S 024-083-C01
(25) To remove the right thrust lever, remove the following pins from connectors DO8313J and DO8315J (Figs. 405 and 406):
(a)
Connector DO8313J:
1) Pins Wire No. 19 031 No. 20 032 No. 21 033 No. 22 034 No. 23 035 No. 24 036
(b)
Connector DO8315J:
1) Pins Wire No. 19 021 No. 20 022 No. 21 023 No. 22 024 No. 23 025 No. 24 026
S 024-081-C01
(26)
Separate the left (right) thrust reverser wire bundle from other wire bundles that do not require removal.
S 024-082-C01
(27)
Remove the clamps for the wire bundle.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 409 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S114
S829
S272 (INBOARD) S787 S77 S566 S564 CONDUIT SEE A
S149 (OUTBOARD) 8 2 3 4 S819
R384 S113
1 7 CONDUIT S786 S828
FWD RIGHT SIDE 4 3 2 S650 S651
A
S814 S822 S824 S825 S815 S823 6 7 S826 S827 8 D2487J 1 6
5 LEFT SIDE D3524J D8313J D8315J 5 A D5148J FWD D5150J
Thrust Lever Wire Bundle Installation Figure 405
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 410 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-038-C01
(28) Cut the lockwire and remove the nut (3, Fig. 404) from the left control shaft.
S 034-039-C01
CAUTION:_______BE CAREFUL WHEN YOU PUSH THE LEFT CONTROL SHAFT. THE KEY (9, FIG. 406) IS LOOSE AND YOU COULD CAUSE THE KEY TO FALL.
(29)
Push the left control shaft clear of the control stand with the dowel (5, Fig. 406).
S 024-040-C01
(30)
Remove the thrust lever assembly:
(a)
Pull the dowel to the left until you can lift the thrust lever assembly from the control stand. 1) Use a dowel on the right side of the control stand to hold
the right start lever and the thrust lever which is not being removed.
(b)
Tag the position of the spacers which are being removed.
NOTE: The position and the thickness of the spacers are
____ not always the same in different control stands.
TASK 76-11-01-404-041-C01
4. Thrust Lever Installation_________________________
A. References
(1)
AMM 26-21-51/401, Engine and APU Fire Control Module
(2)
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System
(3)
AMM 27-51-00/501, Trailing Edge Flap System
(4)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
(5)
AMM 76-11-04/201, Engine Control Cables
(6)
AMM 76-11-00/501, Engine Control System
B. Access
(1)
Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
202 Lower Nose Compartment
205 Electronic Compartment
(2)
Access Panel
1201 Electronic Compartment
C. Procedure
S 424-042-C01
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