AD/TPE 331/19 - Turbine Bearing Support Replacement and Pitch Control Sleeve Pin - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07427 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AlliedSignal (Garrett/AiResearch) Turbine Engines - TPE 331 Series

 

AD/TPE 331/19 Turbine Bearing Support Replacement and

Pitch Control Sleeve Pin - Inspection


3/86

 

Applicability:  TPE-331-3U-303G, -3UW-303G, -5-251C, -5-251K, -6-251M which are listed in the reference document by their S/Nos. and those additional engines which had SB TPE- 331-72-0055 incorporated.

 

Document: 1. AiResearch SB TPE-331-72-0087, Rev. 2; or 2. FAA AD No. 74-24-05, or

3. AD/AIR-T/24A.

 

Compliance: 1. For engines with less than 100 hours time in service - Within 25 hours time in service after 31 January 1975.

 

2.    For engines with more than 100 hours time in service - Within 300 hours time in service after 31 January 1975.

 

3.    For spare engines - Before installation in an aircraft after 31 January 1975.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.