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 13) Tighten the bolts to 95-105 pound-inches (11-12 Newton
 ú  meters) and install a lockwire to the bolts.
 ú
 ú  NOTE:____If no more than one insert is damaged and it is
 ú  preventing the installation of the one bolt to
 ú  secure the cover, do these steps:
 ú  1. Continued service is permitted until the next
 ú  engine shop visit.
 ú  2. Use a temporary marking to identify the bolt
 ú  that was intentionally uninstalled.
 ú
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 ALL  ú ú C02.1 Page 607 ú Jul 12/02
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(5)  S 416-008-C00Close the fan cowl panel (AMM 71-11-02/201).
 (6)  S 796-013-C00Do the leak check procedure for the transfer gearbox as given in the Power Plant Test Reference Table (AMM 71-00-00/501).

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 ALL  ú ú C01 Page 608 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
RADIAL DRIVE SHAFT, INNER HOUSING AND OUTER HOUSING - REMOVAL/INSTALLATION
__________________________________________________________________________
 1.  General
_______
 A.  This procedure contains two tasks for the removal and installation of the radial drive shaft and the inner housing and outer housing.
 B.  You must remove the transfer gearbox to get access to the radial drive shaft.
 C.  You must remove the radial drive shaft to get access to the inner housing and outer housing.
 TASK 72-62-02-004-001-C00
 2.  Radial Drive Shaft (RDS) and Housing Removal
____________________________________________
 A.  General
 (1)  For this procedure the Radial Drive Shaft (RDS) will be referred to as the RDS.
 B.  Equipment
 (1)  
Guide Puller - 856A2781G01,
 CFM International, P.O. Box 15514,
 Cincinnati, OH 45215.

 (2)  
Puller - 856A3600, CFM International,

 P.O. Box 15514, Cincinnati, OH 45215
 C.  Consumable Materials
 (1)  Acetone - CP1039 (AMM 70-10-01/201)
 D.  References
 (1)  
AMM 71-11-02/201, Fan Cowl Panels

 (2)  
AMM 72-62-01/401, Transfer Gearbox

 (3)  
AMM 72-62-02/601, Radial Drive Shaft

 (4)  
AMM 78-31-00/201, Thrust Reverser

 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

 

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 72-62-02
 ALL  ú ú C01 Page 401 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
　
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