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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MAINTENANCE MANUAL EFFECTIVITY GUN ALL 27-61-00 Page 209 Oct 10/2007 D633A101-GUN BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details WARNING: DO THE STEPS BELOW IF THE AIRPLANE OPERATES AT AIRPORTS WHERE DEICING FLUID THAT CONTAIN POTASSIUM FORMATE IS USED.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 www.aero.cn 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
