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

E. Prepare for the Removal
SUBTASK 27-51-58-480-005
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR CAN RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed in the nose and main landing gear, do this task: Landing
Gear Downlock Pins Installation, TASK 32-00-01-480-801.
SUBTASK 27-51-58-040-003
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
F. Wheel Well Flap Torque Tube Removal
SUBTASK 27-51-58-480-003
(1) Install the clamp set, SPL-1726 on a torque tube outboard of the applicable torque tube
(Figure 402):
NOTE: The clamp set can be used to stop inadvertent movement of the flap drive system while
the torque tubes are disconnected. If the flap drive system moves, then it will be
necessary to do the flap drive system adjustment.
(a) Put the clamp assembly in its location on the applicable torque tube.
(b) Turn the knob to tighten the clamp assembly on the torque tube.
(c) Turn the rod until it touches the structure to make sure the clamp assembly does not turn.
SUBTASK 27-51-58-020-005
(2) Remove the torque tube guard [52]:
(a) Remove the nuts [55], washers [54] and bolts [53] that attach the torque tube guard [52].
(b) Remove the torque tube guard [52] from the tube assembly [51].
SUBTASK 27-51-58-020-006
(3) Remove the tube assembly [51]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 416
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Remove the screws [6] that attach the coupling sleeves [5] to the splined couplings [4].
(b) Move the coupling sleeves [5] off the splined couplings [4].
(c) Remove the tube assembly [51].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 417
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Wheel Well Flap Torque Tube Installation
Figure 404 (Sheet 1 of 3)/27-51-58-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 418
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Wheel Well Flap Torque Tube Installation
Figure 404 (Sheet 2 of 3)/27-51-58-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 419
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Wheel Well Flap Torque Tube Installation
Figure 404 (Sheet 3 of 3)/27-51-58-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 420
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-58-400-803
7. Wheel Well Flap Torque Tube Installation
(Figure 404)
A. General
(1) This task is applicable to the torque tubes in the wheel well between the Tee angle gearboxes.
B. References
Reference Title
12-22-51-640-801 Trailing Edge Flap Torque Tube and Torque Tube Support
Lubrication (P/B 301)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-820-802 Trailing Edge Flap Drive System Adjustment (P/B 501)
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (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
SPL-1726 Clamp Set - Trailing Edge Flap Torque Tube
(Part #: C27022-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
D00633 Grease - Aircraft General Purpose BMS3-33
E. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
6 Screw 27-51-58-03-010 GUN ALL
51 Tube assembly 27-51-58-03-060 GUN ALL
F. 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
G. Wheel Well Flap Torque Tube Installation
　
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 飛機維護手冊5 AIRCRAFT MAINTENANCE MANUA(94)