Document ID: chunk:federal_register_of_legislation:F2006B07396:body:0
Version: federal_register_of_legislation:F2006B07396
Segment Type: other
Provision Reference: 
Character Range: 0–1187

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/TFE731/13 Turbine Interstage Transition Duct Re-Inspection 6/86

 Applicability: TPE 731-2, -3, -3A, -3AR, -3B, -3BR, -3R engines.

 Requirement: In accordance with requirements of FAA AD 86-03-01 Amdt 39-5212.

            Reference Documents:

             FAA AD 86-03-01 Amdt 39-5212 Garrett SB TFE 731-72-3309 R1 Garrett SB TFE 731-72-3159 R5
            Compliance: At next major periodic inspection or at next access of affected part, whichever occurs first after 30 June 1986.

            Background:  This Directive has been issued to require re-inspection of certain turbine interstage transition ducts which were previously inspected by compliance with Garrett SB TFE731-72-3159 (AD/TFE731/7).

            The ducts, listed by serial number in Garrett SB TFE 731-72-3309 R1, are considered suspect following advice of an error in the inspection procedure carried out on the affected ducts during compliance with Garrett SB TFE 731-72-3159 (AD/TFE731/7).