(2)
Install the lockpin assembly in the operating head of the inflation reservoir to prevent an accidental operation of the inflation reservoir (Ref. TASK 25-62-00-481-001).
(3)
Remove the inflation reservoir assembly from the flexible control assembly as follows:
CAUTION : DO NOT PUSH THE END OF THE WIRE INTO THE WIRE-CONTROL
_______ ASSEMBLY. THIS CAN CAUSE A KINK IN THE WIRE.
(a)
Remove and discard the lockwire from the knurled sleeve nut (2).
(b)
Loosen the knurled sleeve nut and disassemble the two collets from the flexible control assembly.
(c)
Disconnect the inflation cable from the release cable.
(4) Install the TEST TOOL - RELEASE CABLE , ESCAPE SLIDE (TLW101) on the flexible control assembly as follows:
CAUTION : DO NOT PUT WEIGHT ON THE FWD PULLEY WHEN YOU CONNECT THE
_______ WIRE- CONTROL ASSEMBLY TO THE FLEXIBLE CONTROL-ASSEMBLY. WEIGHT ON THE PULLEY CAUSES TENSION IN THE WIRE, WHICH CAN CAUSE THE END OF THE WIRE TO BREAK.
(a) Remove the cover cap from the test tool.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 514 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(b)
Engage the adapter with the release cable and put the collets in position around the joint.
(c)
Turn the knurled sleeve nut to safety the connection of the test tool and the flexible control assembly.
(d)
Set the cursor of the test tool to zero.
(5) Make sure that the skin offset and the lateral clearances of the hatch are correctly adjusted (Ref. TASK 52-21-11-820-001).
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 501/TASK 52-21-00-991-001) R **ON A/C 151-199, 401-499,
(Ref. Fig. 501A/TASK 52-21-00-991-001-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 52-21-00-720-050
A. Functional Test of the Automatic Slide Release Signal
(1) Do this test to examine:
-
the automatic operation of the slide release mechanism during the removal of the hatches,
-
the manual operation of the slide release mechanism,
-
the operation of the hatch locking mechanism from the inner and the outer side.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 515 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. In the center of the cabin:
-
pull down and remove the cover flap from the hatch.
-
pull the pull-lever of the hatch control handle down and hold the hatch in position.
-carefully lower the top of the hatch into the cabin until it comes free of the cabin lining.
R R R - remove the hatch from the opening.
2. In the AFT cargo compartment:
- measure the travel of the release cable with the test tool.
- adjust the cursor of the test tool to zero.
3. In the center of the cabin:
In the center of the cabin:
-
the white indicator light SLIDE ARMEDcomes on.
-
the hooks of the locking mechanismdisengage from the upper rollerfittings.
-
the linkage of the hatch control handle locks the pull lever in this lower position.
-
the extended latch pin moves therelease lever of the slide releasemechanism to its end position.
-
the flexible control assembly of the slide release mechanism transmits this movement (as the automatic slide release signal) to the inflation reservoir in the AFT cargo compartment.
-
the white indicator light SLIDE ARMED goes off.
In the AFT cargo compartment:
-
the end of the release cable retracts and operates the spring-loaded test tool.
-
the latch pin disengages from the release lever.
In the AFT cargo compartment:
-
the cursor on the scale of the testtool should reach the green area atmin. 50.0 mm (1.9685 in.).
In the AFT cargo compartment:
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 516 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- remove the red pull handle of - the end of the release cable retracts
the slide release mechanism and operates the spring-loaded test
from its stowage position and tool.
pull it down (manual operation
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3(21)
