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时间:2011-04-04 10:10来源:蓝天飞行翻译 作者:航空
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 NOTE: On inlet cowls with the rubstrips, you can see 5
____ rubstrips on the aft edge of the inlet cowl between the 11 and 1 o'clock positions.
 (a)  
If you see the fiberglass backing under the rubstrip, you must replace the rubstrip.

 (b)  
Refer to the Maintenance Manual (AMM 71-11-01/401) for the replacement of these rubstrips.


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 71-11-01
 ALL  ú ú C03 Page 603 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 416-005-C00
 (4) Close the fan cowl panels (AMM 71-11-02/201).
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 71-11-01
 ALL  ú ú C01 Page 604 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FAN COWL PANELS - MAINTENANCE PRACTICES (OPENING AND CLOSING)
_____________________________________________________________
 1.  General
_______
 A.  This procedure contains two tasks. The first task is to open the fan cowl panels. The second task is to close the fan cowl panels.
 B.  Each fan cowl panel is held open with a hold-open rod. The hold-open rod is spring-loaded in the stowed position, and has a double action lock. Two clear movements of the lock are necessary to release the hold-open rod from the extended position.
 C.  An unlock indication will be seen when the hold-open rod is released (stowed position) and will not be seen when the hold-open rod is locked (extended position).
 TASK 71-11-02-012-001-C00
 2.  Open the Fan Cowl Panel
_______________________
 A.  References
 (1)
27-81-00/201, Leading Edge Component Deactivation

 B.  
Access

 (1)  
Location Zone
 506 Engine No. 1 - Fan Frame
 606 Engine No. 2 - Fan Frame


 (2)  
Access Panel
 5746 Fan Cowl Panel (LH) - Engine No. 1
 5846 Fan Cowl Panel (LH) - Engine No. 2
 5737 Fan Cowl Panel (RH) - Engine No. 1
 5837 Fan Cowl Panel (RH) - Engine No. 2


 C.  
Procedure (Fig. 201)


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 71-11-02
 ALL  ú ú C01 Page 201 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE B
SEE C
LEFT FAN COWL PANEL
LATCH 
(4 PLACES) 
SEE  A 
LATCH 
RIGHT FAN 
COWL PANEL 

SEE D
Fan Cowl Panel Opening and Closing Figure 201 (Sheet 1)
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-11-02
 ALL  ú ú C01 Page 202 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
PRESS 
HERE 
COLLAR 
PUSH  UNLOCK  SLEEVE 
INDICATION 
TRIGGER 
HOLD OPEN 
ROD 
LIFT 
HERE 
RECEIVER 
HOLD OPEN ROD (STOWED) 
A  B 
HOLD OPEN
ROD  ENGINE 
RECEIVER  HOLD OPEN  RECEIVER  IDENTIFICATION 
ROD  PLATE 
 
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