R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(a)
Remove the nut (120) and the bolt (119).
(b)
Remove and discard the cotter pin (110).
(c)
Remove the castellated nut (111) and the washer (112).
(d)
Remove the release lever (113) and the spacer (114).
(e)
Remove the stop screw (115).
(f)
Remove the nuts (117), the bolts (116) and the bearing flange
(118) from the frame structure.
(g)
Remove and discard the lock-wire from the screws (125) and (128).
(h)
Remove the screw (125), the washer (126) and the release lever (127).
(i)
Disassemble the release lever: 1 Remove the screw (128) and the washer (129).
_
2 Remove the lever (130) from the release lever (127).
_
(j)
Remove the nuts (122), the bolts (123) and the bearing flange
(124) from the frame structure.
(k)
Remove the camshaft assembly (121) together with the bearing flanges (118) and (124).
(l)
Remove the bearing flanges (118) and (124) from the shaft ends of the camshaft assembly (121).
(m)
Disassemble the camshaft assembly:
1 Remove the bush (144).
_
2 Carefully pull the shaft (130) out of the camshaft (135).
_
3 Remove the nut (143) and the bolt (141).
_
R EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 453 201-299, 401-499, Aug 01/05
CES CES TASK 25-62-43-400-003
4_ Remove the lever (142) from the camshaft:
WARNING : BE CAREFUL WHEN YOU REMOVE THE LEVER FROM THE_______
CAMSHAFT.
THE LEVER IS CONNECTED TO THE TORSION-SPRING, AND
THE TENSION OF THE TORSION-SPRING WILL CAUSE SUDDEN
MOVEMENT OF THE LEVER. THIS CAN CAUSE INJURY TO
PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
a_ Remove the lever (142) from the camshaft (135).
5_ Remove the torsion spring (140) and the washers (139) from the
camshaft (135).
6_ Remove the nut (138) and the bolt (131).
7_ Remove the levers (132) and (137) together with the bush (134)
from the camshaft (135).
8_ Remove the washers (133) and (136) from the camshaft (135).
Installation of the Emergency Escape-Slide Release-Mechanism Assembly
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific clean cloth No specific feeler gage No specific nonmetallic scraper No specific slide gage No specific warning notice No specific access platform 2.1 m (6 ft. 11 in.) No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) TLW101 1 TEST TOOL - RELEASE CABLE , ESCAPE SLIDE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (Ref. 20-31-00)
Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 455 201-299, 401-499, Aug 01/05
CES C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
6 cotter pin 25-62-04 10 -070A
6 Cotter pin 25-62-04 10 -070A
7 cotter pin 25-62-04 10 -070A
45 cotter pins 25-62-04 13 -080
45 cotter pins 25-62-04 13A-080
55 cotter pin 25-62-04 13 -170
55 cotter pin 25-62-04 13A-170
64 cotter pin 25-62-04 13 -080
64 cotter pin 25-62-04 13A-080
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本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備4(96)
