TCH.1C-27J-2-27JG
2-20.2 INSTALLATION (refer to figure
(refer to figure
) , (refer to figure
) and (refer to figure
) (Cont'd)
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).
8.Tighten the turnbuckles (7 , 8, 39 and 40) up to
previously note position.
FOLLOW ON MAINTENANCE:
1.Perform fuselage cables tension.
2.Perform center wing cable tension.
3.Perform outer wing cables tension.
4.Perform the functional test and adjustment as
described in AILERON TENSION REGULATOR (refer
to para
5.Connect electrical power to aircraft (refer to manual
6.Restore hydraulic power system (refer to manual
7.Remove all the rigging pins (1, 4 and 6) previously
inserted (refer to figure
figure
8.Perform the functional test MEASUREMENT OF
AILERON MANOEUVRE EFFORT (without hydraulic)
(refer to para
9.Close the access panels 553A, 553B and 553C.
10.Remove maintenance platform (AGE NO. 00074).
27-10-15
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