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AD FAA-2012-0060

Airworthiness Directives; Pratt & Whitney (P&W) Division Turbofan Engines

Resumen

We are adopting a new airworthiness directive (AD) for certain P&W PW4000 series turbofan engines. This AD was prompted by reports of 3rd and 4th stage vane fractures in the low-pressure turbine (LPT) of certain PW4000-94" and PW4000-100" turbofan engines. This AD requires dimensional inspections of LPT 3rd stage vanes and the rear turbine case, inspection of LPT 4th stage vanes at the next LPT overhaul and removal of vanes with non-conforming airfoil fillet radii and vanes with more than one strip and recoat repair. This AD also requires disassembly and reassembly of the 2nd stage high-pressure turbine (HPT) rotor and 3rd stage LPT rotor at the next HPT and LPT overhauls. We are issuing this AD to prevent 3rd and 4th stage vane fractures in the LPT, damage to the LPT rotor, uncontained engine failure, and damage to the airplane.

Detalles de la directiva

Número de AD

FAA-2012-0060

Número de documento

2012-23791

Tipo

Rule

Fecha de publicación

October 3, 2012

Fecha de entrada en vigor

November 7, 2012

Fabricante afectado

Pratt & Whitney (P&W) Division Turbofan

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2012-0060

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

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