R 1EFF : 001-049, 054-099, 101-149, 201-299, 1 27-21-61Page 431 1301-399, 1May 01/05 1 1 1CES 1
R R (8) In the zone 241, make sure that the floor panels 231WF, 241BF, 241FF, 241KF are removed.
R R (9) In the zone 131, make sure that the ceiling panels 131AC, 131BC, 131CC are removed.
R (10) In the zone 131, make sure that the partition panel 131PW is removed.
R R (11) In the zones 151 and 161, make sure that the ceiling panels 151AC, 151BC, 151CC, 151DC, 161AC, 161BC are removed.
R R (12) In the zone 161, make sure that the partition panels 161DW, 162DW are removed.
**ON A/C ALL
Subtask 27-21-61-860-052
B. Aircraft Maintenance Configuration
(1) Make sure that the PIN - RIGGING (98D27207547000) (48) or RIGGING PIN SET (98D27207516000) pin (98D27207516160) is installed on the cable quadrant (45). (Refer to Detail Q).
(2) Make sure that the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (2) is installed on the input lever of the tension regulator (1). (Refer to Details G and A).
(3) Make sure that the TOOL - LOCKING (FE171901) (18) with th pins (17) is installed on the tension regulator (1).
(4) Make sure that the Blue hydraulic system (Ref. TASK 29-10-00-864-003) is depressurized.
(5) Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002)
(6) On the CAPT and F/O rudder pedals, make sure that the warning notices are in position.
Subtask 27-21-61-640-050
C. Apply COMMON GREASE (Material No. 04-004) to all the nuts and bolts.
R 1EFF : ALL 1 27-21-61Page 432 1 1 May 01/05 1 1 1CES 1
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 401/TASK 27-21-61-991-001) R **ON A/C 151-199, 401-499,
(Ref. Fig. 401A/TASK 27-21-61-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 401B/TASK 27-21-61-991-001-B)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 402/TASK 27-21-61-991-002) R **ON A/C 151-199, 401-499,
(Ref. Fig. 402A/TASK 27-21-61-991-002-A)
**ON A/C 301-399,
(Ref. Fig. 402B/TASK 27-21-61-991-002-B)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-21-61-991-003, 404/TASK 27-21-61-991-006, 405/TASK 27-21-61-991-004, 406/TASK 27-21-61-991-005)R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-21-61-420-050
A. Installation of the Rudder Control Cables (Forward Part)
(1) Install the cables through the frames and on the tension regulator.
(a) Put the cables (4) and (5) through the frames 35, 33, 28, 23 and 14 as follows:
-
put the cable (4), with the cylindrical fool-proof device (Ref. Detail D), on the right (inboard side)
-
put the cable (5), with the spherical fool-proof device (Ref. Detail C), on the left (outboard side).
NOTE : The fool-proof device is to avoid error when you install
____
the cables.
(b)
Put the cable (4) through the pulley (20) (Refer to Detail B).
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(66)
