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: 113 of 233
9
AILERON CONTROL SYSTEM
9.1
AILERON CONTROL SYSTEM
9.1.1 DESCRIPTION
The general arrangement of the aileron system used in Jabiru Aircraft is shown in drawings below:
Figure 77 and Figure 78.
The aileron control system is comprised of a control column and two enclosed push-pull cables fitted
with spherical bearings.
Due to space constraints not all different variations are shown herein. When ordering spare parts
provide as must detail as possible
– part description, aircraft model, serial number etc to Jabiru to
ensure accurate part identification.
WARNING
All spherical bearings must be fitted with a large washer on the outside of the through-bolt to
prevent the bearing case and cable releasing in the event of a bearing failure.
Figure 77
– Aileron Controls – Type 1
