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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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The maximum deflection from the initial contour is

_ not more than 0.25 inch (6.3 mm).

 4.  
The angle of the deflection is not more than 60


_ degrees. c) A maximum of six blades with tip curl of the leading edge is permitted with the limits as follows:
 1.  The tip curl does not extend more than 1.3 inch
_ (33 mm) across the blade tip.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-31-02
 ALL  ú ú C02 Page 618 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
2.  
The tip curl does not extend more than 2.0 inch

_
 (51 mm) down the leading edge.


 3.  
The maximum deflection from the initial contour is

_
 not more than 0.6 inch (15 mm).


 4.  
The angle of the deflection is not more than 60

_
 degrees.


 5.  
No more than three adjacent blades have tip curl


_
 with the specified limits.
 d) One blade with tip curl of the leading edge is
 permitted with the limits as follows:

 1.  
The tip curl does not extend more than 2.0 inch

_ (51 mm) across the tip of the blade.

 2.  
The tip curl does not extend more than 2.0 inch

_
 (51 mm) into the leading edge.


 3.  
The maximum deflection from the initial contour is

_
 not more than 1.0 inch (25 mm).


 4.  
The angle of the deflection is not more than 45


_ degrees. e) There is no limit on the quantity of blades with tip curl of the trailing edge as follows:
 1.  The tip curl does not extend more than 0.5 inch
_ (12.7 mm) across the blade tip.
 2.  The tip curl does not extend more than 0.5 inch
_ (12.7 mm) down the trailing edge.
 3.  
The maximum deflection from the initial contour is

_
 not more than 0.25 inch (6.3 mm).


 4.  
The angle of the deflection is not more than 60


_ degrees. f) A maximum of six blades with tip curl of the trailing edge is permitted with the limits as follows:
 1.  
The tip curl does not extend more than 1.0 inch

_
 (25 mm) across the blade tip.


 2.  
The tip curl does not extend more than 1.0 inch

_
 (25 mm) down the leading edge.


 3.  
The maximum deflection from the initial contour is

_
 not more than 0.3 inch (7.0 mm).


 4.  
The angle of the deflection is not more than 60

_
 degrees.


 5.  
No more than three adjacent blades have tip curl


_
 with the specified limits. 5) Cracks or tears on the full Area D are not serviceable. 6) If there is distortion in Area D, the limits are as
 follows:
 NOTE: To find if a fan blade has distortion, compare it to
____
 the other blades from the rotor.

 a)  No more than 0.34 inch (8.0 mm) out of contour in two locations.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-31-02
 ALL  ú ú C01 Page 619 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
b)  The length (D) must be more than six times the depth
 (C) (Fig. 601)
 c)  Do a flourescent penetrant inspection of the area (AMM 70-40-01/201)
 S 216-014-C00
 (6)  Examine the fan blade retainers and spacers for the conditions that follow (Fig. 605):
 (a)  
Cracks are not serviceable; replace the retainer or spacer.

 (b)  
There is no limit of fretting and corrosion.


 S 216-015-C00
 (7)  Examine the areas of the fan blade dampers for the conditions that follow (IF INSTALLED) (Fig. 605):
 
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