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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
1 Tube assembly 27-51-58-01-010 GUN ALL
2 Tube assembly 27-51-58-01-005 GUN ALL
3 Tube assembly 27-51-58-10-015 GUN ALL
6 Screw 27-51-58-03-010 GUN ALL
F. Location Zones
Zone Area
561 Left Wing - Rear Spar to Trailing Edge, Outboard Of Inboard Flap,
Inboard of Fixed Trailing Edge
567 Left Wing - Outboard Flap
661 Right Wing - Rear Spar to Trailing Edge, Outboard of Inboard Flap,
Inboard of Fixed Trailing Edge
667 Right Wing - Outboard Flap
G. Outboard Wing Flap Torque Tube Installation
SUBTASK 27-51-58-420-001
(1) Install the tube assembly [1], tube assembly [2] or tube assembly [3]:
(a) Apply grease, D00633 to the coupling sleeves [5].
(b) Put the tube assembly [1], tube assembly [2] or tube assembly [3] in its position.
(c) Put the coupling sleeves [5] on the splined couplings [4].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 407
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(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 27-51-58-080-001
(2) Remove the clamp set, SPL-1726 from the torque tubes.
SUBTASK 27-51-58-420-002
(3) Install the applicable torque tube guard [10]:
(a) Put the torque tube guard [10] on the torque tube.
(b) Install the bolts [7], bolts [11], or bolts [12], washers [8] and nuts [9] that attach the torque
tube guard [10].
SUBTASK 27-51-58-820-001
(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 27-51-58-640-001
(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 27-51-58-440-001
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-58-710-001
(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 27-51-58-710-002
(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 27-51-58-710-003
(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 27-51-58-000-802
4. Inboard Wing Flap Torque Tube Removal
(Figure 403)
A. General
(1) This task is applicable to the torque tubes inboard of the seal rib angle gearbox and outboard of
the Tee 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)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-58
Page 408
Oct 10/2007
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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
550 Subzone - Left Wing: Trailing Edge, Aft of Rear Spar, Inbd of
　
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