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

(b) Retract the lower slider assembly [6].
(c) Make sure the PSEU BITE displays NO GND
(d) Move the speedbrake handle to the UP position.
(e) Extend the lower slider assembly [6].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-61
Page 513
Jun 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(f) Make sure the PSEU BITE displays GND.
SUBTASK 27-62-61-420-005
(3) Install bolt [2], washer [3], washer [4] and nut [5] to install the lower slider assembly [6] to the lug
on the right landing gear strut.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-62-61-860-035
(1) Push the ON/OFF switch on PSEU BITE display to turn the PSEU BITE off.
SUBTASK 27-62-61-840-002
(2) Close this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-62-61-860-036
(3) Do this task: Put the Speed Brake Hydraulic systems A and B Back to the Condition Before
the Pressurization, TASK 27-62-00-840-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-61
Page 514
Jun 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
INBOARD GROUND SPOILER ACTUATOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the inboard ground spoiler actuator.
(2) An installation of the inboard ground spoiler actuator.
(3) A functional test of the inboard ground spoiler actuator.
B. In this procedure the inboard ground spoiler actuator is referred to as the "actuator".
C. This procedure is applicable to the left and right inboard ground spoiler actuators.
TASK 27-62-71-000-801
2. Inboard Ground Spoiler Actuator 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)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
27-62-00-800-802 Remove Pressure from the Speed Brake Hydraulic Systems A and B
(P/B 201)
B. Tools/Equipment
Reference Description
STD-1110 Container - Hydraulic Fluid Resistant, 5 Gallon (19 Liters)
C. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
552 Left Wing - Spoiler No. 6
652 Right Wing - Spoiler No. 7
D. Prepare for the Removal
SUBTASK 27-62-71-860-001
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-62-71-860-002
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: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-62-71-860-003
(3) Put the SPOILER A and B switches in the OFF position to remove the hydraulic power from the
flight spoilers.
NOTE: SPOILER A and B switches are on the flight control panel (P5-3).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-71
Page 401
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-62-71-860-004
(4) Do this task: Extend the Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-62-71-860-005
(5) Do this task: Remove Pressure from the Speed Brake Hydraulic Systems A and B,
TASK 27-62-00-800-802.
E. Actuator Removal
SUBTASK 27-62-71-020-001
(1) Disconnect the hydraulic lines [10] from the actuator [17]:
(a) Put a 5 gallon (19 liters) hydraulic fluid resistant container, STD-1110 below the actuator [17]
to catch the hydraulic fluid.
(b) Disconnect the hydraulic lines [10] from the actuator [17].
(c) Install the plugs in the hydraulic lines [10].
SUBTASK 27-62-71-020-002
(2) Remove the pin [7], nut [6], washer [5], bushing [4], washer [5] and bolt [2] that attach the
actuator [17] to the inboard ground spoiler [1].
SUBTASK 27-62-71-020-003
(3) Remove the pin [16], nut [15], washer [14], bushing [13], washer [12] and bolt [11] that attaches
the actuator [17] to the structure.
SUBTASK 27-62-71-480-001
(4) Install caps in the hydraulic ports of the actuator [17].
------------------------- END OF TASK ---------------------------
　
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7 AIRCRAFT MAINTENANCE MANUA(24)