AD/BN-2/35 Amdt 2 - Airframe Structural Fatigue Life Limitations

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Legislation au F2006B04747 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pilatus Britten-Norman BN-2 Series Aeroplanes

 

AD/BN-2/35

Amdt 2


Airframe Structural Fatigue Life Limitations 5/93

 

Applicability: All models.

 

Requirement: Retire from service the wing and wing attachment fuselage frames. Compliance: Before 28,000 hours in service.

Background: This amendment extends the interim fatigue life for the Islander series, based on a comparison with the results of the Trislander fatigue test. The manufacturer’s fatigue review of the Islander is not yet complete.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.