(4)  
AMM 78-11-02/401, Turbine Exhaust Plug

 (5)  
AMM 78-31-00/201, Thrust Reverser System

 (6)  
CFMI Standard Practices Manual 70-44-10

 E. Access
 (1)  
Location Zones
 502/602 Left Fan Cowl Panels
 503/603 Right Fan Cowl Panels
 504/604 Left Thrust Reversers
 505/605 Right Thrust Reversers
 506 Engine No. 1 - Turbine Frame
 606 Engine No. 2 - Turbine Frame

 (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

 F. Procedure
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 72-56-00
 ALL  ú ú C01 Page 813 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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-M56-MM-00215-00-B
ENGINES WITH CFMI SB 72-362
Location of the Oil Scavenge Tube Bracket on the LPT Frame
Figure 805 (Sheet 1)

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 72-56-00
 ALL  ú ú C01 Page 814 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
BRACKET ASSEMBLY

6 O'CLOCK

S-M56-MM-00216-00-B ENGINES WITH CFMI SB 72-362 Location of the Oil Scavenge Tube Bracket on the LPT FrameFigure 805 (Sheet 2)
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 72-56-00
 ALL  ú ú C01 Page 815 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

C

S-M56-MM-00217-00-B
ENGINES WITH CFMI SB 72-362
Location of the Oil Scavenge Tube Bracket on the LPT Frame
Figure 805 (Sheet 3)

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 ALL  ú ú C01 Page 816 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 848-068-C00
 (1)  Prepare for the procedure:
 (a)  Remove the Primary Exhaust Sleeve (AMM 78-11-01/401).
 CAUTION: IT IS STRONGLY RECOMMENDED THAT YOU USE PENETRATING OIL
_______ (LIQUID WRENCH) BEFORE YOU REMOVE THE BOLTS THAT HOLD THE EXHAUST PLUG. IF YOU DO NOT USE THE PENETRATING OIL, YOU CAN CAUSE DAMAGE TO THE EQUIPMENT.
 (b)  
Remove the Turbine Exhaust Plug (AMM 78-11-02/401).

 (c)  
Remove the bolts that hold the flame arrestor to the flange assembly and the oil inlet cover. 1) Remove the flame arrestor.

 (d)  
Remove the flange assembly: 1) Remove the bolts that hold the flange assembly to the turbine frame. 2) Use six jackscrews from the tool set to remove the flange

 assembly from the engine.
 3) Remove and discard the gasket seals.

 (e)  
Remove the bolts that hold the rear cover to the midstream fairing. 1) Remove the rear cover.

 S 028-069-C00
 CAUTION: MAKE SURE THAT YOU DO NOT CUT INTO THE METAL OF THE TURBINE
　
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