A320飞机维护手册 AMM DOORS 舱门8(103)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Subtask 52-81-00-220-061
 M. Dimensional Check of the Forward Hinge Assembly
 (1) Between the outer dimension of the bolt (10) and the inner dimension of the spacer (13).
 -------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 15.841 | 15.859 | | | 15.807 | | | | OD 10 |(0.6236) |(0.6243) | | |(0.6223) | | | | | | | 0.016 | 0.052 | | | 0.120 | | | | | (0.0006)| (0.0020)| | |(0.0047)| | F | 15.875 | 15.893 | | | | 15.927 | | | ID 13 |(0.6250) |(0.6257) | | | |(0.6270) | | -------------------------------------------------------------------------------
Subtask 52-81-00-220-062
 N. Dimensional Check of the Forward Hinge Assembly
 (1) Between the outer dimension of the spacer (13) and the inner dimension of the bush (12).
 1EFF : ALL 1 52-81-00Page 615 1 1 Feb 01/98 1 1 1CES 1

 -------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 19.959 | 19.980 | | | 19.918 | | | | OD 13 |(0.7857) |(0.7866) | | |(0.7841) | | | | | | | 0.020 | 0.062 | | | 0.144 | | | | | (0.0007)| (0.0024)| | |(0.0056)| | F | 20.000 | 20.021 | | | | 20.062 | | | ID 12 |(0.7874) |(0.7882) | | | |(0.7898) | | -------------------------------------------------------------------------------
Subtask 52-81-00-220-063
 P. Dimensional Check of the Forward Hinge Assembly
 (1) Between the outer dimension of the bush (12) and the inner dimension of the fitting (14).
 -------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 24.080 | 24.100 | | | 24.080 | | | | OD 12 |(0.9480) |(0.9488) | | |(0.9480) | | | | | | | -0.100 | -0.059 | | | 0.059 | | | | |-(0.0039)|-(0.0023)| | |(0.0023)| | F | 24.000 | 24.021 | | | | 24.021 | | | ID 14 |(0.9448) |(0.9457) | | | |(0.9457) | | -------------------------------------------------------------------------------
Subtask 52-81-00-220-064
 Q. Dimensional Check of the Forward Hinge Assembly
 (1) Between the outer dimension of the bearing (16) and the inner dimension of the hinge assembly (15).
 1EFF : ALL 1 52-81-00Page 616 1 1 Feb 01/98 1 1 1CES 1

 -------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 30.150 | 30.163 | | | 30.134 | | | | OD 16 |(1.1870) |(1.1875) | | |(1.1863) | | | | | | | -0.003 | 0.035 | | | 0.067 | | | | |-(0.0001)| (0.0013)| | |(0.0026)| | F | 30.160 | 30.185 | | | | 30.201 | | | ID 15 |(1.1874) |(1.1883) | | | |(1.1890) | | -------------------------------------------------------------------------------
Subtask 52-81-00-220-076
 R. Not Applicable. Subtask 52-81-00-220-077
 S. Not Applicable. Subtask 52-81-00-220-078
 T. Not Applicable. Subtask 52-81-00-220-079
 U. Not Applicable. Subtask 52-81-00-220-080
 V. Not Applicable. Subtask 52-81-00-220-081
 W. Not Applicable. Subtask 52-81-00-220-082
 X. Not Applicable. Subtask 52-81-00-220-083
 Y. Not Applicable.
 1EFF : ALL 1 52-81-00Page 617 1 1 Feb 01/98 1 1 1CES 1 Subtask 52-81-00-220-065
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门8(103)