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TCH.1C-27J-2-27JG
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00010 PIN, COTTER
MS24665-155
4,00
00012 PIN, COTTER
MS24665-374
1,00
00013 NUT, SELF-LOCKING H14-4
12,00
00033 PIN, COTTER
MS24665-162
4,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para 
1-3
) before performing
maintenance.
PROCEDURE:
2-22.1 REMOVAL (refer to figure 
1-20, sheet 1/4
) , (refer
to figure 
1-20, sheet 2/4
) , (refer to figure 
1-20,
sheet 3/4
) and (refer to figure 
1-20, sheet 4/4
)
1.Insert a rigging pin (1) (AGE NO. 00181) in the LH/
RH (2) control wheel in order to set them in neutral
position.
2.Insert a rigging pins (47 and 50) (AGE NO. 00181) in
the LH sector group (48) and in the RH sector group
(49) located in the center wing section.
3.Remove the retaining clips (27, 29, 30, 35, 37 and 38)
and acting on the turnbuckles (28, 31, 36 and 39)
slowly release the tension of the LH and RH aileron
cabin cables (7 and 11). (If is necessary remove the
LH/ RH AILERON CABIN CABLE in accordance with
maintenance task remove/replace LH / RH aileron
cabin cable (refer to para 
1-12
) .
(Cont'd)
27-10-15
2-175