S 415-012-C00
(11)
Install the forward, bottom panels on the pilot's control stand.
S 865-013-C00
(12)
Put the start lever in the CUTOFF detent.
S 865-014-C00
(13)
Remove the DO-NOT-CLOSE tags and close these circuit breakers.
(a) P6 Load Control Center 1) L IGN 2) R IGN
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-10
ALL ú ú C01 Page 504 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
__________________________________________________________________
1. General
_______
A. This procedure has two tasks, to remove and install the control stand
covers, seals and lightplates.
TASK 76-11-11-004-001-C01
2. Control Stand Covers, Seals and Lightplates Removal
___________________________________________________
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 864-002-C01
(1)
Remove hydraulic power (AMM 29-15-00/201).
S 864-003-C01
(2)
Put the thrust levers in the IDLE position.
S 864-004-C01
(3)
Put the start levers in the CUTOFF position.
S 024-005-C01
(4)
Do these steps to remove the covers, seals and lightplates
(Fig. 401 and 402):
(a) Remove the tie rod nut (7) from the tie rod
(8, Fig. 401).
NOTE: It is recommended that you discard the old tie rod
____ nuts and replace with new tie rod nuts.
(b)
Pull the tie rod (8) from the right side of the control stand.
(c)
Remove the control wheel (6) from the spline shaft (2).
(d)
Remove the left and right upper side doors (5).
(e)
Remove the lower right access panel (9).
(f)
Disconnect the stabilizer trim cutout switches (14).
(g)
Cut the lockwire and remove the nut (1).
(h)
Remove the fire control module (15) from the aft electronic panel (AMM 26-21-51/401).
(i)
Remove the forward and aft cover tie straps
(4 and 2, Fig. 402).
(j)
Remove the forward and aft cover angles (6 and 8).
(k)
Remove the horn cutout switch (16, Fig. 401).
(l)
Lift the cover assemblies (5, Fig. 402) from the control stand.
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 401
ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
1. RIGHT CONTROL
SHAFT NUT 2. STABILIZER TRIM CONTROL WHEEL SHAFT
3. RIGHT CONTROL 16. HORN STAND FRAME
CUTOUT
SWITCH
15. FIRE 4. KEY 5. UPPER RIGHT CONTROL
SIDE DOOR
MODULE
6. RIGHT STABILIZER TRIM CONTROL WHEEL
7. TIE ROD NUT(2 LOCATIONS)
14. STABILIZER
TRIM CUTOUT
SWITCHES
13. BOLT
12. STABILIZER TRIM
INDICATOR LINK
11. RIGHT CONTROL
SHAFT
10. CONNECTOR 8. STABILIZER TRIM LINK CONTROL WHEEL
9. LOWER RIGHT TIE ROD
ACCESS PANEL
FWD
Control Stand Access Installation
Figure 401
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