(b)
Remove the emergency-exit door-frame linings 241LW (242LW), 214CW (242CW) (Ref. TASK 25-23-47-000-002).
(8)
Remove the insulation blankets in the area that you are working (Ref. TASK 25-80-00-000-001).
(9)
Remove the proximity switches 5WN1 and 5WN2
(Ref. TASK 52-73-11-000-003).
(10) Remove the proximity switches 6WN1 and 6WN2
(Ref. TASK 52-73-11-000-004).
R **ON A/C 151-199, 401-499,
Subtask 25-62-43-010-058-A
B. Get Access
(1)
Open the AFT cargo-compartment door with the yellow electric pump (Ref. TASK 52-30-00-860-001).
(2)
Put the access platform in position at the AFT cargo-compartment door.
(3)
Put the warning notice on the AFT cargo-compartment door to tell persons not to close the door.
(4)
Do the special precautions before you work on the offwing escape-slide system(s) (Ref. TASK 25-62-00-481-001).
(5)
Remove the passenger seats in the area of the applicable emergency exit hatches (Ref. TASK 25-21-41-000-001).
(6)
Remove the applicable emergency exit hatches
(Ref. TASK 52-21-11-000-001).
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(7) Remove the access panels: NOTE : Access panel numbers for the RH emergency escape-slide
____ release-mechanism assembly are given in the brackets.
(a)
Remove the cove light panel 241MW (242MW) (Ref. TASK 25-23-48-000-001).
(b)
Remove the emergency-exit door-frame lining 241FW (242FW) (Ref. TASK 25-23-47-000-002).
(8)
Remove the insulation blankets in the area that you are working (Ref. TASK 25-80-00-000-001).
(9)
Remove the proximity switches 6WN1 and 6WN2
(Ref. TASK 52-73-11-000-004).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
4. Procedure
_________
Subtask 25-62-43-020-056
A. Disconnection of the Release Cable-Assembly
(Ref. Fig. 403/TASK 25-62-43-991-009)
(1)
Remove and discard the lockwire (4) from the knurled sleeve-nut (5).
(2)
Loosen the knurled sleeve-nut (5) fully to get access to the two collets (7).
(3)
Remove and keep the two collets (7).
(4)
Disconnect the release cable-assembly from the flexible control-assembly:
CAUTION : DO NOT PUSH THE END OF THE WIRE INTO THE WIRE-CONTROL
_______ ASSEMBLY. THIS CAN CAUSE A KINK IN THE WIRE.
(a)
Carefully remove the end of the release cable-assembly (2) from the related slot of the flexible control-cable (1).
(b)
Make sure that you do not push the end of the wire into the release cable-assembly (2).
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Release-Cable Connection Figure 403/TASK 25-62-43-991-009
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(5)
Remove the protective plug (6) from the pocket (3).
(6)
Put the two collets (7) in their position on the end of the release cable-assembly (2).
(7)
Move the knurled sleeve-nut (5) up and install the protective plug (6).
Subtask 25-62-43-020-055
B. Removal of the Emergency Escape-Slide Release-Mechanism
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 404/TASK 25-62-43-991-003) R **ON A/C 151-199, 401-499,
(Ref. Fig. 404A/TASK 25-62-43-991-003-A)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 405/TASK 25-62-43-991-004) R **ON A/C 151-199, 401-499,
(Ref. Fig. 405A/TASK 25-62-43-991-004-A)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 406/TASK 25-62-43-991-005) R **ON A/C 151-199, 401-499,
(Ref. Fig. 406A/TASK 25-62-43-991-005-A)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 407/TASK 25-62-43-991-006)
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CES
Emergency Escape-Slide Release-Mechanism Assembly Figure 404/TASK 25-62-43-991-003
R EFF : 001-049, 051-099, 101-149, 201-299, 25-62-43 Page 433 May 01/05
CES
Emergency Escape-Slide Release-Mechanism Assembly Figure 404A/TASK 25-62-43-991-003-A 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备4(93)
