Document ID: chunk:federal_register_of_legislation:F2020L01124:body:0:p2
Version: federal_register_of_legislation:F2020L01124
Segment Type: other
Provision Reference: 
Character Range: 2549–3837

the expelling of any moisture that may be present.
                Note 2:  United States of America Federal Aviation Administration (FAA) AD 64‑05‑06 is the source document for the requirements of this AD.
Compliance:        1. Unless previously accomplished, within 6 months after the commencement date of this AD and thereafter at each 100 hours' time in service or every 12 months, whichever occurs first.
                This AD commences on 17 September 2020.

Background:  There have been instances of failure through internal corrosion of the upper left and right hand members of the engine mount assembly, the point of failure being just above the weld junction with the horizontal members of the engine mount. This AD is issued to preclude the possibility of failures on Australian registered aircraft, which could result in the loss of the engine.
             An audit of the Australian Aircraft Register found that Swift Museum Foundation GC-1B aircraft have been on the register for some time and that requirements equivalent to the applicable FAA ADs have not previously been mandated in Australia for these aircraft.
             This AD mandates requirements equivalent to FAA AD 64-05-06.

Pieter van Dijk
Delegate of the Civil Aviation Safety Authority
25 August 2020