曝光臺 注意防騙 網(wǎng)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 27-51-15
Page 415
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-15-400-802
5. Inboard Flap Inboard Track Installation
(Figure 402)
A. General
(1) This task is applicable to the flap tracks at flap supports No. 4 and 5.
B. References
Reference Title
12-22-51-640-813 Inboard Flap Inboard Flap Track Lubrication (P/B 301)
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)
27-51-11-400-801 Inboard Trailing Edge Flap Installation (P/B 401)
27-51-11-820-801 Inboard Trailing Edge Flap Adjustment (P/B 501)
27-51-31-400-802 Inboard Flap Inboard Transmission Installation (P/B 401)
27-59-00-820-801 Flap Skew Detection System Adjustment (P/B 501)
27-59-02-400-804 Inboard Flap Inboard Skew Mechanism Installation (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
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1568 Jack - Hydraulic, General Low Profile
(Part #: B67563, Supplier: 36251, A/P Effectivity: 737-ALL)
(Part #: HW93718, Supplier: 28047, A/P Effectivity: 737-ALL)
(Opt Part #: W93718, Supplier: 36251, A/P Effectivity: 737-ALL)
SPL-1733 Adapter - Hoist, Removal/Installation, Flap Track
(Part #: C27040-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
41 Track assembly 27-51-00-08-165 GUN 001-020, 101-110,
155-157, 201-999
27-51-00-08-170 GUN 001-020, 101-110,
155-157, 201-999
44 Pin 27-51-00-08-130 GUN 001-020, 101-110,
155-157, 201-999
45 Link assembly 27-51-00-08-235 GUN 001-020, 101-110,
155-157, 201-999
53 Fitting Not Specified
57 Pin 27-51-00-08-050 GUN 001-020, 101-110,
155-157, 201-999
59 Pin 27-51-00-08-045 GUN 001-020, 101-110,
155-157, 201-999
63 Pin 27-51-00-08-260 GUN 001-020, 101-110,
155-157, 201-999
66 Pin 27-51-00-08-195 GUN 001-020, 101-110,
155-157, 201-999
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-15
Page 416
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
E. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
541 Left Wing - Fairing Flap Support No. 4
641 Right Wing - Fairing Flap Support No. 5
F. Inboard Flap Inboard Track Installation
SUBTASK 27-51-15-420-007
(1) If they are not installed, install the transmission attach fitting [53] and link assembly [45] on the
flap track assemblies [41]:
(a) Install the transmission attach fitting [53]:
1) Put the transmission attach fitting [53] in its position on the flap track assemblies [41].
2) Install the bolt [60], bolts [64], washers [61] and nuts [62] that attach the transmission
attach fitting [53] to the flap track assemblies [41].
3) Install the pins [63] in the nuts [62].
(b) Install the link assembly [45] on the flap track assemblies [41]:
1) Put the link assembly [45] in its position on the flap track assemblies [41].
2) Install the bolt [72], washer [69], washer [70] and nut [71] to attach the link assembly [45]
to the flap track assemblies [41].
3) Tighten the nut [71] to 290-510 pound-inches (32.8-57.6 newton-meters).
4) Install lockwire between the nut [70] and the washer [71].
5) Install the bolt [68], washer [65] and nut [67] in the bolt [72].
6) Tighten the nut [67] to 30-60 pound-inches (3.4-6.7 newton-meters).
7) Install the pin [66] in the nut [67].
SUBTASK 27-51-15-480-006
(2) If you will use the adapter, SPL-1733, install it on the flap track assemblies [41]:
(a) Install the adapter, SPL-1733 on the flap track assemblies [41] approximately 20 inches (50
cm) aft of the track forward attach fitting.
(b) Put a low profile hydraulic jack, COM-1568 below the adapter, SPL-1733 to support the flap
track assemblies [41].
SUBTASK 27-51-15-420-008
(3) Connect the forward end of the flap track assemblies [41]:
(a) Put the flap track assemblies [41] in its position on the forward attach assembly [50].
(b) Install the bolt [51], washer [54] and nut [58] that attach the flap track assemblies [41] to the
　
中國航空網(wǎng) 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(hù)手冊4(118)