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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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_______ REVERSER. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (7)
Close the thrust reverser (AMM 78-31-00/201).

 S 414-016-C00

 (8)
Close the fan cowl panels (AMM 71-11-02/201).

 S 844-019-C00

 (9)  
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-01
 ALL  ú ú C01 Page 405 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TURBINE EXHAUST PLUG ASSEMBLY - REMOVAL/INSTALLATION
____________________________________________________
 1.  General
_______
 A.  This procedure has two tasks. The first task is for the removal of the Turbine Exhaust Plug. The second task is for the installation of the Turbine Exhaust Plug.
 TASK 78-11-02-004-001-C00
 2.  Remove the Turbine Exhaust Plug
_______________________________
 A.  Equipment
 (1) C78009-1 - Primary Exhaust Nozzle and Plug - Remove and Install Tool ú B. Consumable Materials ú (1) D00600 Oil, Penetrant - Liquid Wrench (CP2162)
 C.  References
 (1)  
AMM 71-11-02/201, Fan Cowl Panels

 (2)  
AMM 78-11-01/401, Primary Sleeve Assembly

 (3)  
AMM 78-31-00/201, Thurst Reverser System

 D.  
Access

 (1)  
Location Zones
 506 Left Engine - Turbine Exhaust Plug
 606 Right Engine - Turbine Exhaust Plug


 E.  
Procedure (Fig. 401)


 S 044-016-C00
 WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  
Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201)

 S 014-014-C00

 (2)  
Open the fan cowl panels (AMM 71-11-02/201).


 S 014-017-C00
 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (3)  Open the thrust reverser (AMM 78-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-11-02
 ALL  ú ú C01.1 Page 401 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-002-C00
 (4)
Remove the sleeve from the turbine exhaust (AMM 78-11-01/401).

 S 034-003-C00

 (5)  
Attach the remove-and-install tool (C78009-1) to the plug with the


 straps (Fig. 402). ú ú S 034-023-C00 ú (6) Apply the penetrant oil to the nuts and studs that attach the plug.
 S 034-004-C00
 (7)  While you hold the plug with the remove-and-install tool, remove the nuts and washers from the plug.
 NOTE: The plug weighs approximately, 55 pounds.
____
 S 024-005-C00
 (8)  Move the plug aft away from the studs.
 TASK 78-11-02-404-006-C00
 3. Install the Turbine Exhaust Plug
________________________________
 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 78-11-01/401, Primary Sleeve Assembly

 (3)  
AMM 78-31-00/201, Thurst Reverser System


 D. Access
 (1)  Location Zones
 506 Engine No. 1 - Turbine Exhaust Plug
 606 Engine No. 2 - Turbine Exhaust Plug

 E. Procedure (Fig. 401)
 S 434-007-C00
 
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