Documentation anomalies
Date issue released
Safety Issue Description

The engine manufacturer’s documents with respect to the propeller mounting flange were technically inconsistent with regard to painting and torqueing procedures.

Issue number
AO-2013-046-SI-03
Transport Function
Aviation: General aviation
Issue Owner
Jabiru Aircraft Pty Ltd
Mode of Transport
Aviation
Issue Status Justification

The documentary changes should ensure the increased reliability of the propeller flange/crankshaft joint and the reduced likelihood of propeller loss due to joint fastener failure.

Proactive action
Action number
AO-2013-046-NSA-016
Organisation
Jabiru Aircraft Pty Ltd
Action date
Action Status
Closed
Action description

On the matter of avoiding paint on all the propeller-mounting flange’s faying surfaces – additional text has been included within the engine overhaul manual to emphasise and strengthen the requirement. Additionally, the latest revision of the process specification, covering surface preparation and painting, unambiguously specifies the manuals’ requirement for nil paint below the cap screw washers and the crank and propeller faying surfaces. On the subject of consistency for the torqueing procedure, this has been amended in both relevant manuals to solely specify the one-step, dynamic torqueing process.