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-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00633 Grease - Aircraft General Purpose BMS3-33
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
5 Gear assembly 27-51-57-01-010 GUN ALL
E. Location Zones
Zone Area
561 Left Wing - Rear Spar to Trailing Edge, Outboard Of Inboard Flap,
Inboard of Fixed Trailing Edge
661 Right Wing - Rear Spar to Trailing Edge, Outboard of Inboard Flap,
Inboard of Fixed Trailing Edge
F. Access Panels
Number Name/Location
561AB Midspan Fixed Trailing Edge Access Panel - WBL 224
661AB Midspan Fixed T.E. Panel
G. Seal Rib Angle Gearbox Installation
SUBTASK 27-51-57-420-001
(1) Install the seal rib angle gear assembly [5]:
(a) Put the seal rib angle gear assembly [5] in its position on the rib [10].
(b) Apply compound, C00913 to the shank and threads of the bolts [6].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-57
Page 404
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(c) Install the bolts [6], washers [7], washers [8] and nuts [9] to attach the seal rib angle gear
assembly [5] to the rib [10].
SUBTASK 27-51-57-420-002
(2) Connect the torque tubes [3] to the seal rib angle gear assembly [5]:
(a) Apply grease, D00633 to the coupling sleeves [1].
(b) Put the splined couplings [3] in the coupling sleeves [1].
(c) Install the screws [4] to attach the torque tubes [3] to the seal rib angle gear assembly [5].
(d) Install lockwire on the screws [4].
(e) Remove the clamp set, SPL-1726 from the torque tube [3] outboard of the seal rib angle
gear assembly [5].
SUBTASK 27-51-57-820-001
(3) If the torque tubes [3] moved, while they were disconnected, do this task: Trailing Edge Flap
Drive System Adjustment, TASK 27-51-00-820-802.
SUBTASK 27-51-57-640-001
(4) Lubricate the torque tubes [3]. To lubricate the torque tube, do this task: Trailing Edge Flap
Torque Tube and Torque Tube Support Lubrication, TASK 12-22-51-640-801.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-57-440-001
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-57-710-001
(2) 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 27-51-57-710-002
(3) Use the primary system to retract the flaps to the UP 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 UP white band.
SUBTASK 27-51-57-410-001
(4) Below the seal rib seal rib angle gear assembly [5], do this task:
Install this access panel:
Number Name/Location
561AB Midspan Fixed Trailing Edge Access Panel - WBL
224
or close this access panel:
Number Name/Location
661AB Midspan Fixed T.E. Panel
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-57
Page 405
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLAP TORQUE TUBES - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the outboard wing flap torque tubes
(2) An installation of the outboard wing flap torque tubes
(3) A removal of the inboard wing flap torque tubes
(4) An installation of the inboard wing flap torque tubes
(5) A removal of the flap torque tubes in the wheel well area
(6) An installation of the flap torque tubes in the wheel well area.
TASK 27-51-58-000-801
2. Outboard Wing Flap Torque Tube Removal
(Figure 401)
A. General
(1) This task is applicable to the torque tubes outboard of the seal rib angle gearbox.
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)
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.
　
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