(a) On the P6 Panel:
1) ENG 2 THR REV CONT SYS - ALTN
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CFM56 ENGINES
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SEE A
AIRPLANE WIRE BUNDLE GROUND SUPPORT EQUIPMENT WIRE BUNDLE
REVERSER CONTROL VALVE MODULE
A
Ground Support Equipment Wire Bundle Installation Figure 403
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S 714-061-C00
(28) Do the Normal Operation and Auto Restow Test (AMM 78-31-00/501).
(a) Cycle the thrust reverser until all of the air is bled from the reverser hydraulic system which is when the sleeves move smoothly.
S 414-062-C00
(29) Close the fan cowl panel (AMM 71-11-02/201).
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CFM56 ENGINES
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THRUST REVERSER HYDRAULIC ACTUATORS - ADJUSTMENT/TEST
_____________________________________________________
1. General
_______
A. This section has one task:
(1)
The adjustment of the rod end of the thrust reverser locking actuator.
B.
You must do this procedure if you cannot do the step that follows:
(1)
Freely install the feedback F70207 rig pin through the feedback lever and bracket with the thrust reverser sleeve locked and stowed and all hydraulic pressure removed (AMM 78-34-02/201).
TASK 78-31-03-825-001-C00
2. Adjust the Rod End of the Thrust Reverser Actuator.
__________________________________________________
A. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
(3)
AMM 71-11-02/201, Fan Cowl Panels
(4)
AMM 78-31-00/201, Thrust Reverser System
(5)
AMM 78-31-00/601, Thrust Reverser System
(6)
AMM 78-31-04/401, Rotary Flex Shafts
B.
Access
(1)
Location Zones
506 Engine No. 1 - Torque box
606 Engine No. 2 - Torque box
(2)
Access Panels 5737L/5746L Engine No. 1 - Fan Cowl Panels 5837R/5846R Engine No. 2 - Fan Cowl Panels 5713L/5714L Engine No. 1 - Access Door Actuator 5813R/5814R Engine No. 2 - Access Door Actuator
C.
Procedure
S 045-036-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER COULD 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).
(2)
Open the fan cowl panels (AMM 71-11-02/201).
S 015-003-C00
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