S 864-007-C00
(6) Put the quadrant in its position to make sure that the rig pin can be put into the PT PWR rig pin hole in the housing and into the throttle gear shaft within the housing.
NOTE: This positions the thrust control push-pull cable-to-control
____ box rack connection so that the cable can be easily disconnected.
S 014-008-C00
(7)
Remove the disconnect clamps from the thrust control and the feedback push-pull cables of the thrust reverser.
S 014-009-C00
(8)
Disconnect the cable cores from the control box racks.
S 934-010-C00
(9)
Tag the feedback cables for the correct installation.
S 024-011-C00
(10)
Remove the mounting bolts of the control box and remove the box from the spar brackets.
S 014-012-C00
(11)
Remove the rig pin from the control box unless the box is to be installed.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-05
ALL ú ú C01 Page 403 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 76-11-05-404-013-C00
3. Strut Drum Control Box Installation (Fig. 401)
___________________________________
A. General
(1) The strut drum control boxes used on engine No. 1 and 2 are alike except the cable quadrants are different.
B. References
(1)
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels
(2)
AMM 27-81-00/201, Leading Edge Flaps and Slats
(3)
AMM 76-11-00/501, Engine Control System
(4)
AMM 78-31-00/201, Thrust Reverser System
(5)
AMM 78-34-02/201, Feedback Push-Pull Cables
C. Access
(1)
Location Zones
507/607 Strut
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
(2)
Access Panels
6301/6401 Leading Edge Access Panel
D. Procedure
S 424-014-C00
(1)
Put the control box in its position on the spar brackets.
S 424-015-C00
(2)
Install the bolts and the washers to the control box.
S 864-016-C00
(3)
If the rig pin is not installed in the control box, put the control box quadrant in position so that the rig pin can be inserted through the PT PWR rig pin hole in the housing into the throttle gearshaft within the housing.
S 414-017-C00
(4)
Connect the cores of the reverser feedback and the thrust control push-pull cables to the correct control box racks.
(5)
Install the disconnect clamps.
(6)
Put lockwire on the clamp screws.
S 414-018-C00
S 414-019-C00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-05
ALL ú ú C01 Page 404 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 414-020-C00
(7) Put the thrust control cables in the cable quadrant as follows:
(a)
ON ENGINE NO. 1; Put the T1A/T1B cable in the quadrant groove with the ball terminal in the indentation. 1) Install lockwire to keep the cable in its position.
(b)
ON ENGINE NO. 2; Install the T2A cable in the quadrant lower groove, and the T2B cable in the upper groove. 1) Install the terminal retainer screws.
S 824-027-C00
CAUTION: MAKE SURE THAT THE VISIBLE PARTS OF THE CONTROL CABLES AND THE
_______
QUADRANTS IN THE WING LEADING EDGE AREA ARE NOT MOIST BEFORE
YOU INSTALL THE ACCESS PANEL 6301 OR 6401. MOISTURE CAN
FREEZE DURING FLIGHT AND PREVENT CORRECT SYSTEM OPERATION.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 發(fā)動(dòng)機(jī)控制 ENGINE CONTROLS(65)
