TCH.1C-27J-2-27JG
2-22.2 INSTALLATION (refer to figure
(refer to figure
) , (refer to figure
) and (refer to figure
)
1.Position syncro-shaft (9) on workbench.
2.Connect at the LH quadrant (10) the syncro-shaft (9)
by using bolts (12), washers (25), and new self locking
nuts (26) (LCM NO. 00013).
3.Connect at the RH quadrant (6) the syncro-shaft (9)
by using bolts (8), washers (34), and new self locking
nuts (33) (LCM NO. 00013).
4.Connect at the RH quadrant (6) the support (45) by
using bolt (42).
5.Connect at the LH quadrant (10) the support (14) by
using bolt (23), washer (19), castellated nut (17) and
new cotter pin (18) (LCM NO. 00012).
6.Connect at the aircraft the syncro-shaft (9) complete
with LH support (14) and RH support (45).
7.Connect at the aircraft RH support (45) and LH
support (14) by using bolts (3, 13, 22 and 46),
washers (4, 15, 21 and 44) and new self locking nuts
(5, 16, 20 and 43) (LCM NO. 00013).
8.Install on grooves of the RH / LH quadrant (6 and 10)
the cables (7 and 11).
9.Insert in the RH / LH quadrant (6 and 10) the new
cotter pins (24, 32, 40 and 41) (LCM NO. 00010 and
00033).
CAUTION
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Do not perform the complete tension of
the cable.
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(Cont'd)
27-10-15
2-177