EASA AD US-2020-03-16
Fuselage - Carry-Thru Spar Lower Cap - Inspection
Federal Register Volume 85, Number 35 (AD 2020-03-16) is a final rule airworthiness directive issued by the FAA addressing Textron Aviation Inc. Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, and T210M airplanes. It mandates inspections and corrective actions for the carry-thru spar lower cap due to fatigue cracking initiated by corrosion pits, which have caused in-flight structural failures. The directive also requires application of protective coatings and reporting inspection results to the FAA.
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 210 (Centurion)Textron Aviation 210GTextron Aviation T210GTextron Aviation 210HTextron Aviation T210HTextron Aviation 210JTextron Aviation T210JTextron Aviation 210KTextron Aviation T210KTextron Aviation 210LTextron Aviation T210LTextron Aviation 210MTextron Aviation T210M