S 012-005-C00
(5)
Remove the cover from the side of the thrust lever.
S 032-006-C00
(6)
Disconnect the leads from the switch.
S 032-007-C00
(7)
Remove the switch attachment screws.
S 022-008-C00
(8)
Remove the switch together with the phenolic plates from the mount.
NOTE: Keep the plates to use with the replacement switch.
____
TASK 78-34-04-402-009-C00
3. Install the Control Switch S828 (S829) of the Thrust Reverser (Fig. 201)________________________________________________________________________
A. Access
(1) Location Zones
101/102 Control Cabin
B. Procedure
S 862-063-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 prosedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 862-045-C00
(2)
Open the applicable THR REV CONTR SYS circuit breaker on the circuit breaker panel P6.
S 422-010-C00
(3)
Put the switch in position on the mount with the actuator button turned in the direction it is shown in Fig. 201.
S 422-011-C00
(4)
Attach the switch and the phenolic plates to the mount with the screws.
NOTE: The leads are connected after the switch is adjusted.
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-34-04
ALL ú ú C03 Page 204 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 822-012-C00
(5) Adjust the switch, refer to par. 4.
TASK 78-34-04-822-013-C00
4. Adjust the Control Switch S828 (S829) of the Thrust Reverser
____________________________________________________________
A. Equipment
(1)
F70044-500, Protractor for the Reverse Thrust Lever
(2)
F70207-180 Kit, Rig Pin
B.
Consumable Materials
(1)
G01148 Tubing - Heat Shrink, Raychem RT-876, 1/16-inch diameter
C.
References
(1)
AMM 78-31-00/201, Thrust Reverser System
(2)
AMM 78-31-00/501, Thrust Reverser System
D.
Access
(1)
Location Zones
101/102 Control Cabin
502/503 Engine No. 1 - Fan Cowl Panels
602/603 Engine No. 2 - Fan Cowl Panels
(2)
Access Panels
5737L/5746L Engine No. 1 - Fan Cowl Panels
5837R/5846R Engine No. 2 - Fan Cowl Panels
E.
Procedure
S 862-064-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 prosedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 862-048-C00
(2)
Open the applicable THR REV CONTR SYS circuit breaker on the circuit breaker panel P6.
S 862-014-C00
(3)
Do the removal procedure for the Thrust Reverser control switch, if it is not done.
(4)
Attach the protractor to the reverse thrust lever (Fig. 202).
S 822-017-C00
(5)
Adjust the protractor to show zero degrees with the reverse thrust lever fully forward and down (stow position).
S 492-016-C00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-34-04
ALL ú ú C03 Page 205 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 862-065-C00
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