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Airworthiness Directives; International Aero Engines AG Turbofan Engines

airworthiness · Rule · Final rule. · Published 2016-09-02 · Effective 2016-10-07 · 81 FR 60582

Document

Document number
2016-21061
Federal Register citation
81 FR 60582
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
International Aero
Publication date
2016-09-02
Effective date
2016-10-07
FAA docket
Docket No. FAA-2016-4123

Abstract

We are adopting a new airworthiness directive (AD) for certain International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. This AD was prompted by the fracture of the high- pressure turbine (HPT) stage 2 hub during flight, which resulted in an in-flight shutdown (IFSD), undercowl fire, and smoke in the cabin. This AD requires inspecting the HPT stage 1 hub and HPT stage 2 hub, and, if necessary, their replacement with parts that are eligible for installation. We are issuing this AD to prevent failure of the HPT stage 1 or HPT stage 2 hubs, which could result in uncontained HPT blade release, damage to the engine, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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