Document ID: chunk:federal_register_of_legislation:F2006B10041:body:0:p2
Version: federal_register_of_legislation:F2006B10041
Segment Type: other
Provision Reference: 
Character Range: 3035–3651

advised of an incident of an in-flight engine fire on a Model G-IV series aeroplane due to chafing of the power feeder cable assembly of an engine alternator. This Directive introduces actions intended to prevent interference and chafing between the alternator power feeder cables and adjacent structure, which could result in an electrical short circuit and consequent fire ignition source in the engine compartment.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 19 May 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 14 June 2000.