BOOSTER ROTOR BLADE
B
NOTE: ALL DIMENSIONS ARE IN INCHES WITH MILLIMETERS IN PARENTHESES S-M56-MM-0976-(1)-00-B
Booster Rotor and Stator Vane Damage Inspection
Figure 603

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01 Page 610 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
AA

AREA A 
SEE  A 
SEE  B 
0.4 (10) 
AREA C  A-A 
LEADING 
EDGE  AREA B 
TRAILING 
EDGE  0.4 (10) 

BOOSTER VANE ASSEMBLY
A
MISSING PIECES
0.787 (20) G
AXIAL  LEADING EDGE
RADIAL
LEADING EDGE E 0.4 (10)
BOOSTER ROTOR BLADE
B
NOTE: ALL DIMENSIONS ARE IN INCHES WITH MILLIMETERS IN PARENTHESES S-M56-MM-1024-(3)-00-B
Booster Rotor and Stator Vane Damage Maximum Service Extension Figure 604
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01 Page 611 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
LPC Blades and Vanes (1st- thru 4th-Stage) - Inspection
_______________________________________________________
 2.  No more than 15 blades are damaged.
_
 4)  Look for nicks, dents and scratches on the airfoil surfaces that are in area E. a) No maximum number if the damage is less than 0.019 inch
 ú  (0.5 mm) in depth.
 1.  Protrusions are permitted if they do not go through
_ the metal. b) A maximum service extension of 50 cycles/75 hours is permitted if the damage is less than 0.059 inch
 (1.5 mm) in depth.
 1.  Protrusions are permitted if they do not go through
_ the metal.
 5)  Look for nicks, dents and scratches on the airfoil surfaces that are not in area E and not in the leading and trailing edges. a) No maximum number if the damage is less than 0.157 inch
 (4 mm) in depth.
 1.  Protrusions are permitted if they do not go through
_ the metal.
 b)  A maximum service extension of 50 cycles/75 hours is permitted if the damage is less than 0.236 inch (6 mm) in depth.
 1.  Protrusions are permitted if they do not go through
_ the metal.
 6)  Look for nicks, dents and scratches on the leading and trailing edges and not in Area E. a) The maximum axial length is 0.039 inch (1 mm). b) A maximum service extension of 50 cycles/75 hours is
 permitted if the axial length is less than 0.059 inch
 (1.5 mm).
 7)  Look for distortion to the leading and trailing edges and not in Area E. a) The maximum axial length is 0.197 inch (5 mm) and the
 maximum radial length is 0.59 inch (15 mm).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01.1 Page 612 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
LPC Blades and Vanes (1st- thru 4th-Stage) - Inspection
_______________________________________________________
 b)  A maximum service extension of 50 cycles/75 hours is permitted if the maximum circumference is 0.275 inch (7 mm) and the radial length is 0.708 inch (18 mm).
 8)  Look for deposits and erosion
 a) No maximum amount.

 (d) Examine the stator vanes as follows:
 NOTE: The limit to the vane inspection are the vanes you see
____ through the borescope viewer.
 NOTE: If damage is found, you must do a borescope inspection
____ of the downstream booster stages and the HPC.
 1) Look for missing pieces. a) A maximum of 20 vanes is permitted with these conditions:
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 ENGINE 發(fā)動機 1(18)