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

Page 604
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flight Spoiler Actuator Wear Limits
Figure 601 (Sheet 2 of 3)/27-61-51-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-51
Page 605
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flight Spoiler Actuator Wear Limits
Figure 601 (Sheet 3 of 3)/27-61-51-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-51
Page 606
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLIGHT SPOILER ACTUATOR QUADRANT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flight spoiler actuator quadrants.
(2) An installation of the flight spoiler actuator quadrants.
(3) A functional test of the flight spoiler actuator quadrants.
B. In this procedure the flight spoiler actuator quadrant is referred to as the "quadrant".
C. This procedure is applicable to the left and right flight spoiler actuator quadrants.
TASK 27-61-61-000-801
2. Flight Spoiler Actuator Quadrant Removal
(Figure 401, Figure 402)
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. 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
562 Left Wing - Spoiler No. 5
563 Left Wing - Spoiler No. 4
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
662 Right Wing - Spoiler No. 8
663 Right Wing - Spoiler No. 9
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
C. Prepare for the Removal
SUBTASK 27-61-61-860-001
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-61-860-002
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: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-61
Page 401
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-61-61-860-003
(3) Do this task: Extend the Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-61-61-860-004
(4) Move the speed brake lever to the DOWN position.
SUBTASK 27-61-61-860-005
(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 27-61-61-860-006
(6) Make sure the ailerons are in the neutral position.
D. Flight Spoiler Actuator Quadrant Removal
SUBTASK 27-61-61-020-001
(1) Disconnect the wing spoiler cables WSA [2] and WSB [4] from the applicable quadrant:
(a) Install the turnbuckle clamps to keep a small tension on the wing spoiler cables WSA [2]
and WSB [4].
(b) Loosen the turnbuckles [3] for the cables.
(c) Remove the guard pin [34], guard [35] and pin [36].
(d) Remove the nuts [28], washers [27], bolts [26] and retainers [29].
(e) Remove the wing spoiler cables WSA [2] and WSB [4] from the quadrant [37].
SUBTASK 27-61-61-020-002
(2) Remove the flight spoiler actuator quadrant [37]:
(a) Remove the pin [33], nut [32], washer [31], and bolt [30] to disconnect the quadrant [37] from
the actuator input arm [21].
(b) Remove the nut [25], washer [24], washer [23], and bolt [22] from the quadrant [37].
NOTE: Keep the bearings and bushing with the quadrant [37].
(c) Remove the quadrant [37] from the structure.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-61
Page 402
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
　
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(52)