(2)
Access Panels
5737L Engine No. 1 - Right Fan Cowl Panel
5738L Engine No. 1 - Left Thrust Reverser
5739L Engine No. 1 - Right Thrust Reverser
5746L Engine No. 1 - Left Fan Cowl Panel
5837R Engine No. 2 - Right Fan Cowl Panel
5838R Engine No. 2 - Left Thrust Reverser
5839R Engine No. 2 - Right Thrust Reverser
5846R Engine No. 2 - Left Fan Cowl Panel
D. Procedure
S 018-023-C00
(1) Open the left and right fan cowl panel (AMM 71-11-02/201).
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72-54-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 018-024-C00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
(2) Open the left and right thrust reverser (AMM 78-31-00/201).
E. Replace the Heat Shield (Fig. 802)
S 038-025-C00
CAUTION:_______DO NOT PERMIT THE HARDWARE TO FALL ON THE MANIFOLD. IF YOU DO NOT OBEY THIS PRECAUTION, DAMAGE TO THE EQUIPMENT CAN OCCUR.
(1)
Remove the two screws, nuts and washers that attach the coverplate to the heat shield and the manifold.
S 038-026-C00
(2)
Remove the four bolts, nuts, washers and the two spacer washers that attaches the heat shield and the manifold to the sector ring and to the angle bracket on the aft flange.
S 028-027-C00
(3)
Remove the heat shield.
S 428-028-C00
(4)
Put the replacement heat shield on the manifold.
(a)
Connect the shield and the coverplate to the manifold with two screws, nuts and washers.
(b)
Tighten the nuts to 50-55 pound-inches (5.5-6.5 Newton meters).
S 438-029-C00
(5) Put the spacer washer between the heat shield and the manifold at the two mounting bolt holes.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 438-030-C00
(6) Install the four bolts, nuts and washers that attach the heat shield and the manifold to the sector ring and the angle bracket on the aft flange.
(a) Tighten the nuts to 50-55 pound-inches (5.5-6.5 Newton meters).
S 418-031-C00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSER. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(7)
Close the left and right thrust reverser (AMM 78-31-00/201).
S 418-032-C00
(8)
Close the left and right fan cowl panels (AMM 71-11-02/201).
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72-54-00
ALL ú ú C01 Page 809 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
LOW PRESSURE TURBINE SHAFT MODULE - DESCRIPTION AND OPERATION
_____________________________________________________________
1. General
_______
A. The low pressure turbine (LPT) shaft module connects the fan shaft with the LPT rotor (Fig. 1). It is composed of the LPT shaft, LPT stub shaft, center vent tube and center vent tube rear extension duct. The aft end of the LPT shaft is supported by the No. 5 bearing; its forward end is coupled with the fan shaft. The LPT shaft has two functions: coupling the fan booster rotor with the LPT rotor and providing for high pressure turbine rear support through the No. 4 bearing. In addition, the LPT shaft houses the center vent tube of the forward and aft engine sumps.
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