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TCH.1C-27J-2-27JG
2-13.2
INSTALLATION. Proceed as follows:
A. Install the cable then stretch them, by means of
the turnbuckles (perform the same number of
rotation reported in the note).
B.Perform cable tension.
C.Remove all the rigging pins previously inserted.
FOLLOW ON MAINTENANCE:
1.Restore hydraulic power system (refer to manual
TCH.1C-27J-2-00GV
) .
2.Connect electrical power to aircraft (refer to manual
TCH.1C-27J-2-00GV
).
3.Close the access panels 212AZ, 212BZ, 214BZ,
130AH, 130AD and 213AZ (212EZ, 212DZ, 213BZ,
130AE and 130AG).
4.Install Pilot (Copilot) seat in order to get access to LH
(RH) Aileron Cabin Cable (refer to manual
TCH.1C-27J-2-25JG
)
5.Perform the functional tests adjustment:
A.AILERON TENSION REGULATOR (refer to para
2-8
) .
B.TRAVEL CHECK OF THE CONTROLWHEEL
(refer to para 
2-6
) .
C.AILERON CONTROL SYSTEM (refer to para 
2-7
) ,
(refer to para 
2-14
) and (refer to para 
2-18
) .
D.MEASUREMENT OF AILERON MANOEUVRE
EFFORT (without hydraulic) (refer to para 
2-6
) .
E.FRICTION MANOEUVRE EFFORT AND
BREAK-OUT CHECK (refer to para 
2-22
) .
27-10-05
2-90