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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)
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 
2-7
) .
5.Connect electrical power to aircraft (refer to manual
TCH.1C-27J-2-00GV
).
6.Restore hydraulic power system (refer to manual
TCH.1C-27J-2-00GV
) .
7.Remove all the rigging pins (1, 4 and 6) previously
inserted (refer to figure 
2-15, sheet 1/4
) and (refer to
figure 
2-15, sheet 2/4
) .
8.Perform the functional test MEASUREMENT OF
AILERON MANOEUVRE EFFORT (without hydraulic)
(refer to para 
2-6
) .
9.Close the access panels 553A, 553B and 553C.
10.Remove maintenance platform (AGE NO. 00074).
27-10-15
2-154