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

737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 526
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Fixed Panel Adjustment
Figure 504 (Sheet 4 of 5)/27-51-11-990-807
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 527
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Fixed Panel Adjustment
Figure 504 (Sheet 5 of 5)/27-51-11-990-807
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 528
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Fixed Upper Panel Adjustment
Figure 505 (Sheet 1 of 3)/27-51-11-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 529
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Fixed Upper Panel Adjustment
Figure 505 (Sheet 2 of 3)/27-51-11-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 530
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Fixed Upper Panel Adjustment
Figure 505 (Sheet 3 of 3)/27-51-11-990-809
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 531
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
INBOARD AFT FLAP - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the inboard aft flap
(2) An installation of the inboard aft flap.
B. The aft flap weighs approximately 60 pounds.
TASK 27-51-12-000-801
2. Inboard Aft Flap Removal
(Figure 401)
A. 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)
B. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
C. Prepare for the Removal
SUBTASK 27-51-12-860-003
(1) Extend the trailing edge flaps to the 40-unit position. To extend them, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-51-12-040-001
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
D. Inboard Aft Flap Removal
SUBTASK 27-51-12-020-001
(1) At the outboard flap support, disconnect the crankshaft [3] from the aft flap drive rod [10]:
(a) Remove the nut [8], washer [7], bushing [6], washer [5] and bolt [4] that attach the
crankshaft [3] to the aft flap drive rod [10].
SUBTASK 27-51-12-980-001
(2) Use the crankshaft [3] to manually move the aft flap assembly [2] to the extended position.
SUBTASK 27-51-12-020-002
(3) Disconnect the inboard and outboard aft flap pushrods [11]:
(a) Remove the nuts [18], washers [17], washers [15], bolts [14] and bushings [13] that attach
the aft flap pushrods [11] to the aft flap assembly [2].
(b) Move the aft flap pushrods [11] away from the aft flap assembly [2].
SUBTASK 27-51-12-020-003
(4) Remove the aft flap assembly [2]:
NOTE: The aft flap assembly [2] weighs approximately 60 pounds.
(a) Support the aft flap assembly [2].
(b) Disconnect the aft flap tracks [21] from the aft flap assembly [2]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-12
Page 401
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Remove the nuts [23], washers [24], washers [26], bolts [27] and bushings [25] that
attach the aft flap tracks [21] to the aft flap assembly [2].
2) Move the aft flap tracks [21] forward, away from the aft flap assembly [2].
(c) Move the trailing edge of the aft flap assembly [2] down, until it is perpendicular to the main
flap [1].
(d) Disengage the inboard and outboard rollers [28] from the programming tracks [38].
NOTE: Disengage the inboard roller [28] first.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-12
Page 402
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Aft Flap Installation
Figure 401 (Sheet 1 of 5)/27-51-12-990-801
　
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(97)