EASA AD CF-2026-47R1
Wing – Wing Access Panels with Un-trimmed Stiffeners and/or Reduced Thickness - Inspection
Airworthiness Directive CF-2026-47R1 addresses inspection and modification requirements for wing access panels with un-trimmed stiffeners and/or reduced thickness on De Havilland Aircraft of Canada Limited model DHC-8 series 100, 200, and 300 aircraft. The directive focuses on ensuring that the right-hand wing access panel stiffener is trimmed and that correct thickness panels are installed to prevent potential ignition sources in the wing fuel tank. It applies to all serial numbers of the specified models.
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland Canada DHC-8-102De Havilland Canada DHC-8-103De Havilland Canada DHC-8-106De Havilland Canada DHC-8-201De Havilland Canada DHC-8-202De Havilland Canada DHC-8-301De Havilland Canada DHC-8-311De Havilland Canada DHC-8-314De Havilland Canada DHC-8-315De Havilland Aircraft of Canada Limited DHC-8 series 100De Havilland Aircraft of Canada Limited DHC-8 series 200De Havilland Aircraft of Canada Limited DHC-8 series 300