(4)
Make sure that the trailing edge flaps are in the UP position.
S 865-005
S 865-006
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(5) S 865-022Make sure the trim cutout switch is in the NORMAL position.
(6) S 865-007Engage the autopilot A in the CWS mode.
S 865-008
CAUTION: DO NOT OPERATE THE STABILIZER TRIM MOTOR MORE THAN ONE
_______ MINUTE FOR EACH 10 MINUTES. THIS CAN CAUSE DAMAGE TO THE STABILIZER TRIM MOTOR.
(7)
Pull the control column to the aft position approximately 2 inches and release.
S 715-009
(8)
Make sure that these occur:
(a)
The stabilizer starts to move.
(b)
The stabilizer leading edge moves down at a rate of 3 units in 30 to 40 seconds.
S 865-010
(9)
Disengage the autopilot A.
S 865-011
(10)
Set the stabilizer to 5 units of trim
S 865-012
(11)
Extend the flaps to 5 degrees.
S 865-013
(12)
Engage the autopilot B in the CWS mode.
S 865-014
CAUTION: DO NOT OPERATE THE STABILIZER TRIM MOTOR MORE THAN ONE
_______ MINUTE FOR EACH 10 MINUTES. THIS CAN CAUSE DAMAGE TO THE STABILIZER TRIM MOTOR.
(13)
Push the control column to the forward position approximately 2 inches and release.
S 715-015
(14)
Make sure that these occur:
(a)
The stabilizer starts to move.
(b)
The stabilizer leading edge moves up at a rate of 1 unit in 4 to 7 seconds.
(15)
Disengage the autopilot B.
S 865-016
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S 865-017
(16)
Set the flaps in the UP position.
S 865-018
(17)
Remove hydraulic power if it is not necessary (Ref 29-15-00/201).
S 865-020
(18)
Remove electrical power if it is not necessary (Ref 24-22-00/201).
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PITCH CONTROL WHEEL STEERING FORCE TRANSDUCER -
_______________________________________________ REMOVAL/INSTALLATION
____________________
1. General_______
A. This procedure contains two tasks. The first task is for the removal of a pitch force transducer. The second task is for the installation of a pitch force transducer. In the second task, you have to adjust the pitch force transducer when you do the installation.
B. Each control column has one pitch force transducer installed on the assembly of the elevator control quadrant. The two pitch force transducers are installed opposite to each other.
TASK 22-11-92-004-001
2. Pitch Force Transducer Removal (Fig.______________________________401)
A. Standard Tools and Equipment
(1) Rig Pins - E1 and E5; 0.309 +0.003/-0.000 inch diameter, 6-inch minimum length (MS20392-4)
B. References
(1)
12-31-11/201, Body Section 41 Access Doors and Panels
(2)
12-31-41/201, Body Section 48 Access Doors and Panels
(3)
27-31-61/401, Elevator Forward Control Quadrant
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本文链接地址：737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(59)
