Resumen
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of moisture in the wing- to-fuselage joint, between the mating front spar and rear spar frame segments. This AD requires a visual inspection of the fuselage front and rear spar frames, an ultrasonic test if applicable, other specified actions, and repair if necessary. The FAA is issuing this AD to address the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2023-1885
Número de documento
2024-15657
Tipo
Rule
Fecha de publicación
July 17, 2024
Fecha de entrada en vigor
August 21, 2024
Fabricante afectado
De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.)
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2023-1885
Temas
Documentos oficiales
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