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AD FAA-2014-0286

Airworthiness Directives; The Boeing Company Airplanes

Resumen

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600 and -700 series airplanes. This AD was prompted by reports of cracking in the body station (STA) 727 bulkhead lower frame. This AD requires a detailed and open hole high frequency eddy current (HFEC) inspection of the left- and right-side lower frame webs and inner chords for cracking, and corrective actions and preventative modifications if necessary. This AD also provides for optional terminating action of the repetitive inspections, under certain conditions. We are issuing this AD to detect and correct cracking in a bulkhead lower frame web and inner chord, which could result in a severed frame and induced skin cracks, and could lead to rapid decompression of the fuselage.

Detalles de la directiva

Número de AD

FAA-2014-0286

Número de documento

2015-09805

Tipo

Rule

Fecha de publicación

April 30, 2015

Fecha de entrada en vigor

June 4, 2015

Fabricante afectado

The Boeing Company

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2014-0286

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de The Boeing Company →

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