76-11-11
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 402 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E64225
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
1. LEFT STABILIZER TRIM CONTROL WHEEL
3. LEFT CONTROL SHAFT NUT
2. AFT TIE STRAP
9. KEY
8. AFT COVER ANGLE
Control Stand Center Components Installation
Figure 402
4. FORWARD TIE STRAP
5.
COVER ASSEMBLIES
6.
FORWARD COVER ANGLE
7.
STABILIZER TRIM CONTROL WHEEL SHAFT
E64227
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-11
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 403 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 76-11-11-404-006-C01
3. Control Stand Covers, Seals and Lightplates Installation
________________________________________________________
A. References
(1)
AMM 26-21-51/401, Engine and APU Fire Control Module
(2)
AMM 29-15-00/201, Hydraulic System
B. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 424-007-C01
(1) Do these steps to install the covers, seals and lightplates.
(a)
Install the cover assemblies (5, Fig. 401) on the control stand.
(b)
Install the horn cutout switch (16, Fig. 401).
(c)
Install the forward and aft cover angles (6 and 8, Fig. 402) on the control stand.
(d)
Install the forward and aft cover tie straps (4 and 2).
(e)
Install the fire control module (15, Fig. 401) for the engine and the APU in the aft electronics control panel (AMM 26-21-51/401).
(f)
Install the left and right upper side doors (6).
(g)
Install the right control wheel (7) on the spline shaft (2).
NOTE: Handles on control wheels must be 90 (|15)
____ degrees apart when installed on the control stand.
(h) Install the tie rod (8) and attach with the tie rod nut (1) at each end.
NOTE: It is recommended that you discard the old tie rod
____ nuts and replace with new tie rod nuts.
1) Tighten the tie rod nuts to 60-70 inch-pounds (6.8-7.9 newton-meters).
NOTE: Make sure at least two threads on the tie rod
____ show after you tighten the tie rod nut.
S 864-008-C01
(2) Supply hydraulic power if it is necessary (AMM 29-15-00/201)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-11 STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 404
ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CONTROL STAND COVERS, SEALS AND LIGHTPLATES - REMOVAL/INSTALLATION
__________________________________________________________________
TASK 76-11-11-904-001-C02
1. Control Stand Covers, Seals and Lightplates Removal and Installation
____________________________________________________________________
A. General
(1) Do not use this configuration.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
76-11-11 STANDS WITH A TIE ROD THROUGH THE SPLINE ú CONFIG 2 SHAFT ú C01A Page 401
ú Mar 15/96
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