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

ACCIDENTAL OPERATION OF THE LEADING EDGE FLAPS. THE LEADING EDGE
FLAPS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE
TO EQUIPMENT.
(4) Install the lockout set, SPL-1734 on the actuator of the adjacent leading edge flap. To do this, do
this task: Leading Edge Flap and Slat Locks Installation, TASK 27-81-00-480-801.
E. Leading Edge Flap Removal
SUBTASK 27-81-11-020-001
(1) Disconnect the flap actuator [4] from the Leading edge flap [1] or Leading edge flap [2]:
(a) Remove the pin [6], nut [7], washer [8], bushing [11], washer [10] and bolt [9] to disconnect
the flap actuator [4] from the outboard Leading edge flap [2].
(b) Remove the pin [15], nut [16], washer [17], bushing [12], washer [13] and bolt [14] to
disconnect the flap actuator [4] from the inboard Leading edge flap [1].
SUBTASK 27-81-11-020-002
(2) Do these steps to remove the outboard Leading edge flap [2] from the fixed leading edge:
(a) Disconnect the bullnose linkage [53] from the fixed leading edge flap.
1) Remove the pin [55], nut [54], washer [56], anti-rotation washers [41], bushing [44],
washer [43] and bolt [42].
(b) Disconnect hinges 1 thru 4 on the Leading edge flap [2] from the fixed leading edge.
1) At hinges 1 and 4, remove the pins pin [21], nuts [22], washers [20], bushings [19],
washers [24], and bolts [23].
2) At hinges 2 and 3, remove the pin [34], nuts [33], washers [25], bushings [26], washers
[28], and bolts [27].
(c) Remove the nut [32], washers [31], and bolt [30] to disconnect the bonding jumper [29] from
the fixed leading edge.
(d) Remove the Leading edge flap [2] from the wing.
SUBTASK 27-81-11-020-003
(3) Do these steps to remove the inboard Leading edge flap [1] from the fixed leading edge:
(a) Disconnect the bullnose linkages [53] from the fixed leading edge flap.
1) Remove the pin [55], nuts [54], washers [56], anti-rotation washers [41], bushings [44],
washers [43] and bolts [42].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 402
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(b) Disconnect hinges 5 thru 8 on the Leading edge flap [1] from the fixed leading edge flap.
1) At hinge 5, remove the pin [21], nut [22], washer [20], bushing [19], washer [24], and bolt
[23].
2) At hinges 6 and 7, remove the pin [34], nuts [33], washers [25], bushings [26], washers
[28], and bolts [27].
3) At hinge 8, remove the pin [40], nut [39], washer [35], bushing [38], washer [36], and bolt
[37].
(c) Remove the nut [32], washers [31], and bolt [30] to disconnect the bonding jumper [29] from
the Leading edge flap [1].
(d) Remove the Leading edge flap [1] from the wing.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 403
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 1 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 404
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 2 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 405
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 3 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 406
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 4 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 407
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 5 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 408
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 6 of 10)/27-81-11-990-801
737-600/700/800/900
　
中國航空網 m.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7 AIRCRAFT MAINTENANCE MANUA(62)