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Aircraft Service Manual
Jabiru Aircraft
Pty Ltd
JTM001-1
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
REVISION
1
Dated: Nov 2011
Issued By: SW
Page: 155 of 233
Figure 130
– Typical Rudder Installation (Steel Hinges)
12.4 RUDDER CONTROL CABLE
12.4.1 DESCRIPTION
Control Cables are of the enclosed push-pull type, fitted with spherical bearings at both ends. To
operate, the outer cover of the cable must be clamped firmly at each end.
12.4.2 CONTROL CABLE REMOVAL
11.
Unbolt the connections (rod end bearings) at either ends of the cable.
12.
Unbolt the clamps at either end of the cable.
13.
Where required, remove any ties etc used to restrain the cables in the aircraft.
14.
Tie a string or light wire to one end of the cable.
15.
Draw the cable out of the aircraft, leaving the string/wire in place to allow installation of a
replacement part.
12.4.3 CONTROL CABLE INSPECTION
The Control Cable is a Primary Control and may not be repaired or removed without reference to
Jabiru Aircraft Pty Ltd or our approved local agent.
Details of inspections required for control cables are given in Sections 9.3.3 and 0.
12.4.4 CONTROL CABLE INSTALLATION
Reverse the steps detailed above for installation.