Document ID: chunk:federal_register_of_legislation:F2014L00670:body:0:p2
Version: federal_register_of_legislation:F2014L00670
Segment Type: other
Provision Reference: 
Character Range: 2890–4007

AD 2007-26-09 Amdt 39-15311, paragraph (k) refers.
Compliance:  Unless previously accomplished, the required actions for Normal Category aeroplanes and Utility and Aerobatic Category aeroplanes must be taken from the effective date of this AD.

             Note 4:  Compliance with AD/PHZL/79 Amdt 1 constitutes compliance with the equivalent requirement(s) of this AD.
             The effective date of this AD is 8 June 2014.
Background:  This AD was originally issued to require placards to be fitted to limit operation of the propeller at certain engine speeds.  This will prevent failure of the propeller blade due to vibration.  Engine speed limitations were previously published in amendments to the Australian Civil MkI an MkII Flight Manuals.

             AD/PHZL/79 Amdt 1, which became effective on 7 August 2003, corrected errors relating to the identification of undampered engines.

             This AD, AD/PHZL/79 Amdt 2, makes reference to the latest FAA AD which encompasses the equivalent requirement(s) of this AD.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

3 June 2014