TCH.1C-27J-2-27JG
2-70.1
REMOVAL (refer to figure
) , (refer
to figure
)
(Cont'd)
CAUTION
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Install protection caps on the
disconnected electrical connectors and
hoses.
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4.Remove tube assy (23 and 24) (behind flap sector
assembly).
5.Remove tee (16, 19 and 20) (which is on the left
behind the autopilot motor of the aileron in order to
disconnect the left side of pipe and remove the
clamps (17 and 18) that connect them to the structure.
6.Loosen the self-locking nuts (54, 60, 70 and 72) that
connect the bracket (43) to the rear spar of the central
wing and collect related washers (53, 61, 62,67, 69
and 78) and bolts (52, 63, 66 and 76). Discard
removed the self-locking nuts.
7.Unfasten the self-locking nuts (42 and 48) that
connect the rods to the bracket from the life raft side.
Discard removed the self-locking nuts.
8.Remove the cotter pins (47 and 77), loosen the
castellated nuts (46 and 73) and remove the bolts (41
and 50) collecting the washers (44, 45, 74 and 75)
that connect the bracket (43) to the drive unit (1).
9.Remove bracket (43) and rods (49 and 71) (which are
still assembled).
10.Get access to the panel with 26 screws and
disconnect the electrical connectors (34 and 35) which
are identical (so, should be better to make a sign over
them to avoid getting wrong).
(Cont'd)
27-50-25
2-571