AIRFOIL LEADING OR TRAILING EDGE TIP CORNER
POSSIBLE AIRFOIL DAMAGE
NOTE: ALL DIMENSIONS ARE IN INCHES WITHGMM-1121724-01-A
MILLIMETERS IN PARENTHESES.
High Pressure Compressor Rotor Borescope Inspection
Figure 801 (Sheet 2)
G36082
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-00-00
ALL ú ú C01 Page 809 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
1132825-00-A
HPC Blade Borescope Blending Tool Figure 802 (Sheet 1)
G36088
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-00-00
ALL ú ú C01 Page 810 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
MOTOR SPEED
1132826-00-A
HPC Blade Borescope Blending ToolFigure 802 (Sheet 2)
G36134
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-00-00
ALL ú ú C01 Page 811 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TIP
GSM1140221-00-1
Blend Area Example Figure 803
G36181
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-00-00
ALL ú
ú C01 Page 812
ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
PRIMARY BLADE BLADE TIP ABRASIVE POLISHING MEASURING EDGE TIP BALL TIP BALL TIP GRIND TIP
SPANNER WRENCH (INSERTED IN SPINDLE)
GMM-1140222-00-A
Borescope Blend Tool Tip Selection/Blend Tip Installation
Figure 804
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-00-00
ALL ú ú C01 Page 813 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G36198
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FAN AND BOOSTER - DESCRIPTION AND OPERATION
___________________________________________
1. General
_______
A. The fan and booster (LPC) module is driven by the low pressure turbine and provides two separate air streams. The primary (or inner) air stream flows through the fan and booster section where the air is compressed for introduction into the high pressure compressor. The secondary (or outer) air stream is mechanically compressed by the fan as it enters the engine and is ducted to the outside of the core engine. This secondary air stream adds to the propulsive force generated by the core engine.
中國航空網 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 發動機 1(73)
