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时间:2011-04-08 11:56来源:蓝天飞行翻译 作者:航空
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 72-62-02
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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-M56-MM-00538-00-B
Inner and Outer Radial Drive Shaft Housing Figure 402 (Sheet 3)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
C


INNER HOUSING O-RING
AREA TO BE BONDED
C-C

S-M56-MM-00541-00-B
Inner and Outer Radial Drive Shaft Housing Figure 402 (Sheet 4)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
(e)  If the inner and outer housings can not be removed easily, do the steps that follow: 1) Do not remove the housings. 2) Remove the guide puller from the inner and outer housings. 3) Remove the outer housing. 4) Examine the outer housing for damage (AMM 72-62-02/601). 5) If there is no damage to the outer housing, install the
 outer housing in the fan frame.
 NOTE: Do not continue with the removal procedure if the
____ outer housing is not damaged.
 (f)  
If the inner and outer housings are easily removed, then continue with this procedure.

 (g)  
Remove the guide puller from the inner and outer housings.

 (h)  
Move the inner and outer housings apart.

 (i)  
Remove the preformed packings (O-rings). 1) Discard the preformed packings (O-rings).

 (j)  
Examine the inner and outer housings (AMM 72-62-02/601).


 TASK 72-62-02-404-009-C00
 3. Radial Drive Shaft (RDS) and Housing Installation
_________________________________________________
 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)  
Oil - Engine (AMM 70-10-01/201)

 (2)  
Acetone - CP1039 (AMM 70-10-01/201)

 (3)  
Loctite activator 747T, CP2400 (AMM 70-10-01/201)

 (4)  
Loctite 222, CP2410 (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 78-31-00/201, Thrust Reverser System


 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

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 72-62-02
 ALL  ú ú C01 Page 408 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(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
 
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