TASK 27-61-00-840-802
5. Put the Spoiler Systems A and B Back to the Condition Before the Pressure Removal
(Figure 201, Figure 202)
A. References
Reference Title
12-12-00-610-801 Hydraulic Reservoir Servicing (P/B 301)
SWPM 20-60-03 Standard Wiring Practices Manual
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-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
E. Procedure
SUBTASK 27-61-00-080-002
(1) Remove the flight controls hydraulic module locks from the spoiler shutoff valves.
(a) Remove the lockpins.
(b) Remove the lock, SPL-1675 from the two spoiler shutoff valves.
(c) Put the manual override lever at the two spoiler shutoff valves in the position 1 (ON
position).
(d) Before you connect the electrical connector, examine the connector for corrosion.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 209
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
WARNING: DO THE STEPS BELOW IF THE AIRPLANE OPERATES AT AIRPORTS WHERE
DEICING FLUID THAT CONTAIN POTASSIUM FORMATE IS USED. ALSO DO THE
STEPS FOR ALL AIRPLANES THAT YOU FOUND CORROSION IN THE
ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. THE ELECTRICAL
CONNECTOR IS PART OF A SYSTEM THAT IS NECESSARY FOR SAFE FLIGHT.
(e) If there was corrosion, refer to (SWPM 20-60-03) to correct the problem.
(f) Apply the D5026NS or ZC-026 compound, G50171 to the connector (SWPM 20-60-03)
(g) Connect the electrical connector to the spoiler shutoff valve at the spoiler hydraulic
modules A and B.
SUBTASK 27-61-00-860-011
(2) Set the SPOILER A and B switches on the forward overhead panel to the ON position.
SUBTASK 27-61-00-860-012
(3) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 12 C00204 FLIGHT CONTROL SHUTOFF VALVES SPOILER
SUBTASK 27-61-00-860-013
(4) Pressurize the hydraulic reservoirs if it is necessary. To pressurize them, do this task: Hydraulic
Reservoir Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 210
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SPOILER CONTROL SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) Spoiler Control System Operational Test
(a) This test can be used to quickly give the status of the spoiler control system. This test can
be done without special tools or equipment.
(2) Spoiler Control Cables Adjustment
(3) Ratio Changer Input Rod Adjustment
(4) Flight Spoiler Adjustment
(a) An adjustment of the clearance between the flight spoilers and the flaps.
(5) Spoiler Actuator Linkage Adjustment
(6) Spoiler Mixer Adjustment
(7) Spoiler Position Sensor Adjustment
(a) This is an adjustment and test of the operation of the spoiler position sensors No. 3 and 10.
(8) Flight Spoiler System Test
(a) This is a test of the operation of the flight spoilers No. 2, 3, 4, 5, 8, 9, 10, and 11.
(9) Spoiler Manual Operation Test
(10) Spoiler Operation Time Test
(11) Alternate Spoiler Position Sensor Test
(a) This is a test of the operation of the spoiler position sensors No. 4 and 9.
(12) Spoiler Mixer No-Back Assembly Test
(13) Spoiler Mixer Centering Mechanism Operational Test
B. The spoiler control system gives lateral control and speed brake signals to the flight spoiler
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 飛機維護手冊6 AIRCRAFT MAINTENANCE MANUA