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(b) Remove the nuts [11], washers [10], washers [8], bolts [7] and bushings [9] that attach the
support assembly [6] to the spoiler actuator support [2].
(c) Remove the support assembly [6].
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Flap Torque Tube Support Installation
Figure 401 (Sheet 1 of 2)/27-51-59-990-801
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Flap Torque Tube Support Installation
Figure 401 (Sheet 2 of 2)/27-51-59-990-801
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TASK 27-51-59-400-801
3. Flap Torque Tube Support Installation
(Figure 401)
A. 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)
27-51-00-860-804 Retract 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. 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
6 Support assembly 27-51-59-01-040 GUN ALL
27-51-59-01-045 GUN ALL
E. 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
F. Flap Torque Tube Support Installation
SUBTASK 27-51-59-420-001
(1) Install the torque tube support assembly [6]:
(a) Put the support assembly [6] in its position on the spoiler actuator support [2].
(b) Apply compound, C00913 to the shank and threads of the bolts [7] and bolts [12].
(c) Install the bolts [12], washers [13], washers [14] and nuts [15] to attach the outboard side of
the support assembly [6] to the spoiler actuator support [2].
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(d) Install the bushings [9], bolts [7], washers [8], washers [10] and nuts [11] to attach the
inboard side of the support assembly [6] to the spoiler actuator support [2].
SUBTASK 27-51-59-420-002
(2) Connect the torque tubes [4] to the support assembly [6]:
(a) Apply grease, D00633 to the coupling sleeves [3].
(b) Put the splined couplings [1] in the coupling sleeves [3].
(c) Install the screws [5] to attach the torque tubes [4] to the support assembly [6].
(d) Install lockwire on the screws [5].
(e) Remove the clamp set, SPL-1726 from the torque tubes [4] inboard and outboard of the
support assembly [6].
SUBTASK 27-51-59-820-001
(3) If the torque tubes [4] turned while they were disconnected, do this task: Trailing Edge Flap
Drive System Adjustment, TASK 27-51-00-820-802.
SUBTASK 27-51-59-640-001
(4) Lubricate the torque tubes [4] and the support assembly [6]. To lubricate the torque tube support
[4], do this task: Trailing Edge Flap Torque Tube and Torque Tube Support Lubrication,
TASK 12-22-51-640-801.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-59-440-001
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
SUBTASK 27-51-59-860-002
(2) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(96)
