(9)
In the zones 151 and 161, remove the ceiling panels 151AC, 151AY, 151BC, 151CC, 151DC, 161AC, 161BC (Ref. TASK 25-55-11-000-002) (Ref. TASK 25-55-12-000-002).
R 1EFF : 151-199, 301-399, 401-499, 1 27-41-44Page 408 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 27-41-44-010-050-C
R A. Get Access
R (1) Put the access platform in position at the zone 121.
R (2) Put the access platform in position at the zone 132.
R (3) Put the access platform in position at the zone 154.
R (4) Put the access platform in position at the zone 312.
R (5) Open the access doors 811, 825, 826, 312AR.
R (6) In the zones 211 and 221, remove the floor panels 211GF, 211KF,
R 221EF, 231CF 221LF (Ref. TASK 53-12-11-000-001) (Ref. TASK 53-12-12-
R 000-001).
R (7) In the zone 241, remove the floor panels 231WF, 241BF, 241FF, 241KF
R (Ref. TASK 53-22-12-000-001) (Ref. TASK 53-32-12-000-002).
R (8) In the zone 131, remove the ceiling panels 131AC, 131BC, 131CC, 131PW
R (Ref. TASK 25-54-12-000-002).
R (9) In the zones 151 and 161, remove the ceiling panels 151AC, 151BC,
R 151CC, 151DC, 161AC, 161BC (Ref. TASK 25-55-11-000-002) (Ref. TASK
R 25-55-12-000-002).
**ON A/C ALL
Subtask 27-41-44-860-050
B. Aircraft Maintenance Configuration
(1) Pressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-
00-863-001) (Ref. TASK 29-24-00-863-001).
(2) On the center pedestal, make sure that the pitch-trim control wheels
are in the 0 position.
(3) Put the PITCH TRIM CONTROL LOCKING (98D27403500000) in position to
prevent the movement of the pitch-trim control wheels.
(4) Put the PIN - RIGGING (0U190360) (66) on the input lever of the THS actuator (65) (See Details Q and 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)
(5)
Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001).
(6)
Put the warning notices on the CAPT and F/0 side-sticks.
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)
Cable Linkage
Figure 402/TASK 27-41-44-991-002
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-41-44Page 411 1 1 May 01/05 1 1 1CES 1
Cable Linkage Figure 402A/TASK 27-41-44-991-002-A
R 1EFF : 151-199, 401-499, 1 27-41-44Page 412 1 1 Aug 01/05 1 1 1CES 1
Cable Linkage
Figure 402B/TASK 27-41-44-991-002-B
R 1EFF : 301-399, 1 27-41-44 Page 413
1 1 May 01/05
1 1
1CES 1
THS Actuator Figure 403/TASK 27-41-44-991-008
1EFF : 1 1R 1CES ALL 1 11 1 27-41-44 Page 414 May 01/05
**ON A/C ALL
(Ref. Fig. 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 27-41-44-010-051
A. Removal of the THS Control Cables
(1)
At FR35, 33, 28, 23, 14, remove the cable guides (See Detail F) as follows :
(a)
Cut and discard the cables ties (21).
(b)
Remove the retainers (20).
(c)
Remove the half-shells (19).
(2)
At zone 121, cut and remove the lockwire from the screws (4) and discard it (See Detail A).
(3)
Remove the screws (4) and the washers (3).
(4)
Remove the chain guard (2).
(5)
At FR42, 48, 53, 58, 63, 67, remove the cable guides (See Detail F) as follows:
(a)
Cut and discard the cable ties (21).
(b)
Remove the retainers (20).
