曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

(g) Connect the electrical connector to the spoiler shutoff valve at the spoiler hydraulic
modules A and B.
SUBTASK 27-62-00-860-011
(2) Set the SPOILER A and B switches on the forward overhead panel to the ON position.
SUBTASK 27-62-00-860-012
(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 27-62-00-860-013
(4) Make sure the hydraulic reservoirs are full. To fill 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 27-62-00
Page 210
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SPEED BRAKE CONTROL SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) List of associated tasks
(2) Speed Brake Control System Operational Test
(3) Speed Brake Control Lever Adjustment
(4) Speed Brake Control Cables Adjustment
(5) Ground Spoiler Control Valve Adjustment
(6) Ground Spoiler Interlock Valve Adjustment
(7) Ground Spoiler Adjustment
(8) Speed Brake Lever Friction Test
(9) Spoiler Operation Time Test
(10) Speed Brake Throttle Switch Test
(11) Engine Throttle Switch (S1) Functional Test
(12) Speed Brake Antiskid Inoperative Test
(13) Speed Brake Squat Switch Test
(14) Speed Brake RTO Test
(15) Speed Brake Extended Light Test
(16) Speed Brake Lever Brake Backlash Adjustment
TASK 27-62-00-710-801
2. Speed Brake Control System Operational Test
A. General
(1) You can use this test to quickly give the status of the speed brake control system. You can use
this test without special tools or equipment.
B. References
Reference Title
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
27-62-00-840-801 Put the Speed Brake Hydraulic systems A and B Back to the
Condition Before the Pressurization (P/B 201)
C. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
D. Procedure
SUBTASK 27-62-00-710-001
(1) Do the speed brake control system operational test:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-00
Page 501
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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.
(a) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
(b) Move the speed brake lever from the DOWN position to the UP position.
1) Make sure the speed brakes move to the UP position.
(c) Move the speed brake lever from the UP position to the DOWN position.
1) Make sure the speed brakes move to the retracted position.
(d) 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 ---------------------------
TASK 27-62-00-820-801
3. Speed Brake Control Lever Adjustment
(Figure 501)
A. General
(1) Use this procedure to adjust the speed brake control lever [8].
B. References
Reference Title
27-61-00-820-808 Spoiler Position Sensor Adjustment (P/B 501)
27-62-34-400-802 Speed Brake Armed Switch and Speed Brake Handle Position
Switch Adjustment (P/B 401)
C. 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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
E. Access Panels
Number Name/Location
112A Forward Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
　
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(jī)維護(hù)手冊(cè)6 AIRCRAFT MAINTENANCE MANUA(58)