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(fèi)者

(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
31 Tube assembly 27-51-58-01-015 GUN ALL
32 Tube assembly 27-51-58-01-020 GUN ALL
33 Tube assembly 27-51-58-03-030 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
550 Subzone - Left Wing: Trailing Edge, Aft of Rear Spar, Inbd of
Outboard Trailing Edge Flap
553 Left Wing - Inboard Flap
650 Subzone - Right Wing: Trailing Edge, Aft of Rear Spar, Inboard of
Outboard Trailing Edge Flap
653 Right Wing - Inboard Flap
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 414
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
G. Inboard Wing Flap Torque Tube Installation
SUBTASK 27-51-58-420-003
(1) Install the tube assembly [31], tube assembly [32] or tube assembly [33]:
(a) Apply grease, D00633 to the coupling sleeves [5].
(b) Put the tube assembly [31], tube assembly [32] or tube assembly [33] in its position.
(c) Put the coupling sleeves [5] on the splined couplings [4].
(d) Install the screws [6] to attach the coupling sleeves [5] to the splined couplings [4].
(e) Install the lockwire on the screws [6].
SUBTASK 27-51-58-080-002
(2) Remove the clamp set, SPL-1726 from the torque tubes.
SUBTASK 27-51-58-420-004
(3) For tube assembly [32] or tube assembly [33], install the applicable torque tube guard [37]:
(a) Put the torque tube guard [37] on the torque tube.
(b) Install the bolts [34], or bolts [38], washers [35] and nuts [36] that attach the torque tube
guard [37].
SUBTASK 27-51-58-820-002
(4) If a torque tube turned while the torque tubes were disconnected, do this task: Trailing Edge
Flap Drive System Adjustment, TASK 27-51-00-820-802.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-58-640-002
(1) For the applicable torque tube, do this task: Trailing Edge Flap Torque Tube and Torque Tube
Support Lubrication, TASK 12-22-51-640-801.
SUBTASK 27-51-58-440-002
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-58-710-004
(3) Use the primary system to retract the flaps, do this task: Trailing Edge Flap System Operation
With Primary Control, TASK 27-51-00-860-801.
(a) Make sure the pointers for the flap position indicators are in the UP white band.
SUBTASK 27-51-58-710-005
(4) Use the primary system to extend the flaps to the 40-unit position, do this task: Trailing Edge
Flap System Operation With Primary Control, TASK 27-51-00-860-801.
(a) Make sure the pointers for the flap position indicators are in the 40-unit white band.
SUBTASK 27-51-58-710-006
(5) Use the primary system to retract the flaps, do this task: Trailing Edge Flap System Operation
With Primary Control, TASK 27-51-00-860-801.
------------------------- END OF TASK ---------------------------
TASK 27-51-58-000-803
6. Wheel Well Flap Torque Tube Removal
(Figure 404)
A. General
(1) This task is applicable to the torque tubes in the wheel well between the Tee angle gearboxes.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 415
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (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
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. 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
　
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 飛機(jī)維護(hù)手冊5 AIRCRAFT MAINTENANCE MANUA(93)