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
Open this access panel:
Number Name/Location
112A Forward Access Door
(b) Disconnect the electrical connector [28] from below.
(c) Remove the screws [29] and washers [30] that attach the electrical connector [18].
(d) Remove the electrcial connector [18] from the control stand [13].
SUBTASK 27-51-08-020-002
(2) Remove the flap lever position switches [24] as an assembly:
(a) Remove the screws [22], screw [27] and washers [23] that attach the flap lever position
switches [24] and the clamp [21] to the control stand [13].
(b) Remove the screw [25], washer [26] and clamp [21].
(c) Remove the screws [19], washers [20] and clamps [21] that attach the wires to the control
stand [13].
SUBTASK 27-51-08-020-003
(3) Remove a flap lever position switch [24] independently:
(a) For the 30-unit flap lever position switch [24], remove the screws [22] and washers [23] that
attach the flap lever position switch [24] to the control stand [13].
1) Remove the screw [25], washer [26] and clamp [21].
(b) For the UP flap lever position switch [24], remove the screw [22], screw [27] and washers
[23] that attach the flap lever position switch [24] and the clamp [21] to the control stand
[13].
(c) Remove the screws [19] and washers [20] from a sufficient number of clamps [21] to get
access to cut the wires.
(d) Cut the wires for the applicable flap lever position switch [24].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 402
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Lever Position Switch Installation
Figure 401 (Sheet 1 of 5)/27-51-08-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 403
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Lever Position Switch Installation
Figure 401 (Sheet 2 of 5)/27-51-08-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 404
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Lever Position Switch Installation
Figure 401 (Sheet 3 of 5)/27-51-08-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 405
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Lever Position Switch Installation
Figure 401 (Sheet 4 of 5)/27-51-08-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 406
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flap Lever Position Switch Installation
Figure 401 (Sheet 5 of 5)/27-51-08-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 407
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-08-400-801
3. Flap Lever Position Switch Installation
(Figure 401)
A. References
Reference Title
27-51-00-740-803 Trailing Edge Flap Load Relief System BITE Test (P/B 501)
27-51-08-820-801 Flap Lever Position Switch Adjustment (P/B 501)
27-81-00-730-801 Leading Edge Cruise Depressurization Test (P/B 501)
SWPM 20-10-11 Standard Wiring Practices Manual
B. Location Zones
Zone Area
212 Flight Compartment - Right
C. Access Panels
Number Name/Location
112A Forward Access Door
D. Flap Lever Position Switch Installation
SUBTASK 27-51-08-860-002
(1) Make sure that these circuit breakers are open and have safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
F/O Electrical System Panel, P6-3
Row Col Number Name
C 10 C00284 PANEL & INSTR ELEX PANEL
SUBTASK 27-51-08-420-001
(2) Install the flap lever position switches [24] as an assembly:
(a) Put the flap lever position switches [24] with the wires and electrical connector [18], in their
position in the control stand [13].
(b) Install the screws [22], screw [27] and washers [23] that attach the flap lever position
switches [24] and the clamp [21] to the control stand [13].
(c) Install the screw [25], washers [26] and clamps [21] that attach the wires to the control
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(79)
