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AD FAA-2011-0652

Airworthiness Directives; The Boeing Company Airplanes

Resumen

We are adopting a new airworthiness directive (AD) for all The Boeing Company Model MD-90-30 airplanes. This AD was prompted by reports of cracks of the wing rear spar lower cap at the outboard flap, inboard drive hinge at station Xrs=164.000. This AD requires repetitive eddy current high frequency (ETHF) inspections for cracking on the aft side of the left and right wing rear spar lower caps at station Xrs=164.000, further ETHF inspections if cracks are found, and repair if necessary; and repetitive post-repair inspections, and repair if necessary. We are issuing this AD to detect and correct cracking of the left and right rear spar lower caps, which could result in fuel leaks and damage to the wing skin or other structure, and consequent loss of the structural integrity of the wing.

Detalles de la directiva

Número de AD

FAA-2011-0652

Número de documento

2012-26483

Tipo

Rule

Fecha de publicación

October 31, 2012

Fecha de entrada en vigor

December 5, 2012

Fabricante afectado

The Boeing Company

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2011-0652

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de The Boeing Company →

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