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S 045-034-N00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(5) Do the deactivation procedure for the thrust reverser isolation valve (AMM 78-31-00/201).
NOTE: Do not install the ground deactivation pins in the thrust
____
reverser sleeves.
S 865-035-N00
CAUTION: DO NOT EXTEND THE THRUST REVERSER IF THE CORE COWL PANELS ARE
_______ OPEN. DAMAGE TO THE THRUST REVERSER AND CORE COWL PANELS COULD OCCUR.
MAKE SURE THE AREA AFT OF THE THRUST REVERSER IS CLEAR OF ALL EQUIPMENT, WORKSTANDS, ETC. DAMAGE COULD OCCUR IF THE THRUST REVERSER CONTACTS THE EQUIPMENT.
WHEN YOU MOVE THE THRUST REVERSER MANUALLY, LOOK FOR LOWER ACTUATOR OPERATION, OR LOWER AND CENTER ACTUATOR OPERATION. IF YOU SEE THIS OPERATION, STOP AND LOOK FOR BROKEN FLEXSHAFTS.
(6)
Make sure that the core cowl panels are closed and latched.
S 725-036-N00
(7)
Turn the manual drive mechanism on the sync lock with a 3/8 inch square drive in the correct direction to try to extend the actuator.
NOTE: A torque value of 45 inch-pounds should be sufficient to move
____ the thrust reverser sleeve. However, excess torque is acceptable because of the clutch mechanism in the sync lock which will prevent overtorquing of the manual drive.
S 725-037-N00
(8) Make sure that the actuators do not extend.
(a) If the actuators extend, replace the locking hydraulic actuator (AMM 78-31-17/401).
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S 415-038-N00
(9)
Close the fan cowl panels (AMM 71-11-04/201).
S 445-039-N00
(10)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
S 445-040-N00
(11)
Do the activation procedure for the Speed Brake Control System (AMM 27-62-00/201).
S 945-041-N00
(12)
Remove the DO-NOT-OPERATE tags from the thrust levers.
TASK 78-31-00-825-042-N00
5. Rod End Gap Adjustment for the Locking Hydraulic Actuator
_________________________________________________________
A. General
(1)
Do this task to adjust the rod end gap of the locking hydraulic actuator if the rod end gap is more than the specified limit of
0.100 inch (2.54 mm) with the hydraulic power removed.
(2)
The locking hydraulic actuator is referred to as the locking actuator in this procedure.
B.
References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
(3)
AMM 71-11-04/201, Fan Cowl Panels
(4)
AMM 78-31-00/201, Thrust Reverser System
C.
Access
(1)
Location Zones 415 and 416 Engine 1 - Thrust Reverser Halves 425 and 426 Engine 2 - Thrust Reverser Halves 435 and 436 Engine 3 - Thrust Reverser Halves 445 and 446 Engine 4 - Thrust Reverser Halves
(2)
Access Panels 413 and 414 Fan Cowl Panels - Engine 1 413AL/414AR Rod End Access Panels - Engine 1 423 and 424 Fan Cowl Panels - Engine 2 423AL/414AR Rod End Access Panels - Engine 2 433 and 434 Fan Cowl Panels - Engine 3 433AL/414AR Rod End Access Panels - Engine 3 443 and 444 Fan Cowl Panels - Engine 4 443AL/444AR Rod End Access Panels - Engine 4
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
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