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

2) Install the bolt [7], washer [6], washer [4] and nut [3] that attach the inboard end of the
flap track assembly [1].
3) Install the bolt [8], washer [9], washer [10] and nut [11] that attach the outboard end of
the flap track assembly [1].
(c) Attach the forward end of the flap track assembly [1]:
1) Apply grease, D00633 to the outside of the fuse pin [15] and the inside of the bushings.
2) Install the fuse pin [15] to attach the forward end of the flap track assembly [1] to the
track attach fitting.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-15
Page 408
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(d) Tighten the nut [3] to 1000-1470 pound-inches (113-166 newton-meters).
(e) Tighten the nut [11] to 630-1070 pound-inches (71.2-120.8 newton-meters).
(f) Make sure you can turn the fuse pin [15] in the joint with a maximum of 10 pound-inches
torque.
NOTE: You can push up on the forward end of the flap track assembly [1] to take the
weight off the fuse pin [15] when you measure the torque.
(g) Install the washer [16] and nut [17] on the fuse pin [15].
(h) Tighten the nut [17] to 330-350 pound-inches.
(i) Loosen the nut [17] to align the hole for the pin [18].
(j) Install the pin [18] in the nut [17].
SUBTASK 27-51-15-420-003
(4) Install the failsafe fitting assembly [14] on the track attach fitting:
(a) Put the failsafe fitting assembly [14] in its location on the track attach fitting.
(b) Install the bolts [13] and washers [12] to attach the failsafe fitting assembly [14].
SUBTASK 27-51-15-480-004
(5) If it is necessary, remove the adapter, SPL-1733 from the flap track assembly [1].
SUBTASK 27-51-15-420-004
(6) Do this task: Inboard Flap Outboard Transmission Installation, TASK 27-51-31-400-801.
SUBTASK 27-51-15-420-005
(7) Do this task: Inboard Flap Outboard Skew Mechanism Installation, TASK 27-59-02-400-803.
SUBTASK 27-51-15-420-006
(8) Do this task: Inboard Trailing Edge Flap Installation, TASK 27-51-11-400-801.
SUBTASK 27-51-15-820-001
(9) Do this task: Inboard Trailing Edge Flap Adjustment, TASK 27-51-11-820-801.
SUBTASK 27-51-15-820-002
(10) Do this task: Flap Skew Detection System Adjustment, TASK 27-59-00-820-801.
SUBTASK 27-51-15-640-001
(11) Do this task: Inboard Flap Outboard Flap Track Lubrication, TASK 12-22-51-640-814.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-15-410-001
(1) Install the fairings for the outboard track on the inboard flap:
(a) Do this task: Inboard Flap Support Aft Fairing Installation, TASK 27-51-18-400-802.
(b) Do this task: Inboard Flap Support Forward Fairing Installation, TASK 27-51-18-400-801.
SUBTASK 27-51-15-440-001
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-15-860-002
(3) 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 27-51-15
Page 409
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-15-000-802
4. Inboard Flap Inboard Track Removal
(Figure 402)
A. General
(1) This task is applicable to the flap tracks at flap supports No. 4 and 5.
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)
27-51-31-000-802 Inboard Flap Inboard Transmission Removal (P/B 401)
27-59-02-000-804 Inboard Flap Inboard Skew Mechanism Removal (P/B 201)
32-00-01-480-801 Landing Gear Downlock Pins 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)
　
中國(guó)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(jī)維護(hù)手冊(cè)4(116)