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TCH.1C-27J-2-27JG
2-19.2
INSTALLATION (refer to figure 
2-15, sheet 1/4
) ,
(refer to figure 
2-15, sheet 3/4
) , (refer to figure
2-15, sheet 2/4
) and (refer to figure 
2-15, sheet 4/4
) (Cont'd)
CAUTION
––––––––––––––––––––––––––––––––––
Do not perform the complete tension of
the cable.
––––––––––––––––––––––––––––––––––
B.Aileron center wing cable (if the cable has been
removed, replace aileron center wing cable in
accordance with maintenance task remove/replace
aileron center wing cable (refer to para 
2-11
) ).
CAUTION
––––––––––––––––––––––––––––––––––
Do not perform the complete tension of
the cable.
––––––––––––––––––––––––––––––––––
C.LH aileron fuselage cable (if the cable has been
removed, replace LH aileron fuselage cable in
accordance with maintenance task remove/replace
LH aileron fuselage cable (refer to para 
2-9
) ).
CAUTION
––––––––––––––––––––––––––––––––––
Do not perform the complete tension of
the cable.
––––––––––––––––––––––––––––––––––
5.Install the cables lock (16, 31 and 37) by using the
new cotter pins (LCM NO. 00052) (13, 28 and 35),
tightening the nuts (14, 29 and 34) and by using the
bolts (18, 33 and 38) and washers (15, 30 and 36).
6.Insert the flanged failrlead (11).
7.Insert the new locking ring (LCM NO. 00179) (10) and
tighten the new locking nut (LCM NO. 00408) (9).
(Cont'd)
27-10-15
2-153