51-63-400-801 Flap Limit Switch Installation (P/B 401)
27-51-63-820-801 Flaps Limit Switch Adjustment (P/B 501)
31-51-01-400-801 Flap Landing Warning Switch Installation (P/B 401)
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 飛機(jī)維護(hù)手冊5 AIRCRAFT MAINTENANCE MANUA(98)