曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(c) Do this task: Remove Pressure from the Spoiler Hydraulic Systems A and B,
TASK 27-61-00-800-802.
------------------------- END OF TASK ---------------------------
TASK 27-61-61-000-802
4. Flight Spoiler Actuator Quadrant Functional Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-61-00-820-804 Spoiler Actuator Linkage Adjustment (P/B 501)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B 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.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-61
Page 407
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Reference Description
COM-1691 Protractor - Digital, Vertical or Horizontal
(Part #: KS5549, Supplier: 75245, A/P Effectivity: 737-ALL)
SPL-1670 Mount - Control Wheel Protractor
(Part #: F72790, Supplier: 81205, A/P Effectivity: 737-100, -200, -200C,
-300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900, -900ER,
-BBJ)
SPL-1680 Protractor - Assembly, Control Column
(Part #: 4MIT65B80307-1, Supplier: 81205, A/P Effectivity: 737-100,
-200, -200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800,
-900, -900ER, -BBJ)
(Part #: A27021-29, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. 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
D. Prepare for the Test
SUBTASK 27-61-61-860-007
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-61-860-008
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-61-61-480-001
(3) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 on the
captain’s aileron control wheel.
SUBTASK 27-61-61-860-009
(4) Move the speed brake lever to the DOWN position.
SUBTASK 27-61-61-860-010
(5) Put the ailerons in the neutral position.
SUBTASK 27-61-61-480-002
(6) Install the protractor, COM-1691 on the flight spoilers 2, 4, 9 and 11.
SUBTASK 27-61-61-820-003
(7) Adjust the protractor, COM-1691 to zero.
E. Flight Spoiler Actuator Quadrant Test
SUBTASK 27-61-61-020-003
(1) Turn the captain’s aileron control wheel clockwise until the spoiler No. 9 starts to extend.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-61
Page 408
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Make sure the control wheel is 11 +/-1 degrees clockwise from zero.
SUBTASK 27-61-61-020-004
(2) Turn the control wheel 87 degrees clockwise:
(a) Make sure that the spoiler No. 9 moves 37 +/-3 degrees up from the retracted position.
(b) Make sure that the spoiler No. 11 moves 32 +/-3 degrees up from the retracted position.
(c) Make sure the spoiler No. 2 is in the retracted position.
SUBTASK 27-61-61-020-005
(3) Turn the wheel counterclockwise until the spoiler No. 9 starts to retract.
(a) Make sure the control wheel is a minimum of 70 degrees clockwise.
SUBTASK 27-61-61-020-006
(4) Turn the wheel counterclockwise until the spoiler No. 9 is fully retracted.
(a) Make sure the spoiler is fully retracted when the control wheel is 5 +/-3 degrees
clockwise.
SUBTASK 27-61-61-020-007
(5) Turn the wheel counterclockwise until the spoiler No. 2 starts to extend.
(a) Make sure the control wheel is 11 +/-1 degrees counterclockwise from zero.
SUBTASK 27-61-61-020-008
(6) Turn the control wheel 87 degrees counterclockwise:
　
中國航空網 m.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(54)