(2)
Put a warning notice in position to tell persons not to operate the flight controls.
Subtask 27-64-45-010-051
B. Get Access
(1) Remove the spoiler 5 (Ref. TASK 27-64-45-000-001).
4. Procedure
_________
**ON A/C 001-003, 051-052,
(Ref. Fig. 601/TASK 27-64-45-991-003)R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 601A/TASK 27-64-45-991-003-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.
Subtask 27-64-45-220-051
A. Dimensions of the Spoiler 5
NOTE : Limits on chrome plated items only apply when there is a layer of
____
chrome remaining on the bearing surfaces.
(1) Complete an inspection of these dimensions.
-------------------------------------------------------------------------------| 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 | 7.899 | 7.924 | | | 7.880 | | | | OD 1 |(0.3109) |(0.3120) | | |(0.3102) | | | | | | | 0.000 | 0.038 | | | 0.076 | | | | | (0.0000)| (0.0015)| | |(0.0029)| | B | 7.924 | 7.937 | | | | 7.956 | | | ID 2 |(0.3120) |(0.3125) | | | |(0.3132) | | -------------------------------------------------------------------------------
Spoiler 5
Figure 601/TASK 27-64-45-991-003- 12 (SHEET 1)
R 1EFF : 001-003, 051-052, 1 27-64-45Page 604 1 1 May 01/05 1 1 1CES 1
Spoiler 5
Figure 601/TASK 27-64-45-991-003- 22 (SHEET 2)
R 1EFF : 001-003, 051-052, 1 27-64-45Page 605 1 1 May 01/05 1 1 1CES 1
Spoiler 5 Figure 601A/TASK 27-64-45-991-003-A
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-64-45Page 606 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 27-64-45-220-052
B. Dimemsions of the Spoiler 5
NOTE : Limits on chrome plated items only apply when there is a layer of
____
chrome remaining on the bearing surfaces.
(1) Complete an inspection of these dimensions.
-------------------------------------------------------------------------------| 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 | 25.380 | 25.393 | | | 25.350 | | | | OD 2 |(0.9992) |(0.9997) | | |(0.9980) | | | | | | | 0.007 | 0.053 | | | 0.113 | | | | | (0.0002)| (0.0020)| | |(0.0044)| | C | 25.400 | 25.433 | | | | 25.463 | | | ID 1 |(1.0000) |(1.0012) | | | |(1.0024) | | -------------------------------------------------------------------------------
Subtask 27-64-45-220-053
C. Dimensions of the Spoiler 5
NOTE : Limits on chrome plated items only apply when there is a layer of
____
chrome remaining on the bearing surfaces.
(1) Complete an inspection of these dimensions.
1EFF : ALL 1 27-64-45Page 607 1 1 Feb 01/03R 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 | 19.030 | 19.043 | | | 19.000 | | | | OD 3 |(0.7492) |(0.7497) | | |(0.7480) | | | | | | | 0.007 | 0.053 | | | 0.113 | | | | | (0.0002)| (0.0020)| | |(0.0044)| | C | 19.050 | 19.083 | | | | 19.113 | | | ID 2 |(0.7500) |(0.7512) | | | |(0.7524) | | -------------------------------------------------------------------------------
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7(7)
