-------------------------------------------------------------------------------| 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 | 22.959 | 22.980 | | | 22.932 | | | | OD 23 |(0.9038) |(0.9047) | | |(0.9028) | | | | | | | 0.020 | 0.062 | | | 0.116 | | | | | (0.0007)| (0.0024)| | |(0.0045)| | C | 23.000 | 23.021 | | | | 23.048 | | | ID 19 |(0.9055) |(0.9063) | | | |(0.9074) | | -------------------------------------------------------------------------------
Subtask 27-84-61-220-072
W. 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 20 |(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 22 |(0.7494) |(0.7500) | | | |(0.7506) | | -------------------------------------------------------------------------------
1EFF : ALL 1 27-84-61Page 620 1 1 Feb 01/01R 1 1 1CES 1
Subtask 27-84-61-220-073
X. 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 | | | 18.982 | | | | OD 20 |(0.7483) |(0.7492) | | |(0.7473) | | | | | | | 0.020 | 0.062 | | | 0.116 | | | | | (0.0007)| (0.0024)| | |(0.0045)| | C | 19.050 | 19.071 | | | | 19.098 | | | ID 21 |(0.7500) |(0.7508) | | | |(0.7518) | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 27-84-61-640-057
A. Application of Special Materials
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 601/TASK 27-84-61-991-007)
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 601A/TASK 27-84-61-991-007-A)R **ON A/C ALL
(1) For the Slat tracks 1 and 2, apply a layer of COMMON GREASE (Material No. 04-024) to: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(76)
