S 824-018-C00
(7)
Adjust the start control push-pull cable (AMM 76-11-00/501).
S 414-019-C00
(8)
Install the access panel No. 6301 (engine No. 1) or 6401 (engine No. 2) from the upper aft surface of the nacelle strut (AMM 12-31-71/201).
S 444-020-C00
WARNING: REFER TO AMM 27-81-00/201 FOR THE LEADING EDGE FLAP LOCK
_______ PROCEDURE. FLAPS MOVE VERY QUICKLY AND CAN CAUSE INJURY TO PERSONS.
(9)
Remove the leading edge flap locks and retract the flaps (AMM 27-81-00/201).
S 444-021-C00
(10)
Remove the lockpin from the control valve of the applicable thrust reverser (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-06
ALL ú ú C02 Page 405 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST CONTROL PUSH-PULL CABLE - REMOVAL/INSTALLATION
_____________________________________________________
1. General
_______
A. This procedure has two tasks. The first task removes the push-pull cables for the thrust control. The second task installs the push-pull cables for the thrust control.
TASK 76-11-07-004-001-C00
2. Remove the Thrust Control Push-Pull Cable
_________________________________________
A. Equipment
(1)
Rig Pin - F70207-8
Component of Rig Pin Kit F70207-93.
Optional: MS20392-4C pin or equivalent 0.311
(+0.000/-0.002)-inch diameter, 3-inch long rod
or bolt
(2)
Rig Pin Assembly - F70207-23.
Component of Rig Pin Kit F70207-93.
Optional: MS20392-3C pin (or equivalent 0.248
(+0.000/-0.002)-inch diameter, 3-inch long rod
or bolt)
B. References
(1)
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels
(2)
AMM 12-31-91/201, Nacelle and Engine-To-Wing Access Doors and Panels
(3)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
(4)
AMM 54-32-01/401, Forward Fairing
(5)
AMM 71-11-02/201, Fan Cowl Panels
(6)
AMM 78-31-00/201, Thrust Reverser System
C. Access
(1)
Location Zones
5700, Engine No. 1 (Left)
5800, Engine No. 2 (Right)
(2)
Access Panels
5726L, Strut Access Door, Eng. No. 1 - left
5727L, Strut Access Door, Eng. No. 1 - top
5728L, Strut Access Door, Eng. No. 1 - top
5729L, Strut Access Door, Eng. No. 1 - top
5731L, Strut Access Door, Eng. No. 1 - right
5746L, Fan Cowl Panel, Eng. No. 1 - left
5826R, Strut Access Door, Eng. No. 2 - left
5827R, Strut Access Door, Eng. No. 2 - top
5828R, Strut Access Door, Eng. No. 2 - top
5829R, Strut Access Door, Eng. No. 2 - top
5831R, Strut Access Door, Eng. No. 2 - right
5846R, Fan Cowl Panel, Eng. No. 2 - right
D. Remove the thrust control push-pull cable (Fig. 401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-07
ALL ú ú C01 Page 401 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
SEE C
THRUST CONTROL CABLE STRUT ACCESS PANELS
1
CLAMP
SEE C
1
CLAMP THRUST
SEE B BLOCKS
CONTROL
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發(fā)動機控制 ENGINE CONTROLS(68)
