R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-45-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-45-991-001-A)
**ON A/C ALL
(11)
In zone 311, on the cable quadrant (1) (Ref. Details B and D), make sure that the PIN - RIGGING (98D27207547000) (8) or RIGGING PIN SET (98D27207516000) pin (98D27207516160) is installed.
(12)
Make sure that the Blue hydraulic system (Ref. TASK 29-10-00-864-003) is depressurized.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-45-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-45-991-001-A)
**ON A/C ALL
R (13) Make sure that the Yellow and Green hydraulic systems are depressurized. (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (14) Make sure that the aircraft electrical circuits are de-energized. 4. Procedure_________ **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-45-991-001) **ON A/C 301-399,
R (Ref. Fig. 401A/TASK 27-21-45-991-001-A) **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 402/TASK 27-21-45-991-002) **ON A/C 301-399,
R (Ref. Fig. 402A/TASK 27-21-45-991-002-A) **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 403/TASK 27-21-45-991-003) **ON A/C 301-399,
(Ref. Fig. 403A/TASK 27-21-45-991-003-A)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-21-45-420-052
A. Installation of the Cable Tension-Regulator Assy
(1)
Apply COMMON GREASE (Material No. 04-004) on all attaching parts.
(2)
Install the regulator (15) on the support (26) with the spacer (25) and the screw (24).
(3)
Install the regulator (15) on the support (20) with the spacer (21) and the screw (22).
(4)
Install the washer (19), the nut (18) and the new cotter pin (17).
(5)
Install the washer (27), the nut (28) and the new cotter pin (29). NOTE : Align the shackle (16) of the regulator (15) in the center.
____ Make sure that the shackle does not touch the support (20).
(6)
Connect the rod (23) to the regulator (15) with the screw (39) (Ref. Detail H). If an adjustment is necessary, do as follows:
(a)
Cut and remove the lockwire from the nuts of the rod (23).
(b)
Loosen the nuts of the rod (23).
(c)
Disengage the washers from the nuts of the rod (23).
(d)
Adjust the rod (23) to the necessary length and without tension.
(e)
TORQUE the nuts of the rod (23) to 0.59 m.daN (52.21 lbf.in). Do not safety at this time.
(7)
Install the washer (36) and the nut (37). Do not safety the nut (37) at this time.
(8)
Install the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (6) on the input lever of the regulator (15) (Ref. Detail J).
(9)
Connect the rod (4) to the regulator (15) with the screws (42) (Ref. Detail J). If an adjustment is necessary, do as follows:
(a) Cut and remove the lockwire from the nuts of the rod (4).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-45Page 418 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(b)
Loosen the nuts of the rod (4).
(c)
Disengage the washers from the nuts of the rod (4).
(d)
Adjust the rod (4) to the necessary length.
(e)
TORQUE the nuts of the rod (4) to 1.374 m.daN (10.13 lbf.ft). Do not safety at this time.
(10)
Install the washer (43) and the nut (41). Do not safety the nut (41) at this time.
(11)
Install the cables (7) and (9) on the regulator (15) (Ref. Details F and G).
(12)
Install the new cotter pins (35) on the cable end housings of the regulator (15).
(13)
Install the spacers (47), the screws (46), the washers (48), the nuts
(49) and the new cotter pins (50) (Ref. Detail K).
(14)
Tighten the screws (2) of the cable quadrant (1) turnbuckles until it is possible to remove the locking equipment (45) from the regulator (15).
(15)
Remove this TOOL - LOCKING (FE171901) (45) with the rigging pins (44).
(16)
Remove the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (6) from the CAPT yaw/brake bellcrank (5) (Ref. Detail C).
**ON A/C 301-399,
Subtask 27-21-45-420-052-A R A. Installation of the Cable Tension-Regulator Assy
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 FLIGHT CONTROLS 飞行操纵2(35)
