曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 of the offwing escape slide).  In the center of the cabin:
 - release the red pull handle and  - the release lever moves automatically
 set it back in its stowage  to its normal position.
 position.
 4. On the hatch structure:  On the hatch structure:
 - push the latch pin against the  - the latch pin retracts to the
 spring and turn its head a  DISARMED position.
 quarter turn counterclockwise.
 5. In the center of the cabin:  In the center of the cabin:
 - install the hatch correctly  - the opening of the emergency exit is
 (Ref. TASK 52-21-11-400-001).  closed.
 - push the latch pin against the  - the latch pin extends in its ARMED
 spring and turn its head a  position and operates the pin of the
 quarter turn clockwise.  related proximity switch.
 - the white indicator light SLIDE ARMED
 comes on.
 - install the cover flap on the  - the white indicator light SLIDE ARMED
 hatch lining and push it  goes off.
 against the hatch.
 - examine the position of the  - make sure that the position of the
 hatch seal.  hatch seal is correct.
 5. Close-up________
 Subtask 52-21-00-860-056

 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 517 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 52-21-00-410-051
 B. Close Access
 (1)
 Install the linings 151CW and 152CW in 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 518 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 52-21-00-710-004

 Operational Test of the Unlocking and the Opening from the Outer Side in the ARMED Mode
 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: 522100-07
 To make sure that the locking mechanism and the slide release mechanism of
 each emergency exit hatch (referred to as hatch) operates satisfactorily.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 2.0 m (6 ft. 7 in.) TLW101 1 TEST TOOL - RELEASE CABLE , ESCAPE SLIDE
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire,corrosion-resistance steel, dia.0.8mm
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 519 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
　
中國航空網 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(22)