(10) to the cable (6) with the cable turnbuckle (23) (See Detail C). Do not put tension. Remove the LOCKING TOOL-CABLE (98F27003500000)
(13)
Install the LOCKING TOOL-CABLE (98F27003500000)
(14)
Connect the cable (11) to the cable (5) with the cable turnbuckle
(23) (See Detail C). Do not put tension. Remove the LOCKING TOOL-CABLE (98F27003500000)
(15)
At FR38, 42, 47.1, 48, 53, 58, 63 and 67, install the cable guides (See Detail F) as follows:
(a)
Install the half-shells (19).
(b)
Install the retainers (20).
(c)
Install new cable ties (21).
(16)
Install the half-shells (14) on the cables (10) and (11) and between the edges of the flanges (12) and (13) (See Detail D and Section EE).
(17)
Install the flanges (12) and (13) on FR70 with the washers (18) and the screws (17). Do not tighten.
(18)
Install the sleeve (16) and the circlip (15).
(19)
Lift the 2 flanges (51) and hold them in this position with the cables (10) and (11) in their grooves (See Detail L).
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(20)
Install the spacer (52), the bolt (50), the washer (53), the nut (55); tighten the nut and safety with the new cotter pin (54) (See Detail L and Section MM).
(21)
Install the spacer (59), the bolt (60), the washer (58), the nut (57); tighten the nut and safety with the new cotter pin (56) (See Detail L and Section PP).
(22)
Attach the springs (41) to the flanges (51) of the tension regulator (40).
(23)
Install the spacer (46), the bolt (47), the washer (45), the nut (44); tighten the nut and safety with the new cotter pin (43) (See Detail J and Section KK).
(24)
Install the guard (34), the 6 washers (32) and the 6 screws (33) (See Details H and J).
(25)
Install the chain guide (26) and the screws (27).
**ON A/C ALL
Subtask 27-41-44-820-050
B. Adjustment
(1) If you install a new forward cable, you must put a pre-tension to the cable before you adjust it.
(a)
Put the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000)
(42)
in position on the tension regulator (40) (See Detail J).
-In theory, the pre-tension time is 48 hours without movement of the aircraft. After this pre-tension time the adjustment of the cable will stay correct.
-A minimum pre-tension time of 4 hours without movement of the aircraft is permitted. The adjustment of the cable will not stay correct for a long time. You must do the full pre-tension procedure when the aircraft stops for maintenance for a sufficiently long time.
-For a pre-tension time between 4 and 48 hours, the stability of the adjustments is in proportion to the pre-tension time.
(b) Use the cable turnbuckles (23) to put a tension of 55 +5 -5 daN (123.6448 +11.2404 -11.2404 lbf) to the cable linkage (See Detail C). Measure this value with a tensiometer.
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(c)
The Linkage must stay in this position for 48 hours.
(d)
With the turnbuckles (23), release the tension on the linkage until you can remove the pin (42).
(e)
Remove the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000)
(42)
from the tension regulator (40).
(2)
Make sure that the flanges (12) and (13) are in the correct position over the cables (10) and (11). Tighten the screws (17) (See Detail D and Section EE).
(3)
Safety the screws (17) with Lockwire corrosion resistant steel dia
0.8 mm (0.03 in.).
(4)
Turn the turnbuckles until you cannot see the threads of the aft and rear wire rope terminal control cables of the THS.
(5)
Safety the turnbuckles with the locking clips.
(6)
Adjust the control cables length (Ref. TASK 27-41-00-820-002). NOTE : If you cannot adjust the control cables, do a visual
____ inspection on the pulleys and the tension regulator. If they are in good condition, replace the control cables.
(7)
Make sure that the distance between the turnbuckles and the fairleads is minimum 25.4 mm (1.0000 in.) over the full travel range of the THS control.
(8)
Make sure that the distance between the ends of the turnbuckles in each THS control cable is minimun 90 mm (3.5433 in.) in all the positions.
Subtask 27-41-44-720-050
C. Test
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