(e)
Install the clip locks on the turnbuckles.
S 865-077
(15)
Do this task: "Remove Hydraulic Power" (Ref 29-11-00/201).
(16)
Do this task: "Remove Electrical Power" (Ref 24-22-00/201).
S 415-079
(17)
Close the access panels on the wing trailing edge
(Ref 06-09-08/201).
M.
Adjust the Inboard Aileron Control Linkage
S 865-078
S 865-080
(1) Do this task to supply systems No. 1 and 4, or 2 and 3 hydraulic power: "Supply Hydraulic Power" (Ref 29-11-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-11-00
ALL ú ú 03 Page 526 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
(2) S 865-081Turn the control wheel to the neutral position.
(3) S 485-082Install rig pins A/S-8 and A/S-9 in the inboard aileron control quadrants (Fig. 504).
(4) S 495-083If you use the inboard aileron rigging straightedge, install the tool as follows: (a) Align the tool at the centerline of the inboard primary hinge.
(5) S 495-084If you use the rigging beam, install the tool as follows: (a) Open the access panels (573AB, left; 673AB, right) (Ref 06-09-08/201). (b) Hold the rigging beam manually at WBL 461.5 below the aileron and the wing.
(6) S 225-199With hydraulic power on and ailerons at neutral, make sure the permitted mismatch between the aileron trailing edge and the lower surface of the wing trailing edge is not out of tolerance (Fig. 505).
(7) S 835-085If the permitted mismatch is out of tolerance, adjust the input control rod between the control quadrant and the power package to get the mismatch in tolerance.
(8) S 085-086Remove all the rig pins.
(9) S 715-087Operate the ailerons for a minimum of two full cycles. (a) Make sure the ailerons align with the lower surface of the wing trailing edge (Fig. 505).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-11-00
ALL ú ú 03 Page 527 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 865-088
(10)
Do this task: "Remove Hydraulic Power" (Ref 29-11-00/201).
S 215-158
(11)
Make sure to install all the lockwire, cotter pins, and clip locks on the turnbuckles.
S 095-090
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(12) Do this task: "Removal of the Door Locks from the Wing Landing Gear" (Ref 32-00-30/201).
TASK 27-11-00-705-091
6. Aileron and Aileron Trim Control System Test____________________________________________
A. General
(1)
The system test of the aileron and aileron trim control examines the movement of the load limiter mechanism. It also does a check on the trim, friction and centering operation, the lockout mechanism, and the aileron response time and movement.
B.
Standard Tools and Equipment
(1)
Stop watch
C.
Special Tools and Equipment
(1)
MIT65B04001-41 Control Wheel Straightedge
(2)
3MIT65B80307-1 Control Wheel Adapter
(3)
4MIT65B80307-1 Control Column Protractor (Recommended)
(4)
F52485-500 Control Column Protractor (Optional)
D.
References
(1)
24-22-00/201, Manual Control
(2)
27-11-00/501, Aileron Lockout System Existing Faults Check
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-11-00 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(63)
