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SUBTASK 27-51-65-080-003
(1) Remove the rig pin, STD-4592 [14] from the cam follower arm [13] and the valve cam [12].
SUBTASK 27-51-65-410-002
(2) Install the lower pan [10] on the flap control unit [1]:
(a) Put the lower pan [10] in its location on the flap control unit [1].
(b) Apply compound, C00913 to the shank and threads of the screws [11].
(c) Install the washers [21] and screws [11] to attach the lower pan [10] to the flap control unit
[1].
------------------------- END OF TASK ---------------------------
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Trailing Edge Flap Control Valve Adjustment
Figure 501 (Sheet 1 of 4)/27-51-65-990-802
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Trailing Edge Flap Control Valve Adjustment
Figure 501 (Sheet 2 of 4)/27-51-65-990-802
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Trailing Edge Flap Control Valve Adjustment
Figure 501 (Sheet 3 of 4)/27-51-65-990-802
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Trailing Edge Flap Control Valve Adjustment
Figure 501 (Sheet 4 of 4)/27-51-65-990-802
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TRAILING EDGE FLAP CONTROL VALVE - REPAIRS
1. General
A. This procedure includes a repair of the trailing edge flap control valve.
B. You can use this procedure if there is too much internal leakage in the control valve. This procedure
can reduce the internal leakage by approximately one-half. It is not necessary to remove the control
valve from the airplane to do this procedure.
TASK 27-51-65-360-801
2. Trailing Edge Flap Control Valve Internal Leakage Repair
(Figure 801)
A. References
Reference Title
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (P/B 201)
27-51-65-820-801 Trailing Edge Flap Control Valve Adjustment (P/B 501)
29-09-00-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
29-11-01-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
B. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
3 Valve assembly 27-51-61-01-265 GUN 001-007, 014-030,
109-122, 155-157, 201-
999
D. Location Zones
Zone Area
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
E. Procedure
SUBTASK 27-51-65-480-003
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR CAN RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed in the nose and main landing gear, do this task: Landing
Gear Downlock Pins Installation, TASK 32-00-01-480-801.
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SUBTASK 27-51-65-860-018
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL SURFACES, THE
THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE
SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT.
(2) Supply system B hydraulic power, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-51-65-860-019
(3) Extend the trailing edge flaps to the 40-unit position. To extend the flaps, do this task: Trailing
Edge Flap System Operation With Primary Control, TASK 27-51-00-860-801.
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(117)
