76-11-02
STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 415 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F14081
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
7. NO. 1 START LEVER (SHOWN REMOVED FOR CLARITY)
A
1. NO. 2 THRUST LEVER
(SHOWN REMOVED
FOR CLARITY)
SEE A
6. NO. 1 THRUST LEVER
2. CONTROL
STAND
3. NO. 2 START
LEVER
5. DOWEL
4. START CONTROL
LINK (2 LOCATIONS)
FWD
Start Lever Installation
Figure 406
F14082
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
76-11-02
STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 416 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 024-039-C03
CAUTION: CORRECT PLACEMENT OF NINE SHIMS ON THE LONG CONTROL SHAFT PER
_______ INSTALLATION IS ESSENTIAL. EXTREME CARE SHOULD BE TAKEN TO MAINTAIN SHIMS IN POSITION AS DOWEL IS INSERTED.
(12) Put the dowel against the right end of the long control shaft and gently move the long control shaft with the dowel.
(a) Put pressure on the long control shaft as you tap the dowel into place to keep the shims in the correct position.
S 024-040-C03
(13) Remove the start levers.
(a)
Remove the No. 2 start lever. 1) Push the dowel through the right support frame, the bushing, and the shim.
2) Make sure the long shaft goes through the left support frame, the bushing, the shim, the No. 1 start lever, the No. 1 thrust lever, two shims, and the No. 2 thrust lever.
(b)
Remove the No. 1 start lever.
1) Push the dowel through the right support frame, the bushing, the shim, the No. 2 start lever, the No. 2 thrust lever, two shims, and the No. 1 thrust lever.
2) Make sure the long control shaft goes through the left support frame, the bushing, and the shim.
TASK 76-11-02-404-041-C03
3. Install the Start Levers________________________
A. Equipment
(1)
Rig Pin Assembly - F70207-11.
Component of Rig Pin Kit
F70207-1, -2, -61 or -78.
Optional: MS20392-4C Pin (or equivalent 0.311
+0.000/0.002-inch diameter, 6-inch long rod or
bolt)
(2)
Dowel Set - Thrust Lever, Control Stand, F80195-1
(3)
Wrench Kit - Control Stand, C76002
(4)
Screwdriver - 90 degree No. 2 Phillips bit
B. References
(1)
AMM 12-31-11/201, Body Section 41 Access Doors and Panels
(2)
AMM 26-21-51/401, Engine and APU Fire Control Module
(3)
AMM 27-09-14/201, Flight Control Cables
(4)
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System
(5)
AMM 27-51-00/501, Trailing Edge Flap Control System
(6)
AMM 27-51-94/401, Flap 40 Unit Switches
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
76-11-02 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 417
ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(7)
AMM 27-51-94/501, Flap 40 Unit Switches
(8)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
(9)
AMM 76-11-00/501, Engine Control System
(10)
AMM 76-11-04/201, Engine Control Cables
C. Access
(1)
Location Zones
101/102 Control Cabin
202 Lower Nose Compartment
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