(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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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72-56-00
ALL ú ú C01 Page 816 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
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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