(3)
AMM 78-31-00/501, Thrust Reverser System
B.
Access
(1)
Location Zones
504 Engine No. 1 - Thrust Reverser System
505 Engine No. 2 - Thrust Reverser System
604 Engine No. 1 - Thrust Reverser System
605 Engine No. 2 - Thrust Reverser System
(2)
Access Panels
101 Control Cabin
102 Control Cabin
5738L Engine No. 1 - Left Thrust Reverser
5739L Engine No. 1 - Right Thrust Reverser
5838R Engine No. 2 - Left Thrust Reverser
5839R Engine No. 2 - Right Thrust Reverser
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH PADDLE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 2 ú C01 Page 201 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
C. Procedure (Fig. 201)
S 042-002-C02
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 012-005-C02
(2)
Remove the crew seats (AMM 25-11-11/201).
S 032-006-C02
(3)
Remove the nut from the tie rod of the trim wheel to the left stabilizer.
S 032-007-C02
(4)
Remove the trim wheel (Fig. 201).
S 032-008-C02
(5)
Pull the trim wheel to the right stabilizer, with the tie rod, from the right side of the control stand.
S 032-009-C02
(6)
Do these steps when you remove the top mechanism doors:
(a)
Disconnect the lightplate electrical connections while you remove the top mechanism doors.
(b)
Make a mark on the connections.
NOTE: This will make the installation easier.
____
(c) Give protection to the lightplates to prevent possible damage.
S 032-010-C02
(7) Remove the lower doors from the control stand.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH PADDLE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 2 ú C01 Page 202 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
TIE ROD TOP MECHANISM DOOR
TIE ROD NUT
STABILIZER TRIM WHEEL SEE B LOWER DOOR
A
Thrust Reverser Arm and Stow Switches Installation
Figure 201 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH PADDLE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 2 ú C01 Page 203 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST DRUM
TOP MOUNTING SCREW SHIM
LOCATSHIM "A" ION C
DSEE LOCASHIM "B" TION
STOP FORWARD SEE C
CAM
LOWER FOLLOWER
MOUNTING ENGINE NO. 2
ARM
SCREW SWITCH BRACKET
SEE E ASSEMBLY
SWITCH BRACKET ENGINE NO. 1
ASSEMBLY SWITCH BRACKET ASSEMBLY
B
CAM FOLLOWER ARM
STOPSHIMSTOW SWITCH, S827
SWITCH ADJUSTMENT SCREW
ARM SWITCH, S826
ARM SWITCH,SWITCH S824
MOUNTING SCREW
STOW SWITCH, S825
D E
Thrust Reverser Arm and Stow Switches Installation Figure 201 (Sheet 2)
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