(6)
Remove the bolt (1) and disconnect the rod (9).
(7)
Remove the cotter pin (32) and discard it. Remove the nut (31) and the washer (30).
(8)
Remove the bolt (34) and disconnect the rods (29) and (33).
(9)
Remove the cotter pin (63) and discard it. Remove the nut (64) and the washer (65).
CAPT Yaw/Brake Bellcrank
Figure 402/TASK 27-21-44-991-002
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-44Page 406 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R CAPT Yaw/Brake Bellcrank
R Figure 402A/TASK 27-21-44-991-002-A
R 1EFF : 301-399, 1 27-21-44 Page 407
1 1 May 01/04
1 1
1CES 1
CAPT Yaw/Brake Bellcrank Figure 403/TASK 27-21-44-991-003
1EFF : 1 1R 1CES ALL 1 11 1 27-21-44 Page 408 May 01/04
(10)
Remove the bolt (67) and disconnect the rod (68).
(11)
Remove the cotter pin (58) and discard it. Remove the nut (57) and the washer (56).
(12)
Remove the bolt (52) and disconnect the rod (69).
(13)
Remove the cotter pin (60) and discard it. Remove the nut (59) and the washer (61).
(14)
Remove the bolt (70) and disconnect the rod (66).
(15)
Remove the cotter pin (55) and discard it. Remove the nut (54) and the washer (53).
(16)
Remove the bolt (51) and disconnect the rod (62).
(17)
Remove the cotter pin (48) and discard it. Remove the nut (47) and the washer (46).
(18)
Remove the bolt (43) and disconnect the rod (42).
(19)
Remove the nuts (41) and discard them. Remove the bolts (49) and the bolts (50).
(20)
Turn the yaw bellcrank (2) 90 deg. to make the removal of the yaw/brake bellcrank possible.
(21)
Remove the sleeves (45) and (73) and the yaw/brake bellcrank.
1EFF : ALL 1 27-21-44Page 409 1 1 May 01/04R 1 1 1CES 1
TASK 27-21-44-400-001
Installation of the CAPT Yaw/Brake Bellcrank
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98A27901002000 3 PIN, RIGGING - RUDDER CONTROL
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific lockwire corrosion resistant steel dia 0.8 mm (0.03 in.) No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
11 cotter pin 27-21-01 01 -010 11 cotter pin 27-21-01 01A-010 19 cotter pin 27-21-01 01 -010 19 cotter pin 27-21-01 01A-010 24 cotter pin 27-21-01 01 -010 24 cotter pin 27-21-01 01A-010 32 cotter pin 27-21-01 01 -010 32 cotter pin 27-21-01 01A-010 41 nuts 27-21-01 07 -120 48 cotter pin 27-21-01 07 -010 55 cotter pin 32-42-01 04 -010 58 cotter pin 32-42-01 04 -010 60 cotter pin 32-42-01 04 -010 63 cotter pin 32-42-01 04 -010
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 32-42-00-710-001 Operational Check of the Normal Braking System 32-43-00-710-001 Operational Check of Alternate Braking System
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-44-991-001 Fig. 401
**ON A/C 301-399,
27-21-44-991-001-A Fig. 401A
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵2(26)
