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FAA AD on Bombardier model DHC-8-400 series airplanes (2008-04-02)

Washington, Usa - To detect and correct cracking of the barrel nuts at the wing front spar wing-to- fuselage joints, which could result in reduced structural integrity of the wing-to-fuselage attachments and detachment of wing

Airworthiness Directive Federal Register Information [Federal Register: February 13, 2008 (Volume 73, Number 30)] [Page 8187-8190] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0167; Directorate Identifier 2008-NM-029-AD; Amendment 39-15374; AD 2008-04-02] RIN 2120-AA64 Airworthiness Directives; Bombardier...

fra/pec - 1085839
Rome, Italy, 02/14/2008 11:14
AVIONEWS - World Aeronautical Press Agency

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