Resumen
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. This AD was prompted by reports of cracking of the midspar fittings, and of the engine and nacelle strut separating from the airplane. This AD requires performing a detailed inspection of the midspar fittings of the nacelle strut to confirm that the correct part number is installed, and installing the correct part number if necessary; performing repetitive high frequency eddy current (HFEC) inspections of the midspar fittings of the nacelle strut for cracks, and repair if necessary; and performing repetitive general visual inspections of the nacelle struts to verify that the nacelle strut has not drooped below its normal position, applying the droop stripe to the nacelle strut and sailboat fairing if necessary, and performing repair if necessary. We are issuing this AD to detect and correct cracking of the midspar fitting, which could result in separation of the nacelle strut and engine from the airplane while in flight, and consequent loss of controllability of the airplane.
Detalles de la directiva
Número de AD
FAA-2012-0490
Número de documento
2012-19819
Tipo
Rule
Fecha de publicación
August 17, 2012
Fecha de entrada en vigor
September 21, 2012
Fabricante afectado
The Boeing Company
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2012-0490
Temas
Documentos oficiales
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