In the AFT cargo compartment:
-
the cursor of the test tool shouldreach in the green area.
On the hatch structure:
-
the latch pin retracts to theDISARMED position.
In the center of the cabin:
-
the opening of the emergency exit isclosed.
-
the latch pin extends in its ARMEDposition and operates the pin of therelated proximity switch.
-
the white indication light SLIDE ARMED comes on.
-
the white indicator light SLIDE ARMEDgoes off.
-make sure that the position of thehatch seal is correct.
A. Put the aircraft back to the serviceable condition. **ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 501/TASK 52-21-00-991-001)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 523 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **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,
(1) Remove the TEST TOOL - RELEASE CABLE , ESCAPE SLIDE (TLW101) 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)
Loosen the knurled sleeve nut and disassemble the two collets from the flexible control assembly.
(b)
Disengage the adapter from the release cable.
(2) Connect the flexible control assembly with the inflation reservoir 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)
Engage the inflation cable with the release cable.
(b)
Put the collets in position and tighten the knurled sleeve nut.
(c)
Safety the knurled sleeve nut with the lockwire,corrosion-resistance steel, dia.0.8mm.
(3) Remove the lockpin assembly from the operating head of the inflation reservoir and put it into its bag (Ref. TASK 25-62-00-081-001).
Subtask 52-21-00-410-055
B. Close Access
(1)
Install the linings 151CW and 152CW of the AFT cargo compartment.
(2)
Close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002).
(3)
Remove the access platform(s).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 524 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 52-21-00-710-005
Operational Test of the Emergency Exit Hatch and Escape Slide Arming and
Disarming
WARNING : MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY INSTALLED IN THE
_______
REGULATOR VALVE ASSEMBLY OF THE INFLATION RESERVOIR.
THIS PREVENTS ACCIDENTAL:
-DISCHARGE OF THE INFLATION RESERVOIR
-DEPLOYMENT OF THE ESCAPE-SLIDE
WHICH CAN CAUSE INJURY AND/OR DAMAGE.
1. Reason for the Job
__________________
Refer to the MPD TASK: 522100-08 To make sure that the removal of each emergency exit hatch (referred to as hatch) with a retracted latch pin (Disarmed Mode) is possible.
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
25-62-00-081-001 Special Precautions after Work on the Offwing
Escape-Slide Systems
25-62-00-481-001 Special Precautions before Work on the Offwing
Escape-Slide Systems
52-21-11-400-001 Installation of the Emergency Exit Hatch
**ON A/C 001-049, 051-099, 101-149, 201-299,
52-21-00-991-001 Fig. 501
R **ON A/C 151-199, 401-499,
52-21-00-991-001-A Fig. 501A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 525 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
中國航空網(wǎng) www.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(24)
