Subtask 27-84-61-220-055
D. Dimensional Check of the Slat-to-Track Attachment Fittings, Track 1 thru 4
(1) Fits and clearance dimensions
NOTE : The limits on the chrome-plated surfaces only apply when there
____ is a layer of chrome on the bearing surfaces.
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B | 19.009 | 19.030 | | | 18.993 | | | | OD 9 |(0.7483) |(0.7492) | | |(0.7477) | | | | | | | 0.007 | 0.041 | | | 0.073 | | | | | (0.0002)| (0.0016)| | |(0.0028)| | B | 19.037 | 19.050 | | | | 19.066 | | | ID 8 |(0.7494) |(0.7500) | | | |(0.7506) | | -------------------------------------------------------------------------------
Subtask 27-84-61-220-056
E. Dimensional Check of the Slat-to-Track Attachment Fittings, Track 1 thru 4
(1) Fits and clearance dimensions
NOTE : The limits on the chrome-plated surfaces only apply when there
____ is a layer of chrome on the bearing surfaces.
1EFF : ALL 1 27-84-61Page 609 1 1 Feb 01/01R 1 1 1CES 1
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| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C | 19.009 | 19.030 | | | 18.977 | | | | OD 33 |(0.7483) |(0.7492) | | |(0.7471) | | | | | | | 0.027 | 0.069 | | | 0.133 | | | | | (0.0010)| (0.0027)| | |(0.0052)| | C | 19.057 | 19.078 | | | | 19.110 | | | ID 11 |(0.7502) |(0.7511) | | | |(0.7523) | | -------------------------------------------------------------------------------
Subtask 27-84-61-220-057
F. Dimensional Check of the Slat-to-Track Attachment Fittings, Track 1 thru 4
(1) Fits and clearance dimensions
NOTE : The limits on the chrome-plated surfaces only apply when there
____ is a layer of chrome on the bearing surfaces.
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C | 19.009 | 19.030 | | | 18.993 | | | | OD 33 |(0.7483) |(0.7492) | | |(0.7477) | | | | | | | 0.007 | 0.041 | | | 0.073 | | | | | (0.0002)| (0.0016)| | |(0.0028)| | C | 19.037 | 19.050 | | | | 19.066 | | | ID 12 |(0.7494) |(0.7500) | | | |(0.7506) | | -------------------------------------------------------------------------------
1EFF : ALL 1 27-84-61Page 610 1 1 Feb 01/01R 1 1 1CES 1
Subtask 27-84-61-220-058
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(72)
