AD/BEA 121/29 - Aircraft Fatigue Life
1AD/BEA 121/29 - Aircraft Fatigue Life
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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 Beagle B121 (Pup) Series Aeroplanes
AD/BEA 121/29 Aircraft Fatigue Life 9/95
Applicability: B121 Pup, all models.
Requirement: Retire the airframe from service before exceeding 17900 fatigue hours. Fatigue hours shall be calculated in accordance with Jetstream Alert Service Bulletin B121/101.
Note: CAA(UK) AD 014-03-95 refers.
Compliance: Effective 17 August 1995.
Background: The Beagle Pup has been allocated a mandatory fatigue life by the United Kingdom Civil Aviation Authority.