曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
-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
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Put the Aileron Hydraulic Systems A and B Back to the Condition Before Pressure Removal
SUBTASK 27-11-00-080-001
(1) Remove the lock, SPL-1675 from the flight controls shutoff valves for systems A and B:
(a) Remove the lock, SPL-1675 from the shutoff valves.
(b) Before you connect the electrical connectors, examine the connectors for corrosion.
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.
(c) If there was corrosion, refer to (SWPM 20-60-03) to correct the problem.
(d) Apply the D5026NS or ZC-026 compound, G50171 to the connectors (SWPM 20-60-03).
(e) Install electrical connectors on the shutoff valves.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 206
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(f) Move the manual override levers on the shutoff valves to position 1.
SUBTASK 27-11-00-860-002
(2) Set the FLT CONTROL A and B switches on the forward overhead panel, P5, to the ON position.
SUBTASK 27-11-00-860-003
(3) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 13 C00363 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
C 13 C01074 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
SUBTASK 27-11-00-610-001
(4) If it is necessary to service the hydraulic reservoirs, 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 27-11-00
Page 207
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
AILERON - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) An adjustment of the aileron cables
(2) An adjustment of the pogo and power control unit
(3) An adjustment of the aileron balance tab
(4) An adjustment of the aileron feel and centering unit
(5) A check of the aileron system adjustment
(6) A test of the aileron surface friction and motion
(7) A test of the first officer’s control wheel lost motion
(8) A test of the manual reversion control friction
(9) A test of the aileron response (operation)
(10) A test of the control wheel centering check
(11) A test of the aileron control wheel force
(12) A test of the aileron trim response
(13) An operational test of the aileron spring cartridge and transfer mechanism
(14) A functional test of the aileron transfer mechanism
(15) A test of the control wheel travel stop
(16) A test of the control wheel travel interference
(17) A test of the aileron balance tab position
(18) A test of the aileron travel
(19) A functional test of the aileron power control unit (PCU) pogos
(20) A flight test to find and correct asymmetrical flight control forces
TASK 27-11-00-820-801
2. Aileron Cables Adjustment
A. General
(1) Before you do cable adjustment, permit a minimum of one hour at a constant ambient
temperature of ±58F (±2.88C) for the airframe temperature to become stable.
(a) For the new aileron wing control cables ABSA, ABSB installation, reinspection/
readjustment of the new cables’ tension must be done within 7-9 days. Further inspection/
adjustment should be accomplished within 6 to 9 months of the last cable tension
inspection.
(b) The cable tension values will not be correct when there are temperature differences along
the cable run.
B. References
Reference Title
27-11-00-860-801 Remove Pressure from the Aileron Hydraulic Systems A and B
(P/B 201)
27-11-00-860-802 Put the Aileron Hydraulic Systems A and B Back to the Condition
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(100)
