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时间:2011-04-17 09:19来源:蓝天飞行翻译 作者:航空
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 (2)  
D00010 Compound - Antiseize, Never-Seez, MIL-A-907


 B. References
 (1)  
AMM 71-11-06/201, Core Cowl Panels

 (2)  
IPC 80-11-02 Fig. 1


 C. Access
 (1)  
Location Zone
 412 Engine No. 1
 422 Engine No. 2
 432 Engine No. 3
 442 Engine N0. 4


 (2)  
Access Panel
 417 and 418 Core Cowl Panels - Engine No. 1
 427 and 428 Core Cowl Panels - Engine No. 2
 437 and 438 Core Cowl Panels - Engine No. 3
 447 and 448 Core Cowl Panels - Engine No. 4

 

 D. Procedure
 S 212-038-N00
 (1)  Prepare to install the filter.
 (a)  
Make sure the filter screen has no damage and no separation from the sleeve. 1) Replace the filter if you find these conditions.

 (b)  
Make sure the filter screen has no contamination. 1) If you find contamination, clean the filter.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 80-11-04
 ALL  ú ú N01 Page 204 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 422-039-N00
 (2)  Do these steps to install the filter (Fig. 201):
 (a)  Put the filter in the boss on the case of the start valve.
 (b)  Lubricate the new packing with the lubricant.
 (c)  Install the packing on the tube.
 (d)  Put the bushing end of the tube into the top mounting hole on
 the start valve.
 (e)  Lubricate the threads of the tube nut with the antiseize
 compound.
 (f)  Install the nut in the filter boss on the start valve.
 (g)  Tighten the nut.
 (h)  Remove all the unwanted compound.
 S 412-031-N00
 (3)  Close the core cowl panels (AMM 71-11-06/201).
 S 862-032-N00
 (4)  Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P6
 main power distribution panel.
 (a)  6J18, ENG START AIR CONT

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 80-11-04
 ALL  ú ú N01 Page 205 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.


 


 
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