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时间:2011-04-09 10:08来源:蓝天飞行翻译 作者:航空
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3
UPPER LOCKING ACTUATOR
CLEARANCE FOR THE NONLOCKING ACTUATORS
3 IS 0.0-0.080 INCH (0.0-2.0 mm) A-A
Thrust Reverser System - Inspection/Check Figure 601 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-31-00
 ALL  ú ú C01 Page 605 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

Thrust Reverser System - Inspection/Check
Figure 601 (Sheet 5)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-31-00
 ALL  ú ú C01 Page 606 ú Jul 15/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////


(-77 OPTIONAL)
C-C
LAMINATED SHIM BONDED TO STRUCTURE
SOLID SHIM (-39) AND LAMINATED SHIM (-40) BONDED TOGETHER AND THEN BONDED TO STRUCTURE
Thrust Reverser System - Inspection/Check Figure 601 (Sheet 6)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT VIBRATION ISOLATOR ú

 78-31-00
 COWL SUSPENSION  ú ú C01 Page 607 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

D-D


LAMINATED SHIM COMPRESSION PAD AND SHIM E-E E-E

LAMINATED SHIM BONDED TO STRUCTURE COMPRESSION PAD (-21) AND SOLID SHIM (-22) Thrust Reverser System - Inspection/Check Figure 601 (Sheet 7)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT VIBRATION ISOLATOR ú

 78-31-00
 COWL SUSPENSION  ú ú C01 Page 608 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

SOLID SHIM COMPRESSION PAD AND SHIM G-G G-G

SOLID SHIM BONDED TO STRUCTURE
COMPRESSION PAD (-28) AND SOLID SHIM (-20). THE SOLID SHIM (-20) IS INSTALLED WITH BMS 10-11, TYPE I
Thrust Reverser System - Inspection/Check
Figure 601 (Sheet 8)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT VIBRATION ISOLATOR ú

 78-31-00
 COWL SUSPENSION  ú ú C01 Page 609 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////


J-J
LAMINATED SHIM BONDED TO STRUCTURE
SOLID SHIM (-39) AND LAMINATED SHIM (-40) BONDED TOGETHER AND THEN BONDED TO STRUCTURE
Thrust Reverser System - Inspection/Check Figure 601 (Sheet 9)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH VIBRATION ISOLATOR COWL ú

 78-31-00
 SUSPENSION  ú
 ú C01 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.  Page 610Mar 15/95 

////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

UPPER COMPRESSION PAD
NAC STA 233.15
K-K


315A1921-1 COMPRESSION PAD L-L
Thrust Reverser System - Inspection/Check
 
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