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时间:2011-04-09 10:08来源:蓝天飞行翻译 作者:航空
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 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-01
 ALL  ú ú C01 Page 401 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-004-C00
 (4)  
Remove the skirt fairing from the sleeve.

 S 034-005-C00

 (5)  
Attach the remove-and-install tool (C78009-1) to the sleeve with the straps (Fig. 402).

 S 034-006-C00

 (6)  
Remove the bolts and washers that connect the sleeve to the rear flange of the turbine frame.

 S 024-007-C00

 (7)  
When it is necessary, move the sleeve aft to be clear of the exhaust plug before you lower the sleeve.


 TASK 78-11-01-404-008-C00
 3.  Install the Primary Sleeve Assembly___________________________________
 A. Equipment
 (1) C78009-1 Primary Exhaust Nozzle and Plug, Remove and Install Tool
 B. Consumable Materials
 (1)  D00006 Antiseize Compound, Bostik Never-Seez Pure Nickel Special
 C. References
 (1)  
AMM 71-11-02/201, Fan Cowl Panels

 (2)  
AMM 78-31-00/201, Thrust Reverser System


 D. Access
 (1)  Location Zones
 506 Left Engine - Turbine Exhaust Area
 606 Right Engine - Turbine Exhaust Area

 E. Procedure (Fig. 401)
 S 034-009-C00
 (1)  
If you installed the skirt fairing, remove it from the sleeve.

 S 434-010-C00

 (2)  
Attach the remove-and-install tool to the sleeve with the straps (Fig. 402).

 S 424-011-C00

 (3)  
Lift the sleeve and do the steps that follow:

 (a)  
Align the largest opening in the mounting ring of the sleeve with the locating pin.

 (b)  
Install the locating pin at the 12:00 o'clock position, approximately, on the rear flange of the turbine frame.

 


 S 424-012-C00
 (4)  Attach the sleeve with the bolts and washers.
 (a)
Lubricate bolt threads and shank with antiseize compound.

 (b)
Tighten the bolts 70-80 pound-inches (8-9 Newton meters).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-01
 ALL  ú ú C01 Page 402 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////


Primary Sleeve Assembly Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-01
 ALL  ú ú C01 Page 403 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

REMOVE/INSTALL TOOL (C78009-28)
C78009 Remove/Install Tool Figure 402
 E03638
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-01
 ALL  ú ú C01 Page 404 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(5)  S 434-013-C00Remove the remove-and-install tool from the sleeve.
 (6)  S 434-014-C00Install the skirt fairing as follows: (a) Loosely install all the screws to the fairing. (b) Tighten the screws to 17 pound-inches (2 Newton meters).
 S 414-015-C00

 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
 
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