3. Job Set-up
__________
Subtask 52-32-11-860-057
A. Aircraft Maintenance Configuration
(1)
Make sure that the AFT cargo compartment door (referred to as cargo door) is closed and locked (Ref. TASK 52-30-00-860-001).
(2)
Put the access platform in position below the closed cargo door.
(3)
Remove the access panel 826AR from the cargo door.
(4)
Disassmble the locking handle mechanisn from the locking shaft (Ref. TASK 52-32-21-000-001).
(5)
Remove the handle flap mechanism from the cargo door (Ref. TASK 52-32-21-000-002).
(6)
Attach the cargo door to the crane to take the load from the hinge pins (Ref. TASK 52-31-11-000-001).
4. Procedure
_________
Subtask 52-32-11-220-050
A. Measurement of the Deflection Unit
(Ref. Fig. 608/TASK 52-32-11-991-001)
-------------------------------------------------------------------------------| 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-C | 7.912 | 7.922 | | | 7.900 | | | | OD 1 |(0.3114) |(0.3118) | | |(0.3110) | | | | | | | 0.008 | 0.033 | | | 0.066 | | | | | (0.0003)| (0.0012)| | |(0.0025)| | C-C | 7.930 | 7.945 | | | | 7.966 | | | ID 2 |(0.3122) |(0.3127) | | | |(0.3136) | | -------------------------------------------------------------------------------
1EFF : 051-052, 1 52-32-11Page 658 1 1 Aug 01/05R 1 1 1CES 1
Fit and Clearances of the Locking Handle Mechanism
Figure 608/TASK 52-32-11-991-001
1EFF : 051-052, 1 52-32-11Page 659 1 1 Aug 01/05R 1 1 1CES 1
Subtask 52-32-11-220-051
B. Measurement of the Locking Handle Mechanism
(Ref. Fig. 608/TASK 52-32-11-991-001)
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | D-D | 6.336 | 6.345 | | | 6.315 | | | | OD 3 |(0.2494) |(0.2498) | | |(0.2486) | | | | | | | 0.005 | 0.029 | | | 0.071 | | | | | (0.0001)| (0.0011)| | |(0.0027)| | D-D | 6.350 | 6.365 | | | | 6.386 | | | ID 4 |(0.2500) |(0.2505) | | | |(0.2514) | | -------------------------------------------------------------------------------
Subtask 52-32-11-220-052
C. Measurement of the Handle Flap Mechanism
(Ref. Fig. 609/TASK 52-32-11-991-002)
-------------------------------------------------------------------------------| 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-C | 6.336 | 6.345 | | | 6.323 | | | | OD 1 |(0.2494) |(0.2498) | | |(0.2489) | | | | | | | 0.005 | 0.029 | | | 0.063 | | | | | (0.0001)| (0.0011)| | |(0.0024)| | C-C | 6.350 | 6.365 | | | | 6.386 | | | ID 2 |(0.2500) |(0.2505) | | | |(0.2514) | | ------------------------------------------------------------------------------- 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 DOORS 舱门5(57)