TCH.1C-27J-2-27JG
2-21.1 REMOVAL (refer to figure
), (refer
to figure
16.Remove the aft quadrant (42) with the two bearings
(32 and 45), the spacer (33) and washer (43) fromthe
support (44).
2-21.2 INSTALLATION (refer to figure
),
(refer to figure
), (refer to figure
), (refer to figure
)
1.Install the aft quadrant (42) with the two bearings (32
and 45), the spacer (33) and washer (43) to the
support (44).
CAUTION
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When the following cables are positioned
in the related grooves of the aft quadrant,
connect them to the turnbuckles but do
not perform the complete tension of
cables at this step.
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NOTE
Performing next step does not pull the cable
excessively to avoid their repositioning on
pulleys in fuselage and in right outer wing.
2.In the grooves of the aft quadrant (42) install
cables(34 and 35).
3.Install on the aft quadrant (42), the bolts (40, 46 and
55), flat washers (38, 48 and 53), the castellated nuts
(36, 49 and 51), the new cotter pins (37, 50 and52)
(LCM NO. 00052) and cable lock clevises (39, 47and
54).
4.Install new locking ring (30) (LCM NO. 00179), locking
nut (29) and fair lead flange (31) on thesupport (44).
(Cont'd)
27-10-15
2-167