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AD FAA-2015-5816

Airworthiness Directives; The Boeing Company Airplanes

Resumen

We are adopting a new airworthiness directive (AD) for all 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, 747SR, and 747SP series airplanes. This AD was prompted by reports of cracking found in the splice plates, hinge fittings, terminal fittings, the upper skin of the outboard and center sections, upper chord, and rear spar webs before reaching the inspection interval specified in AD 2006-10-16. Cracked and fractured Maraging steel fasteners were also found. This AD requires repetitive inspections for cracking, an inspection to determine whether fasteners are magnetic, repetitive ultrasonic inspections for cracking and fractures of affected fasteners, and related investigative and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2015-5816

Número de documento

2016-29307

Tipo

Rule

Fecha de publicación

December 21, 2016

Fecha de entrada en vigor

January 25, 2017

Fabricante afectado

The Boeing Company

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2015-5816

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de The Boeing Company →

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