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
stand [13].
(d) Install the screws [19], washers [20] and clamps [21] that attach the wires to the control
stand [13].
SUBTASK 27-51-08-420-002
(3) Install a flap lever position switch [24] independently:
(a) Splice the wires from the new flap lever position switch [24] with the wires in the control
stand [13] (SWPM 20-10-11).
(b) For the 30-unit flap lever position switch [24], install the screws [22] and washers [23] that
attach the flap lever position switch [24] to the control stand [13].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 408
Feb 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Install the screw [25], washers [26] and clamps [21] that attach the wires to the control
stand [13].
(c) For the UP flap lever position switch [24], install 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].
(d) Install the applicable screws [19], washers [20] and clamps [21] that attach the wires to the
control stand [13].
SUBTASK 27-51-08-820-001
(4) Do this task: Flap Lever Position Switch Adjustment, TASK 27-51-08-820-801.
SUBTASK 27-51-08-420-003
(5) Connect the electrical connector [18]:
(a) Put the electrical connector [18] in its position.
(b) Install the screws [29] and washers [30] to attach the electrical connector [18].
(c) Connect the electrical connector [28] from below the control stand [13].
(d) Close this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-51-08-860-003
(6) Remove the safety tags and close these circuit breakers:
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
SUBTASK 27-51-08-740-001
(7) Do this task: Trailing Edge Flap Load Relief System BITE Test, TASK 27-51-00-740-803.
SUBTASK 27-51-08-730-001
(8) Do this task: Leading Edge Cruise Depressurization Test, TASK 27-81-00-730-801.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-08-410-001
(1) Install the control stand cover [1] on the control stand [13] with the screws [2] and the bolt [5].
SUBTASK 27-51-08-010-005
(2) Install the stabilizer trim lightplate [3] on the control stand [13]:
(a) Connect the wires [14] to the stabilizer trim lightplate [3]:
1) Put the wires [14] for in their position on the stabilizer trim lightplate [3].
2) Install the washers [15], washers [16] and nuts [17] to attach the wires [14].
(b) Put the stabilizer trim lightplate [3] in its location on the control stand [13].
(c) Loosely install the screws [4].
(d) Adjust the position of the stabilizer trim lightplate [3] to align with the stabilizer trim
indicator.
(e) Tighten the screws [4].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 409
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-08-410-002
(3) Install the upper side cover [7] and the lower side cover [11] on the right side of the control stand
[13]:
(a) Put the upper side cover [7] and the lower side cover [17] in their position on the control
stand [13].
NOTE: The lower side cover [11] goes under the upper side cover [7].
(b) Install the screws [6] that attach the upper side cover [7] and lower side cover [11] to the
control stand [13].
(c) Install the pocket assembly [12] with the screws [10] on the lower side cover [11].
SUBTASK 27-51-08-410-003
(4) Install the stabilizer trim wheel [8] on the right side of the control stand [13]:
(a) Put the stabilizer trim wheel [8] on the shaft.
NOTE: Make sure the handle on the stabilizer trim wheel is 75 to 105 degrees from the
handle on the left stabilizer trim wheel.
(b) Install the bolt [8] to attach the stabilizer trim wheel [9].
SUBTASK 27-51-08-860-007
(5) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-3
Row Col Number Name
C 10 C00284 PANEL & INSTR ELEX PANEL
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-08
Page 410
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLAP LEVER POSITION SWITCHES - ADJUSTMENT/TEST
1. General
A. This procedure has an adjustment of the flap lever position switches.
B. The flap lever position switches are installed on the control stand and operate with the flap 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(80)
