1.
Reason for the Job
__________________
Refer to the MPD TASK: 522100-01
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 501 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
C. 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 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
**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 **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. Job Set-up
__________
Subtask 52-21-00-010-052
A. Get Access
(1)
Open the AFT cargo-compartment door and install the actuator safety locks (Ref. TASK 52-30-00-860-001).
(2)
Put the access platform in position at the AFT cargo-compartment door.
(3)
Remove the linings 151CW and 152CW in the AFT cargo compartment to get access to the inflation reservoirs 7506MM and 7507MM.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-00Page 502 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 52-21-00-860-051
B. Preparation for the Test
**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,
(1)
Make sure that the hatch is correctly closed and its extended latch pin is engaged with the related release lever (Ref. TASK 52-21-11-400-001).
(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.
(b)
Loosen the knurled sleeve nut and disassemble the two collets from the flexible control assembly.
(c)
Disengage 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 503 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Operation of Emergency Exit Hatch
Figure 501/TASK 52-21-00-991-001- 12 (SHEET 1)
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-21-00Page 504 1 1 May 01/05 1 1 1CES 1
Operation of Emergency Exit Hatch
Figure 501/TASK 52-21-00-991-001- 22 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-21-00Page 505 1 1 May 01/05 1 1 1CES 1
Operation of Emergency Exit Hatch
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(18)
