曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Page 403
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-16-400-801
3. Inboard Aft Flap Track Installation
(Figure 401)
A. References
Reference Title
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-12-400-801 Inboard Aft Flap Installation (P/B 401)
27-51-18-400-802 Inboard Flap Support Aft Fairing Installation (P/B 401)
B. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
2 Track 27-51-16-01-070 GUN 001-028, 101-121,
155-157, 201-999
3 Cartridge assembly 27-51-15-02-030 GUN 001-028, 101-121,
155-157, 201-999
4 Nut 27-51-15-02-020 GUN 001-028, 101-121,
155-157, 201-999
5 Cartridge assembly 27-51-15-02-025 GUN 001-028, 101-121,
155-157, 201-999
7 Washer 27-51-16-01-035 GUN 001-028, 101-121,
155-157, 201-999
8 Nut 27-51-16-01-040 GUN 001-028, 101-121,
155-157, 201-999
9 Bushing 27-51-16-01-045 GUN 001-028, 101-121,
155-157, 201-999
10 Washer 27-51-16-01-030 GUN 001-028, 101-121,
155-157, 201-999
11 Bolt 27-51-16-01-025 GUN 001-028, 101-121,
155-157, 201-999
D. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
E. Inboard Aft Flap Track Installation
SUBTASK 27-51-16-420-001
(1) If the downstop is not installed on the aft flap track [2], do these steps:
(a) Install the bolt [11], bushings [9], washer [10], washer [7] and nut [8] on the aft flap track [2].
(b) Tighten the nut [8] to 50-75 pound-inches (5.7-8.4 newton-meters).
SUBTASK 27-51-16-420-002
(2) Install the aft flap track [2] in the main flap [1]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-16
Page 404
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Carefully put the aft flap track [2] in its position in the aft flap track support [6] in the main
flap [1].
NOTE: Make sure the downstop is forward of the forward cartridge assemblies [5].
(b) Apply a layer of sealant, A00247 to the mating surface of the cartridge assemblies [3] and
cartridge assemblies [5] and the aft flap track support [6].
(c) Put the cartridge assemblies [3] and cartridge assemblies [5] in their position in the aft flap
track support [6].
(d) Install the nuts [4] that attach the cartridge assemblies [3] and cartridge assemblies [5] to
the aft flap track support [6].
SUBTASK 27-51-16-420-003
(3) Do this task: Inboard Aft Flap Installation, TASK 27-51-12-400-801.
NOTE: It is necessary to do the aft flap adjustment after you install the aft flap.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-16-410-001
(1) Do this task: Inboard Flap Support Aft Fairing Installation, TASK 27-51-18-400-802.
SUBTASK 27-51-16-440-001
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-16-860-002
(3) Retract the trailing edge flaps to the retracted position. To retract the flaps, 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 27-51-16
Page 405
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
INBOARD FLAP SUPPORT FAIRING - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the forward fairing for the outboard flap support on the inboard flap.
(2) An installation of the forward fairing for the outboard flap support on the inboard flap.
(3) A removal of the aft fairing for the outboard flap support on the inboard flap.
(4) An installation of the aft fairing for the outboard flap support on the inboard flap.
TASK 27-51-18-000-801
2. Inboard Flap Support Forward Fairing Removal
(Figure 401)
A. General
(1) This task is applicable to the forward fairing on the No. 3 and No. 6 flap supports.
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
C. Location Zones
Zone Area
542 Left Wing - Fairing Flap Support No. 3
642 Right Wing - Fairing Flap Support No. 6
D. Procedure
SUBTASK 27-51-18-040-001
(1) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
　
中國(guó)航空網(wǎng) m.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(jī)維護(hù)手冊(cè)4(122)