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AD: Airbus

AD NUMBER: 2008-14-17
MANUFACTURER: Airbus
SUBJECT: Airworthiness Directive 2008-14-17
SUMMARY:
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: During fatigue tests (EF3) on the A340-600, multiple damage were found in the upper side shell structure at skin and frame (FR) 84 & 85 interface, from stringer 6 to 15 LH/RH. This damage occurred between 58,341 and 72,891 simulated Flight Cycles (FC). Due to the higher Design Service Goal and different design (e.g. skin thickness) A330-200 and A340-300 aircraft series, the damage assessment concluded on [a] potential impact on these aircraft series. * * * * * The unsafe condition is loss of integrity of the upper shell structure of the fuselage. We are issuing this AD to require actions to correct the unsafe condition on these products.

FMI: www.faa.gov/regulations_policies/airworthiness_directives/

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