-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 1.5738 | 1.5742 | | | 1.5731 | | | | OD 1 |(39.974) |(39.984) | | |(39.956) | | | | | | | 0.0006 | 0.0019 | | | 0.0040| | | | | (0.015) | (0.048) | | |(0.101) | | A | 1.5748 | 1.5757 | | | | 1.5771 | | | ID 3 |(39.999) |(40.022) | | | |(40.058) | | -------------------------------------------------------------------------------
Subtask 54-51-17-220-053
E. Inspection of the Pylon-to-Wing Forward Attach-Fitting
(1) Do a detailed inspection of the pylon-to-wing forward attach-fitting and make sure that the dimensions are correct. (Ref. Fig. 602/TASK 54-51-17-991-009)
-------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 1.7340 | 1.7346 | | | 1.7337 | | | | OD 2 |(44.043) |(44.058) | | |(44.035) | | | | | | | -0.0023 | -0.0007 | | | 0.0000| | | | |-(0.058) |-(0.017) | | |(0.000) | | A | 1.7323 | 1.7333 | | | | 1.7337 | | | ID 7 |(44.000) |(44.025) | | | |(44.035) | | -------------------------------------------------------------------------------
Subtask 54-51-17-220-054
F. Inspection of the Pylon-to-Wing Forward Attach-Fitting
(1) Do a detailed inspection of the pylon-to-wing forward attach-fitting and make sure that the dimensions are correct. (Ref. Fig. 602/TASK 54-51-17-991-009)
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 1.7340 | 1.7346 | | | 1.7337 | | | | OD 4 |(44.043) |(44.058) | | |(44.035) | | | | | | | -0.0023 | -0.0007 | | | 0.0000| | | | |-(0.058) |-(0.017) | | |(0.000) | | A | 1.7323 | 1.7333 | | | | 1.7337 | | | ID 5 |(44.000) |(44.025) | | | |(44.035) | | -------------------------------------------------------------------------------
Subtask 54-51-17-220-055
G. Inspection of the Pylon-to-Wing Forward Attach-Fitting
(1) Do a detailed inspection of the pylon-to-wing forward attach-fitting and make sure that the dimensions are correct. (Ref. Fig. 602/TASK 54-51-17-991-009)
-------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 1.7340 | 1.7346 | | | 1.7337 | | | | OD 4 |(44.043) |(44.058) | | |(44.035) | | | | | | | -0.0023 | -0.0007 | | | 0.0000| | | | |-(0.058) |-(0.017) | | |(0.000) | | A | 1.7323 | 1.7333 | | | | 1.7337 | | | ID 6 |(44.000) |(44.025) | | | |(44.035) | | -------------------------------------------------------------------------------
Subtask 54-51-17-220-056
H. Inspection of the Pylon-to-Wing Forward Attach-Fitting
(1) Do a detailed inspection of the pylon-to-wing forward attach-fitting and make sure that the dimensions are correct. (Ref. Fig. 602/TASK 54-51-17-991-009)
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 1.7340 | 1.7346 | | | 1.7337 | | | | OD 3 |(44.043) |(44.058) | | |(44.035) | | | | | | | -0.0023 | -0.0007 | | | 0.0000| | | | |-(0.058) |-(0.017) | | |(0.000) | | A | 1.7323 | 1.7333 | | | | 1.7337 | | | ID 5 |(44.000) |(44.025) | | | |(44.035) | | -------------------------------------------------------------------------------
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 NACELLES/PYLONS(64)