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FAA AD on Bombardier model DHC-8-400 series airplanes (2008-18-04)

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

Airworthiness Directive Federal Register Information Federal Register: [Page 51903-51906] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0356; Directorate Identifier 2008-NM-042-AD; Amendment 39-15661; AD 2008-18-04] RIN 2120-AA64 Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes...

fra/pec - 1094071
Rome, Italy, 09/10/2008 12:06
AVIONEWS - World Aeronautical Press Agency

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