22-11-26
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AUTOPILOT ELEVATOR ACTUATOR - ADJUSTMENT/TEST
_____________________________________________
1. General
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A. This procedure contains three tasks. The first task and second task are the adjustment of the autopilot elevator actuator. The first task uses the F80217-125 test set for adjustment of the actuator. The second task uses the DFCS BITE test for the adjustment of the actuator (airplanes with -912 and on FCC). You can use one of these tests to adjust the actuator. The third task is the autopilot elevator actuator test.
TASK 22-11-26-825-001
2. Autopilot Elevator Actuator Adjustment (F80217-125 Test Set)
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A. References
(1)
AMM 12-31-41/201, Body Section 48 Access Doors and Panels
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-31-00/501, Elevator and Tab Control System
(4)
AMM 29-15-00/201, Hydraulic A, B, and Standby System
B. Access
(1)
Location Zone
704 Tail Cone
(2)
Access Panel
3802 Tail Cone Access Door
C. Special Tools and Equipment
(1) Test Set - Autopilot Elevator/Rudder/Aileron Control Unit - P/N F80217-125
D. Standard Tools and Equipment
(1)
VTVM - FLUKE (Digital)
(2)
Pressure source - Dry air, 0 to 5 psi, with gage, fittings (to connect to the pitot tubes of the feel system)
(3)
Ladder or stand - use to measure the elevator position on tail cone
E. Autopilot Elevator Actuator Adjustment
S 865-003
(1)
Supply electrical power (AMM 24-22-00/201).
S 865-078
(2)
Make sure that the elevator is rigged properly by doing the following:
NOTE: The elevator must be correctly rigged before you can adjust
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the autopilot elevator actuators.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SHAFT QUADRANT OUTPUT B ACTUATOR AUTOPILOT
SEE A CONTROL ARM ELEVATOR
A ACTUATOR AUTOPILOT
A/P ACTUATOR B LEVER ASSEMBLY SEE ELEVATOR A PCU B B PCU SHAFT QUADRANT INPUT ELEVATOR
ROD ASSEMBLY CONNECTOR ELECTRICAL FWD A
LEVER ASSEMBLY
HYDRAULIC LINE 9.43 INCHES NOMINAL
A/P ACTUATOR A
ROD ASSEMBLY NOMINAL 17.52 INCHES
TUBE LEVER LOWER TORQUE
B
A/P Elevator Actuator Installation Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-26
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(a)
Set the horizontal stabilizer B dimension to 41.57 |0.01 inch.
(b)
With hydraulic power on, make sure that the trailing edge of the elevator is aligned with the index plate mark |0.16 inch above and below the mark. If the elevator is not aligned, make adjustments: "Adjustment - Elevator and Tab Control System" (AMM 27-31-00/501).
S 865-004
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Supply hydraulic power (AMM 29-15-00/201).
S 865-006
(4)
Open the SHUTOFF VALVE FLT CONT circuit breakers on the P6 Circuit Breaker Panel.
S 015-007 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 2(3)
