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SUBTASK 27-51-58-420-005
(1) Install the tube assembly [51]:
(a) Apply grease, D00633 to the coupling sleeves [5].
(b) Put the tube assembly [51] 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].
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SUBTASK 27-51-58-080-003
(2) Remove the clamp set, SPL-1726 from the torque tubes.
SUBTASK 27-51-58-420-006
(3) Install the torque tube guard [52]:
(a) Put the torque tube guard [52] on the tube assembly [51].
(b) Install the bolts [53], washers [54] and nuts [55] that attach the torque tube guard [52].
SUBTASK 27-51-58-820-003
(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 27-51-58-640-003
(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 27-51-58-440-003
(2) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-58-710-007
(3) 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 27-51-58-710-008
(4) 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.
------------------------- END OF TASK ---------------------------
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FLAP TORQUE TUBE SUPPORT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flap torque tube support
(2) An installation of the flap torque tube support.
TASK 27-51-59-000-801
2. Flap Torque Tube Support Removal
(Figure 401)
A. 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)
B. 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)
C. 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
D. Prepare for the Removal
SUBTASK 27-51-59-860-001
(1) Extend the trailing edge flaps to the 40-unit position. To extend them, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-51-59-040-001
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
E. Flap Torque Tube Support Removal
SUBTASK 27-51-59-020-001
(1) Disconnect the torque tubes [4] from the support assembly [6]:
(a) Install clamp set, SPL-1726 on the torque tubes [4] inboard and outboard of the support
assembly [6].
(b) Remove the screws [5] that attach the coupling sleeves [3] to the splined couplings [1].
(c) Move the coupling sleeves [3] off the splined couplings [1].
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SUBTASK 27-51-59-020-002
(2) Remove the torque tube support assembly [6]:
(a) Remove the nuts [15], washers [14], washers [13] and bolts [12] that attach the support
assembly [6] to the spoiler actuator support [2].
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(95)
