Release-Mechanism Camshaft Assembly Figure 408A/TASK 25-62-43-991-007-A22 (SHEET 2)
R EFF : 151-199, 401-499, 25-62-43 Page 449 Aug 01/05
CES
(3) Remove the release-mechanism tie-rod assemblies:
**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) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(a)
Remove and discard the cotter pins (45).
(b)
Remove the castellated nuts (46) and the washers (47).
(c)
Record the location of the bushes (52) and (53).
(d)
Hold the tie-rod assembly (54), and remove the bolt (50) and the washer (48).
(e)
Release the tie-rod assembly (54) from the lever assembly and remove the bushes (52) and (53).
(f)
Record the location of the bushes (61) and (62).
(g)
Hold the over-center spring-rod assembly (63) (referred to as the spring-rod assembly) and remove the bolt (51) and the washer (49).
(h)
Release the spring-rod assembly (63) from the lever assembly and remove the bushes (61) and (62).
(i)
Remove and discard the cotter pin (55).
(j)
Remove the castellated nut (56) and the washer (57).
(k)
Record the location of the bushes (59) and (60).
(l)
Hold the tie-rod assembly (54) and remove the bolt (58).
(m)
Release the tie-rod assembly (54) from the camshaft assembly and remove the bushes (59) and (60).
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CES
(n)
Remove and discard the cotter pin (64).
(o)
Remove the castellated nut (65) and the washer (66)
(p)
Record the location of the bushes (69) and (70).
(q)
Hold the spring-rod assembly (63) and remove the bolt (68) and the washer (67).
(r)
Release the spring-rod assembly (63) from the bracket (75) and remove the bushes (69) and (70).
(s)
Disassemble the spring-rod assembly: 1 Remove the eye-end fittings (42) and (44) from the bellows
_
(40).
2 Remove the bushes (41) and the spring (43) from the bellows
_
(40).
(t)
Remove the nut (72) and the bolt (71).
(u)
Remove the nuts (74) and the bolts (73), and the bracket (75) from the frame structure.
(4) Remove the release-mechanism lever assembly:
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 407/TASK 25-62-43-991-006) R **ON A/C 151-199, 401-499,
(Ref. Fig. 407A/TASK 25-62-43-991-006-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(a)
Remove the nuts (81), the bolts (80) and the release-mechanism lever assembly (82).
(b)
Remove the lever assembly from the lever bracket: 1 Remove and discard the cotter pin (85).
_
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CES
2 Remove the castellated nut (86), the washer (87) and the bolt
_
(88).
3 Remove the lever assembly (83) together with the washers (84)
_ from the lever bracket (94).
4 Record the location of the bushes (89) and (90).
_
5 Remove the bushes (89) and (90).
_
(c)
Remove and discard the lockwire from the setscrew (93) and the locking device (92).
(d)
Remove the nut (91), the locking device (92) and the setscrew (93).
(e)
Disassemble the lever assembly (83): 1 Carefully remove the double lever (105) together with the
_ bushes (104) and the washers (103).
2 Remove the bushes (104) from the double lever (105).
_
3 Remove the nuts (99).
_
4 Remove the lever (101), the bushes (98) and the washers (97).
_
5 Remove the bolts (95) and the washers (96) from the lever
_
(100).
6 Remove the bushes (102) from the levers (100) and (101).
_
(5) Remove the release-mechanism camshaft assembly:
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 408/TASK 25-62-43-991-007) R **ON A/C 151-199, 401-499,
(Ref. Fig. 408A/TASK 25-62-43-991-007-A)
R EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 452 201-299, 401-499, Aug 01/05
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本文链接地址：A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备4(95)
