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Spoiler Wheel Well Mechanical Components Inspection
Figure 601 (Sheet 1 of 2)/27-61-00-990-813
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Spoiler Wheel Well Mechanical Components Inspection
Figure 601 (Sheet 2 of 2)/27-61-00-990-813
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 604
Oct 10/2007
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SPOILER POSITION SENSOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) The removal of a spoiler position sensor.
(2) The installation of a spoiler position sensor.
B. There are four spoiler position sensors. The spoiler position sensors No. 3 and No. 10 are for the
flight spoiler system and spoiler position sensors No. 4 and No. 9 are for the autopilot system.
C. This procedure only contains the tasks for the spoiler position sensors No. 3 and No. 10. For the
removal and installation procedures of the spoiler position sensors No. 4 and No. 9, refer to
(TASK 22-11-27-000-801).
D. The spoiler position sensor No. 3 (T539) is installed on the left wing spoiler No. 3. The spoiler position
sensor (T540) No. 10 is installed on the right wing spoiler No. 10. To get access to the spoiler position
sensors, you must extend the spoilers.
TASK 27-61-04-000-801
2. Spoiler Position Sensor Removal
(Figure 401)
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (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-1745 Set - Lock, Flight Spoiler Actuator (Contains 8 Lock Assemblies)
(Part #: C27047-19, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
C. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
564 Left Wing - Spoiler No. 3
664 Right Wing - Spoiler No. 10
D. Prepare for the Removal
SUBTASK 27-61-04-860-001
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
737-600/700/800/900
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EFFECTIVITY
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SUBTASK 27-61-04-860-002
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM THE FLIGHT CONTROL SURFACES.
THE AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, STABILIZER AND
NOSE GEAR CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS
CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
SUBTASK 27-61-04-860-003
(3) Do this task: Extend the Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-61-04-860-004
(4) Do this step to extend the spoiler:
(a) Move the speedbrake lever to the UP position.
SUBTASK 27-61-04-860-005
(5) Do this task: Put the Spoiler Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-61-00-840-801.
SUBTASK 27-61-04-860-006
(6) Install set, SPL-1745 on the spoiler actuator No. 3 or No. 10.
E. Procedure
SUBTASK 27-61-04-020-001
(1) Do these steps to disconnect the electrical connectors of the spoiler position sensor [1],
(Figure 401):
(a) Remove the lockwire.
(b) Disconnect the electrical connector.
SUBTASK 27-61-04-020-002
(2) Do these steps to remove the spoiler position sensor [1]:
(a) Remove the bolt [7], washer [8] and nut [5] in the crank [9].
(b) Remove the bolt [2], washer [3] and nut [5] in the mounting bracket [6].
(c) Remove the spoiler position sensor [1].
------------------------- END OF TASK ---------------------------
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