(5)
Make sure that the access doors 811, 825, 826, 312AR are open.
(6)
In the zones 211 and 221, make sure that the floor panels 211GF, 211KF, 221EF, 231CF 221LF are removed.
(7)
In the zone 241, make sure that the floor panels 231WF, 241BF, 241FF, 241KF are removed.
(8)
In the zone 131, make sure that the ceiling panels 131AC, 131BC, 131CC 131DC, 131EC 131PW are removed.
(9)
In the zones 151 and 161, make sure that the ceiling panels 151AC, 151BC, 151AY, 151CC, 151DC, 161AC, 161BC are removed.
R 1EFF : 151-199, 301-399, 401-499, 1 27-41-44Page 429 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 054-099, 101-149, 201-299,
R Post SB 53-1143 For A/C 001-003,
R Subtask 27-41-44-010-055-C
R A. Get Access
R (1) Make sure that the access platform is in position at the zone 121.
R (2) Make sure that the access platform is in position at the zone 132.
R (3) Make sure that the access platform is in position at the zone 154.
R (4) Make sure that the access platform is in position at the zone 312.
R (5) Make sure that the access doors 811, 825, 826, 312AR are open.
R (6) In the zones 211 and 221, make sure that the floor panels 211GF,
R 211KF, 221EF, 231CF 221LF are removed.
R (7) In the zone 241, make sure that the floor panels 231WF, 241BF, 241FF,
R 241KF are removed.
R (8) In the zone 131, make sure that the ceiling panels 131AC, 131BC,
R 131CC 131PW are removed.
R (9) In the zones 151 and 161, make sure that the ceiling panels 151AC,
R 151BC, 151CC, 151DC, 161AC, 161BC are removed.
**ON A/C ALL
Subtask 27-41-44-860-052
B. Aircraft Maintenance Configuration
(1) Make sure that the PITCH TRIM CONTROL LOCKING (98D27403500000) is
installed to prevent the movement of the pitch-trim control wheels.
(2) Make sure that the PIN - RIGGING (0U190360) (66) is installed on the
input lever of the THS actuator (65) (See Details Q and R).
R **ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 402/TASK 27-41-44-991-002)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 402A/TASK 27-41-44-991-002-A)
**ON A/C 301-399,
(Ref. Fig. 402B/TASK 27-41-44-991-002-B)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-41-44-991-008)
(3)
Make sure that the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) are depressurized.
(4)
On the CAPT and F/0 side-sticks, make sure that the warning notices are in position.
(5)
Apply COMMON GREASE (Material No. 04-004) to all the attachment parts.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 402/TASK 27-41-44-991-002) R **ON A/C 151-199, 401-499,
(Ref. Fig. 402A/TASK 27-41-44-991-002-A)
**ON A/C 301-399,
(Ref. Fig. 402B/TASK 27-41-44-991-002-B)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-41-44-991-008, 404/TASK 27-41-44-991-003, 405/TASK 27-41-44-991-004, 406/TASK 27-41-44-991-005, 407/TASK 27-41-44-991-006, 408/TASK 27-41-44-991-007)R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-41-44-420-050
A. Installation of the THS Control Cables
(1)
Install the chain (7) on the gear wheel of the lower shaft assembly (1). Keep to the 33.5 links dimension (See Detail B).
(2)
Do the routing of the cables (5) and (6) through FR14, 23, 28, 33,
35.
NOTE : The upper cable (5) goes along the left (when you look from
____ the rear to the front of the aircraft). The lower cable (6) goes along the right.
(3)
At FR14, 23, 28, 33, 35, install the cable guides (See Detail F) as follows:
(a)
Install the half-shells (19).
(b)
Install the retainers (20).
(4)
Install the chain (35) on the gear wheel of the input shaft (25) of the THS actuator (65). Keep to the 33.6 links dimension (See Detail G).
(5)
Do the routing of the cables (10) and (11) to the tension regulator (40).
NOTE : The cable (10) goes along the right (when you look from the
____ rear to the front of the aircraft). The cable (11) goes along the left.
(6)
Insert the cable (11) inside the rudder-control tension-regulator. (The cable (10) goes along the right).
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