(2) Make sure that the dimensions are correct.
 -------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | CC | | | | | | | | | OD11 | 15.882 | 15.893 | | | 15.870 | | | | | (0.6252)| (0.6257)| | | (0.6252)| | | | | | | 0.000 | 0.036 | | | 0.036 | | | | | (0.0000)| (0.0014)| | |(0.0028)| | ID10 | 15.893 | 15.918 | | | | 15.942 | | | | (0.6257)| (0.6267)| | | |(0.6281) | | |--------|---------|---------|---------|---------|---------|---------|--------| | CC | | | | | | | | | OD13 | 19.057 | 19.070 | | | 19.042 | | | | | (0.7502)| (0.7508)| | | (0.7496)| | | | | | | 0.000 | 0.044 | | | 0.048 | | | | | (0.0000)| (0.0017)| | |(0.0034)| | ID12 | 19.070 | 19.101 | | | | 19.130 | | | | (0.7508)| (0.7520)| | | |(0.7531) | | |--------|---------|---------|---------|---------|---------|---------|--------| | CC | | | | | | | | | OD19 | 15.882 | 15.893 | | | 15.870 | | | | | (0.6252)| (0.6257)| | | (0.6252)| | | | | | | 0.000 | 0.036 | | | 0.036 | | | | | (0.0000)| (0.0014)| | |(0.0028)| | ID20 | 15.893 | 15.918 | | | | 15.942 | | | | (0.6257)| (0.6267)| | | |(0.6281) | | |--------|---------|---------|---------|---------|---------|---------|--------| | DD | | | | | | | | | OD22 | 12.700 | 12.715 | | | 12.686 | | | | | (0.5000)| (0.5006)| | | (0.4994)| | | | | | | 0.000 | 0.041 | | | 0.0082 | | | | | (0.0000)| (0.0016)| | |(0.0032)| | ID21 | 12.715 | 12.741 | | | | 12.768 | | | | (0.5006)| (0.5021)| | | |(0.5026) | | |--------|---------|---------|---------|---------|---------|---------|--------| | DD | | | | | | | | | OD23 | 12.704 | 12.715 | | | 12.691 | | | | | (0.5001)| (0.5006)| | | (0.4996)| | | | | | | 0.000 | 0.0037 | | | 0.074 | | | | | (0.0000)| (0.0014)| | |(0.0029)|
 1EFF : ALL 1 52-11-14Page 613 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | ID24 | 12.715 | 12.741 | | | | 12.765 | | | | (0.5006)| (0.5021)| | | |(0.5025) | | -------------------------------------------------------------------------------

R (3) If the wear of the bushings is not in the tolerances.
R (a) Replace the bushings (Ref. TASK 52-10-00-915-001).
 (b) Or replace the parts on which they are installed.
 5. Close-up
________
 Subtask 52-11-14-420-064
 A. Installation of the Door-Damper and Emergency-Operation Cylinder
 (1)
 Install the door-damper and emergency-operation cylinder (Ref. TASK 52-11-14-400-001).

 (2)
 Install the telescopic rod (Ref. TASK 52-11-14-400-001).

 Subtask 52-11-14-865-073
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
 Subtask 52-11-14-410-076
 C. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 1EFF : ALL 1 52-11-14Page 614 1 1 Aug 01/00 1 1 1CES 1

 (4) Close the FWD passenger/crew door 831 or 841 (Ref. TASK 52-10-00-410-
001).
 (5) Remove the access platform(s). Subtask 52-11-14-862-053
 D. De-energize the ground service network (Ref. TASK 24-42-00-862-001)
 1EFF : ALL 1 52-11-14Page 615 1 1 Feb 01/98 1 1 1CES 1

 SEAL - DOOR - REMOVAL/INSTALLATION
__________________________________ TASK 52-11-18-000-001 Removal of the Door Seal
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門1(160)