Subtask 27-84-62-220-112
BP. Dimensional Check of Slat 5, Track 11
(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 | 9.497 | 9.512 | | | 9.473 | | | | OD 20 |(0.3738) |(0.3744) | | |(0.3729) | | | | | | | 0.018 | 0.055 | | | 0.103 | | | | | (0.0007)| (0.0021)| | |(0.0040)| | C | 9.530 | 9.552 | | | | 9.576 | | | ID 17 |(0.3751) |(0.3760) | | | |(0.3770) | | -------------------------------------------------------------------------------
Subtask 27-84-62-220-113
BQ. Dimensional Check of Slat 5, Track 11
(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 27-84-62Page 658 1 1 Feb 01/01R 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C | 9.497 | 9.512 | | | 9.489 | | | | OD 20 |(0.3738) |(0.3744) | | |(0.3735) | | | | | | | 0.000 | 0.028 | | | 0.044 | | | | | (0.0000)| (0.0011)| | |(0.0017)| | C | 9.512 | 9.525 | | | | 9.533 | | | ID 21 |(0.3744) |(0.3750) | | | |(0.3753) | | -------------------------------------------------------------------------------
Subtask 27-84-62-220-114
BR. Dimensional Check of Slat 5, Track 11
(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 | 9.497 | 9.512 | | | 9.478 | | | | OD 20 |(0.3738) |(0.3744) | | |(0.3731) | | | | | | | 0.013 | 0.043 | | | 0.081 | | | | | (0.0005)| (0.0016)| | |(0.0031)| | C | 9.525 | 9.540 | | | | 9.559 | | | ID 19 |(0.3750) |(0.3755) | | | |(0.3763) | | -------------------------------------------------------------------------------
1EFF : ALL 1 27-84-62Page 659 1 1 Feb 01/01R 1 1 1CES 1
Subtask 27-84-62-220-115
BS. Dimensional Check of Slat 5, Track 12
(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 | 11.079 | 11.097 | | | 11.062 | | | | OD 6 |(0.4361) |(0.4368) | | |(0.4355) | | | | | | | -0.001 | 0.035 | | | 0.069 | | | | |-(0.0000*| (0.0013*| | |(0.0027*| | B | 11.096 | 11.114 | | | | 11.131 | | | ID 2 |(0.4368) |(0.4375) | | | |(0.4382) | | ********** DIFFERENCE IN IN. MARKED BY A STAR IS TRUNCATED **********
中國航空網(wǎng) 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(107)
