(Ref. Fig. 601A/TASK 27-54-62-991-046-A)
**ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-62-220-065
A. Dimensions of the Joint that Connect the Actuator Lever to the Drive Strut (Tracks 3 and 4).
(1) Do a check of the dimensions that follow:
Outboard Flap - Fits and Clearances (Tracks 3 and 4)
Figure 601/TASK 27-54-62-991-046
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-62Page 604 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Outboard Flap - Fits and Clearances (Tracks 3 and 4) R Figure 601A/TASK 27-54-62-991-046-A
R 1EFF : 301-399, 1 27-54-62Page 605 1 1 May 01/04 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 15.841 | 15.859 | | | 15.807 | | | | OD 1 |(0.6236) |(0.6243) | | |(0.6223) | | | | | | | 0.016 | 0.052 | | | 0.120 | | | | | (0.0006)| (0.0020)| | |(0.0047)| | A | 15.875 | 15.893 | | | | 15.927 | | | ID 2 |(0.6250) |(0.6257) | | | |(0.6270) | | -------------------------------------------------------------------------------
Subtask 27-54-62-220-066
B. Dimensions of the Joint that Connects the Actuator Lever to the Drive Strut (Tracks 3 and 4).
(1) Do a check of the dimensions that follow:
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 15.841 | 15.859 | | | 15.822 | | | | OD 1 |(0.6236) |(0.6243) | | |(0.6229) | | | | | | | 0.003 | 0.034 | | | 0.072 | | | | | (0.0001)| (0.0013)| | |(0.0028)| | A | 15.862 | 15.875 | | | | 15.894 | | | ID 4 |(0.6244) |(0.6250) | | | |(0.6257) | | -------------------------------------------------------------------------------
Subtask 27-54-62-220-067
C. Dimensions of the Joint that Connects the Actuator Lever to the Drive Strut (Tracks 3 and 4).
(1) Do a check of the dimensions that follow:
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-62Page 606 1201-299, 401-499, 1Aug 01/05 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 15.841 | 15.859 | | | 15.781 | | | | OD 1 |(0.6236) |(0.6243) | | |(0.6212) | | | | | | | 0.046 | 0.074 | | | 0.194 | | | | | (0.0018)| (0.0029)| | |(0.0076)| | A | 15.905 | 15.915 | | | | 15.975 | | | ID 5 |(0.6261) |(0.6265) | | | |(0.6289) | | -------------------------------------------------------------------------------
Subtask 27-54-62-220-068
D. Dimensions of the Joint that Connects the Actuator Lever to the Drive Strut (Tracks 3 and 4).
(1) Do a check of the dimensions that follow:
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 20.959 | 20.980 | | | 20.918 | | | | OD 2 |(0.8251) |(0.8259) | | |(0.8235) | | | | | | | 0.020 | 0.062 | | | 0.144 | | | | | (0.0007)| (0.0024)| | |(0.0056)| | A | 21.000 | 21.021 | | | | 21.062 | | | ID 3 |(0.8267) |(0.8275) | | | |(0.8292) | | -------------------------------------------------------------------------------
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6(87)
