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

(d) Install the pins [50] through the nuts [49].
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-14-410-001
(1) Install the leading edge panel [40] on the outboard end of the main flap [1]:
(a) Apply sealant, A00247 to the mating surface of the leading edge panel [40] and the main
flap [1].
(b) Put the leading edge panel [40] in its position.
(c) Install the bolts [42]:
1) Apply compound, C00528 to the forward and aft rows of holes in the leading edge panel
[40].
2) Install the bolts [42] in the forward and aft rows of holes.
3) Apply sealant, A00247 to the bolts [42] that go in the ribs and stiffeners in the main flap
[1].
4) Install the bolts [42] in the ribs and stiffeners.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 413
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-14-410-002
(2) Install the upper skin panel [4] on the outboard end of the main flap [1]:
(a) Apply sealant, A00247 to the mating surface of the upper skin panel [4] and the main flap
[1].
(b) Put the upper skin panel [4] in its position.
(c) Install the bolts [3]:
1) Apply compound, C00528 to the forward and aft rows of holes in the upper skin panel
[4].
2) Install the bolts [3] in the forward and aft rows of holes.
3) Apply sealant, A00247 to the bolts [3] that go in the ribs and stiffeners in the main flap
[1].
4) Install the bolts [3] in the ribs and stiffeners.
SUBTASK 27-51-14-410-003
(3) Install the lower skin panel [58] on the inboard end of the main flap [1]:
(a) Apply sealant, A00247 to the mating surface of the lower skin panel [58] and the main flap
[1].
(b) Put the lower skin panel [58] in its position.
(c) Install the bolts [57]:
1) Apply compound, C00528 to the forward and aft rows of holes in the lower skin panel
[58].
2) Install the bolts [57] in the forward and aft rows of holes.
3) Apply sealant, A00247 to the bolts [57] that go in the ribs and stiffeners in the main flap
[1].
4) Install the bolts [57] in the ribs and stiffeners.
SUBTASK 27-51-14-410-004
(4) Do this task: Inboard Flap Support Aft Fairing Installation, TASK 27-51-18-400-802.
SUBTASK 27-51-14-440-001
(5) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-14-860-002
(6) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
Flaps, TASK 27-51-00-860-804.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 414
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Aft Flap Pushrod Adjustment
Figure 402 (Sheet 1 of 2)/27-51-14-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 415
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Aft Flap Pushrod Adjustment
Figure 402 (Sheet 2 of 2)/27-51-14-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-14
Page 416
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
INBOARD FLAP TRACKS - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the outboard track for the inboard flap
(2) An installation of the outboard track for the inboard flap
(3) A removal of the inboard track for the inboard flap
(4) An installation of the inboard track for the inboard flap.
TASK 27-51-15-000-801
2. Inboard Flap Outboard Track Removal
(Figure 401)
A. General
(1) This task is applicable to the flap tracks at flap supports No. 3 and 6.
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)
27-51-11-000-801 Inboard Trailing Edge Flap Removal (P/B 401)
27-51-18-000-801 Inboard Flap Support Forward Fairing Removal (P/B 401)
27-51-18-000-802 Inboard Flap Support Aft Fairing Removal (P/B 401)
27-51-31-000-801 Inboard Flap Outboard Transmission Removal (P/B 401)
27-59-02-000-803 Inboard Flap Outboard Skew Mechanism Removal (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
　
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 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊4(113)