**ON A/C ALL
27-21-43-991-005 Fig. 403
3. Job Set-up
__________
Subtask 27-21-43-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the access platform is in position.
(3)
Make sure that the access door 811 is open.
(4)
Make sure that the Blue hydraulic system is depressurized (Ref. TASK 29-10-00-863-003).
(5)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(6)
Make sure that the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (1) is installed on the yaw/brake bellcrank (see detail B)
4. Procedure
_________
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
(Ref. Fig. 401/TASK 27-21-43-991-003) R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-21-43-991-003-A)
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
(Ref. Fig. 402/TASK 27-21-43-991-004)R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 402A/TASK 27-21-43-991-004-A)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-21-43-991-005)
Subtask 27-21-43-420-055
A. Installation of the Pedal Position Adjuster Assembly
(1)
Apply COMMON GREASE (Material No. 04-004) to the attachment hardware.
(2)
Install the springs (41) and (42) on the rack assembly (26).
(3)
Lift the lower part of the rack assembly (26) to compress the springs
(41) and (42).
(4)
Install the rack assembly (26) on the yoke (29) with the spacer (28) and on the structure (19) with the bolt (18).
(5)
Install the washer (20), the nut (21) and the new cotter pin (22).
(6)
Install the washers (25), the bolt (27), the nut (24) and the new cotter pin (23).
(7)
Install the nut (43) and the screw (44). NOTE : Engage all the threads of the screw (44) but do not fully
____
tighten it.
(8)
Install the actuator (37) with the pins (36) on the structure (35) and the yoke (29).
(9)
Install the washers (34) and the new cotter pins (33).
(10) Install the cable (17) through the screw (44) and to the lower part of the rack assembly (26) with the pin (40).
NOTE : The pin (40) has a slot and a recess for the head of the cable
____
(17).
(11)
Install the locking pin (46).
(12)
Install the cover (5) on the structure (8) and (9).
(13)
Put the cable (17) through the cover (5) and install the pin (16) on the handle (15).
NOTE : The pin (16) has a slot and a recess for the head of the cable
____
(17).
(14)
Install the clip (45).
(15)
Install the washers (11) and the screws (10).
(16)
Install the washers (7) and the screws (6).
(17)
Connect the rod (39) to the yoke (29) with the screw (38).
(18) Install the washer (32), the nut (31) and the new cotter pin (30). Subtask 27-21-43-820-050
B. Adjustment
(Ref. Fig. 403/TASK 27-21-43-991-005)
NOTE : During the adjustment of the cable length, make sure that the
____ terminal heads of the cables (17) are in position in their housings.
(1)
Adjust the length of each rack unlocking control-cable so that the adjustment position limits, the non-control (measured at the handle) is between 0.8 mm (0.0314 in.) and 2 mm (0.0787 in.).
(a) Slowly loosen the screw (44) until you get a non-control clearance at the handle (15) (Ref. Section CC).
-
position 0: non-control more than or equal to 0.8 mm (0.0314 in.)
-
position 12: non-control less than or equal to 2 mm (0.0787 in.).
(2)
Tighten the nut (43).
(3)
Safety the nut (43) with Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.).
1EFF : ALL 1 27-21-43Page 415 1 1 May 01/05R 1 1 1CES 1
Subtask 27-21-43-710-051
C. Operational Test
(1) Remove the pin (1) (Ref. Detail B).
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
(Ref. Fig. 401/TASK 27-21-43-991-003) R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-21-43-991-003-A)
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(24)
