(a)
Replace the bushes (Ref. TASK 52-10-00-915-001).
(b)
Or replace the parts on which they are installed.
(4)
If the link assembly (46) is worn or unserviceable:
(a) Replace the rod end of the link assembly (46).
(5)
If the bearings (40), (41) and (42) are worn or unserviceable:
(a) Replace the flange bearing assemblies (40), (41) and (42).
1EFF : ALL 1 52-13-22Page 613 1 1 Feb 01/98 1 1 1CES 1 Subtask 52-13-22-220-058
F. Inspection of the Escape Slide Control Mechanism
(Ref. Fig. 606/TASK 52-13-22-991-029)
(1)
Do a detailed visual inspection of the bearings, the link assemblies (at rod level) and the parts of the escape slide control mechanism.
(2)
Make sure that the dimensions are correct.
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | EE | | | | | | | | | OD51 | 15.882 | 15.893 | | | 15.870 | | | | | (0.6252)| (0.6257)| | | (0.6252)| | | | | | | 0.000 | 0.036 | | | 0.0072 | | | | | (0.0000)| (0.0014)| | |(0.0028)| | ID50 | 15.893 | 15.918 | | | | 15.942 | | | | (0.6257)| (0.6266)| | | |(0.6281) | | -------------------------------------------------------------------------------
(3)
If the wear of the bushes is not in the tolerances:
(a)
Replace the bushes (Ref. TASK 52-10-00-915-001).
(b)
Or replace the parts on which they are installed.
(4)
If the link assemblies (52), (53) and (54) are worn or unserviceable:
(a) Replace the rod end of the link assemblies (52), (53) and (54).
5. Close-up
________
Subtask 52-13-22-420-058
A. Installation of the Release Mechanism of the Emergency Escape Slide
(Ref. TASK 52-13-22-400-001)
(1)
Install the emergency control handle.
(2)
Install the escape slide gearbox.
1EFF : ALL 1 52-13-22Page 614 1 1 Feb 01/98 1 1 1CES 1
(3)
Install the percussion system.
(4)
Install the flexible control.
(5)
Install the telescopic forks and the girt bar control shaft.
(6) Install the escape slide control mechanism. Subtask 52-13-22-865-060
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
Subtask 52-13-22-410-065
C. Close Access
(1)
Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
(4)
Close the aft passenger/crew door 832 or 842 (Ref. TASK 52-10-00-410-001).
(5) Remove the access platform(s). Subtask 52-13-22-862-050
D. De-energize the ground service network
(Ref. TASK 24-42-00-862-001)
1EFF : ALL 1 52-13-22Page 615 1 1 Feb 01/98 1 1 1CES 1
Escape Slide Control Mechanism
Figure 606/TASK 52-13-22-991-029- 12 (SHEET 1)
1EFF : ALL 1 52-13-22 Page 616
1 1 Feb 01/98
1 1
1CES 1
Escape Slide Control Mechanism
Figure 606/TASK 52-13-22-991-029- 22 (SHEET 2)
1EFF : ALL 1 52-13-22 Page 617
1 1 Feb 01/98
1 1
1CES 1
LATCH AND STOP FITTINGS - DOOR - REMOVAL/INSTALLATION
_____________________________________________________
TASK 52-13-31-000-001
Removal of the Lining Flap
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門2(157)
