Resumen
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747- 200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SP, and 747SR series airplanes. This AD was prompted by a report indicating cracks at eight fastener hole locations in the fuselage skin lap splice between certain stations (STAs) at certain stringers. This AD requires repetitive inspections of the upper fastener row of the fuselage skin lap splice in a certain area for any crack, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2024-1882
Número de documento
2024-23537
Tipo
Rule
Fecha de publicación
October 11, 2024
Fecha de entrada en vigor
November 15, 2024
Fabricante afectado
The Boeing Company
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2024-1882
Temas
Documentos oficiales
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