Document ID: chunk:federal_register_of_legislation:F2006B07413:body:0
Version: federal_register_of_legislation:F2006B07413
Segment Type: other
Provision Reference: 
Character Range: 0–1001

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series

 AD/TFE731/7
 Amdt 2

 Turbine Interstage Transition Duct 11/87

            Applicability: TFE 731-2, -3, -3A, -3AR, -3B, -3BR and -3R engines whose serial numbers are detailed in the Requirement document.

 Requirement: Action in accordance with GTEC SB TFE-731-72-3159R6.

            Compliance: Unless already accomplished, at the next major periodic inspection or at the next access of affected part whichever occurs first after 30 June 1986.

            Note: Compliance with the previous issue of this Directive satisfies compliance with this amendment.

 Background: This Directive is amended to reflect the manufacturers revision 6 of SB
            TFE 731-72-3159 which updates engine application and includes reference to FAA AD 81-24-08 which addresses this subject.