• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:35来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 607/TASK 27-84-62-991-014) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 607A/TASK 27-84-62-991-014-A)


 Slat 4, Track 9 - Attachment Details Figure 605/TASK 27-84-62-991-012
 1EFF : 1 1R 1CES  ALL  1 11 1 27-84-62 Page 611 Feb 01/01

 

 Slat 4, Track 10 - Attachment Details Figure 606/TASK 27-84-62-991-013
 1EFF : 1 1R 1CES  ALL  1 11 1 27-84-62 Page 612 Feb 01/01

 

 Slat 5, Track 11 - Attachment Details
 Figure 607/TASK 27-84-62-991-014

R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-84-62Page 613 1 1 May 01/05 1 1 1CES 1 Slat 5, Track 11 - Attachment Details Figure 607A/TASK 27-84-62-991-014-A


R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-62Page 614 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL


 (a)
 the nut (10), the locking plate (9), the nut (5), the washer (6), the bolt (12) and the eccentric bush (11).

 (b)
 the links (4) and (16) and the bolt (8). NOTE : The bolts (1) and (20) and their related nuts and washers


____ were removed when the Slat No. 5 was removed.
 (11) For the Slat track 12, remove:
 (Ref. Fig. 608/TASK 27-84-62-991-015)

 (a)
 the nut (11), the washer (10) and the bolt (30).

 (b)
 the nut (14), the washer (13), the bolt (29) and the links (8) and (31).

 (c)
 the nut (26), the locking plate (27), the nut (16), the washer (17), the bolt (25) and the eccentric bush (24).

 (d)
 the links (18) and (20) and the bolt (28). NOTE : The bolts (5) and (6) and their related nuts and washers


____ were removed when the Slat No. 5 was removed.
 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 601/TASK 27-84-62-991-008) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 601A/TASK 27-84-62-991-008-A)
 **ON A/C ALL

 (Ref. Fig. 602/TASK 27-84-62-991-009, 603/TASK 27-84-62-991-010, 604/TASK 27-84-62-991-011, 605/TASK 27-84-62-991-012, 606/TASK 27-84-62-991-013)


 Slat 5, Track 12 - Attachment Details Figure 608/TASK 27-84-62-991-015
 1EFF : 1 1R 1CES  ALL  1 11 1 27-84-62 Page 616 Feb 01/01

 

 **ON A/C 001-049, 051-061, 101-105, 201-203,
 (Ref. Fig. 607/TASK 27-84-62-991-014)

R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 607A/TASK 27-84-62-991-014-A)
 **ON A/C ALL
 (Ref. Fig. 608/TASK 27-84-62-991-015)
 Subtask 27-84-62-220-051
 A. Dimensional Check of Slat 2, Track 5
 (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 | 12.666 | 12.684 | | | 12.639 | | | | OD 1 |(0.4986) |(0.4993) | | |(0.4975) | | | | | | | 0.022 | 0.058 | | | 0.112 | | | | | (0.0008)| (0.0022)| | |(0.0044)| | B | 12.706 | 12.724 | | | | 12.751 | | | ID 2 |(0.5002) |(0.5009) | | | |(0.5020) | | ------------------------------------------------------------------------------- Subtask 27-84-62-220-052


 B. Dimensional Check of Slat 2, Track 5
 (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 | 12.666 | 12.684 | | | 12.653 | | | | OD 1 |(0.4986) |(0.4993) | | |(0.4981) | | | | | | | 0.003 | 0.034 | | | 0.060 | | | | | (0.0001)| (0.0013)| | |(0.0023)| | B | 12.687 | 12.700 | | | | 12.713 | | | ID 3 |(0.4994) |(0.5000) | | | |(0.5005) | | -------------------------------------------------------------------------------
 
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 FLIGHT CONTROLS 飞行操纵8(93)