78-34-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-023-C00
(16)
Remove the DO-NOT-OPERATE tags from the thrust levers.
S 874-014-C00
(17)
Do the Normal Operation Test (AMM 78-31-00/501).
(a) Do a check for hydraulic leaks.
(b) Operate the reverser between the stow and deploy positions
until all the air is bled from the system.
NOTE:____ Because of air caught in the reverser hydraulic system,
the initial sleeve movement can be short and sudden
and/or slow. When it makes a smooth movement between
the stow and deploy positions, all the air is bled from
the system.
S 414-015-C00
(18) Close the equipment bay doors of the air conditioning.
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78-34-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FEEDBACK PUSH-PULL CABLES - MAINTENANCE PRACTICES
_________________________________________________
1. General
_______
A. This procedure gives the data for the tasks that follow:
(1)
Remove the feedback push-pull cable.
(2)
Install the feedback push-pull cable.
(3)
Adjust the feedback push-pull cable.
B.
This procedure applies equally to the left or right cable on the two engines.
(1)
The differences will be explained in the procedure.
TASK 78-34-02-002-001-C00
2. Remove the Feedback Push-Pull Cable
___________________________________
A. 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 Fairing Access Doors and Panels
(3)
AMM 71-11-02/401, Fan Cowl Panels
(4)
AMM 78-31-00/201, Thrust Reverser System
B.
Access
(1)
Location Zones
506/606 Engine
507/607 Strut
502/602 Left Fan Cowl
503/603 Right Fan Cowl
(2)
Access Panels
5726L/5826R Access Door Strut
5727L/5827R Access Door Strut
5728L/5828R Access Door Strut
5729L/5829R Access Door Strut
5731L/5831R Access Door Strut
6301L/6401R LE Access Panel
C.
Remove the feedback push-pull cable.
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78-34-02
ALL ú ú C01 Page 201 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 042-002-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1)
Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 012-004-C00
(2)
Remove the fan cowl panel (AMM 71-11-02/401).
S 012-005-C00
(3)
Remove the access panel 6301L (6401R) from the top aft surface of the nacelle strut (AMM 12-31-71/201).
S 012-006-C00
(4)
Remove these access doors from the nacelle strut top and side surfaces (AMM 12-31-91/201):
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