CTHRepealedLegislation
AD/BN-2/35 Amdt 2 - Airframe Structural Fatigue Life Limitations
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AD/BN-2/35 Amdt 2 - Airframe Structural Fatigue Life Limitations
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.