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Jabiru j430 - Aileron Control System

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Aircraft Technical Manual
Jabiru Aircraft Pty Ltd
JTM001-5
J120, J160, J170, J200/J400, J230/J430, J250/J450 Variants
This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled.
ISSUE
1
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Dated: 29th October 2014
Issued By: AS
Page: 141 of 298
6D Aileron Control System
6.50 Aileron Control System (all J-Series)
6.50.1 Description
The general arrangement of the aileron system used in Jabiru Aircraft is shown in drawings below:
Figure 87 and Figure 88.
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 87 Aileron Controls Type 1

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