78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 207 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b) Optionally, remove the switches and the actuator from the bracket and then remove the applicable switch from the actuator.
TASK 78-34-05-402-015-C01
3. Thrust Reverser Arm and Stow Switches Installation
__________________________________________________
A. References
(1) 31-26-00/501, Aural Warning System
B. Access
(1) Location Zones
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
101/102 Control Cabin
C. Procedure
S 432-016-C01
(1)
If the cam followers have been removed, install the cam followers and the switch bracket.
S 432-017-C01
(2)
Put the switch into the actuator and the bracket.
(a) Install the mounting and adjustment screws finger-tight.
NOTE: The screws will be tightened after the switches are
____
adjusted.
S 432-018-C01
(3)
Install the control lever bracket for stabilizer trim.
S 422-019-C01
(4)
Put the switch-and-bracket assembly in its position.
(a)
Connect the leads to the switches.
(b)
Install the screws and washers.
S 822-020-C01
(5) Adjust the takeoff warning and wing thermal anti-ice deactivation switches (S814, S815, S822 and S823) (AMM 31-26-00/501).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 208 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 822-021-C01
(6) Adjust the arm and stow switches (S824, S825, S826 and S827) (Ref para Thrust Reverser Arm and Stow Switch Adjustment).
TASK 78-34-05-822-022-C01
4. Thrust Reverser Arm and Stow Switch Adjustment
__________________________________________________
A. Equipment
(1)
Reverse Thrust Lever Protractor - F70044-500
(2)
Test Cable - Locally fabricated from one
MS24266R16B24S6 plug (to mate with D5148J) and
one MS24266R16B24S8 plug (to mate with D5150J)
connected by 5-foot lengths of No. 20
A.W.G. wire; connect wires pin-to-pin.
B.
References
(1)
AMM 12-31-11/201, Body Section 41 Access Doors and Panels
(2)
AMM 25-11-11/201, Flight Compartment Equipment
(3)
AMM 31-26-00/501, Aural Warning System
(4)
AMM 71-11-02/201, Fan Cowl Panels
(5)
AMM 78-31-00/201, Thrust Reverser System
C.
Access
(1)
Location Zones
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
202 Lower Nose Compartment
101/102 Control Cabin
(2)
Access Panel
1103 - Lower Nose Compartment Access Door
D.
Procedure
S 042-023-C01
WARNING: DO THE DEACITVATION 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) If not already done, do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
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