71-00-02
ALL ú ú C10B Page 453 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
INBOARD AFT OUTBOARD AFT
BOOTSTRAP ARM BOOTSTRAP ARM
SHACKLE SHACKLE
DYNAMOMETER
SHACKLES
LEVER HOIST
CABLE
SHACKLE
CRADLE
TRANSPORTATION
BASE
PULLEYS
(VIEW IN THE FORWARD DIRECTION)
Aft Cradle Attach Points
Figure 414
C78309
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C10B Page 454 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FAN CASE
ATTACH POINT
FAN FRAME
ATTACH ROD
SEE A
FWD
BOLTS
(4 LOCATIONS)
B
ATTACH POINT FAN CASE SEE B FAN CASE ATTACH POINT
FAN FRAME
FAN FRAME ATTACH LINK FWD (REMOVE) BALL LOCK PIN ATTACH LINK FWD (INSTALL) BALL LOCK PIN
RETRACTED BALL LOCK EXTENDED BALL LOCK
PIN LOCATION PIN LOCATION
RETRACTED POSITION EXTENDED POSITION
A A
NOTE: RIGHT SIDE SHOWN LEFT SIDE EQUIVALENT.
Fan Case Attach Points to the Cradle Assembly Figure 415
C78312
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C10B Page 455 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Power Plant Removal - Bootstrap Method
______________________________________
Install the Bootstrap Equipment
3) Use the ball lock pins to connect the attach links (in the extended position) to the cradle.
NOTE: You may have to adjust the attitude of the
____ cradle assembly to get the correct alignment with the engine.
4) At four locations, attach the fan frame attach rod to the fan case attach point.
(b) Do these steps to attach the turbine frame to the cradle (Fig. 416): 1) Attach the turbine frame attach link to the turbine frame
attach point with a ball lock pin and a cotter pin. a) Use a pin and a cotter pin.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C11B Page 456 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TURBINE REAR FRAME
BALL LOCKPINCOTTER PIN
TURBINE FRAME ATTACH LINKS
SEE A
FWD
B
SEE B
ENGINE OUTBOARD TURBINE FRAME ATTACH LINKS
FWD
CRADLE ASSEMBLY
NOTE: OUTBOARD VIEW SHOWN.
A
INBOARD VIEW EQUIVALENT.
Turbine Frame Attach Point to the Cradle Assembly
Figure 416
C78318
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C09B Page 457 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Power Plant Removal - Bootstrap Method
______________________________________ Remove the Power Plant
F. Remove the Engine
S 494-045-C00
(1) Apply a preload to the hoists as follows:
中國航空網 m.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 動力裝置 POWER PLANT 1(124)
