TCH.1C-27J-2-27JG
2-21.1
REMOVAL (refer to figure
) , (refer
to figure
)
(Cont'd)
4.Remove the retaining clips (51, 52, 54 and 56) and
acting on the turnbuckles (57, 58, 59 and 60) between
frames 10 and 12 slowly release the tension of the LH
and RH aileron fuselage cables (53 and 55). If is
necessary remove the LH / RH AILERON FUSELAGE
CABLE in accordance with maintenance task
remove/replace LH / RH aileron fuselage cable (refer
to para
) .
5.Remove from RH / LH quadrant (6 and 10) the cotter
pins (24, 32, 40 and 41). Discard removed cotter pins.
6.Remove the cables (7 and 11) from RH / LH quadrant
(6 and 10).
7.Remove from aircraft RH support (45) and LH support
(14) by removing bolts (3, 13, 22 and 46), washers (4,
15, 21 and 44) and self locking nuts (5, 16, 20 and
43). Discard removed self locking nuts.
8.Remove from the aircraft the syncro-shaft (9)
complete with LH support (14) and RH support (45)
and place it on workbench.
9.Remove from LH quadrant (10) the support (14) by
removing bolt (23), washer (19), castellated nut (17)
and cotter pin (18). Discard removed cotter pin.
10.Remove from RH quadrant (6) the RH support (45) by
removing bolt (42).
11.Remove from RH quadrant (6) the syncro-shaft (9) by
removing bolts (8), washers (34), and self locking nuts
(33). Discard removed self locking nuts.
12.Remove from LH quadrant (10) the syncro-shaft (9) by
removing bolts (12), washers (25), and self locking
nuts (26). Discard removed self locking nuts.
13.Remove syncro-shaft (9).
27-10-15
2-171