Resumen
We propose to adopt a new airworthiness directive (AD) for certain Saab AB, Saab Aeronautics Model SAAB 2000 airplanes. This proposed AD was prompted by a report that on some airplanes, during the paint removal process for repainting the airplane, the basic corrosion protection (anodizing and primer) coating was sanded down to bare metal on the aluminum skin panels and the bare metal might not have been treated correctly for corrosion prevention. This proposed AD would require an inspection of structural components of the airplane for any damaged protective coating; inspections of those areas for pitting corrosion, if necessary; a thickness measurement to determine if there is reduced skin thickness, if necessary; and repair, if necessary. We are proposing this AD to detect and correct damaged protective coatings. This condition could result in pitting corrosion damage; and reduced metal thickness, which could result in reduced static and fatigue strength of the airplane's structural parts.
Detalles de la directiva
Número de AD
FAA-2016-6668
Número de documento
2016-11171
Tipo
Proposed Rule
Fecha de publicación
May 13, 2016
Cierre de comentarios
June 27, 2016
Fabricante afectado
Saab AB, Saab Aeronautics (Type Certificate Previously Held by Saab AB, Saab Aerosystems)
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2016-6668
Temas
Documentos oficiales
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