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Airworthiness Directives; International Aero Engines, AG Engines

airworthiness · Rule · Final rule. · Published 2024-06-11 · Effective 2024-06-26 · 89 FR 49094

Document

Document number
2024-12594
Federal Register citation
89 FR 49094
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
International Aero
Publication date
2024-06-11
Effective date
2024-06-26
FAA docket
Docket No. FAA-2024-0041

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain International Aero Engines, AG (IAE AG) Model V2500 engines. This AD was prompted by an analysis of an event involving an International Aero Engines, LLC (IAE LLC) Model PW1127GA-JM engine, which experienced a high-pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR-7) separation that resulted in an aborted takeoff. This AD requires performing an angled ultrasonic inspection (AUSI) of certain high-pressure turbine (HPT) 1st-stage hubs and HPT 2nd-stage hubs for cracks and replacing if necessary. This AD also requires accelerated replacement of certain HPT 1st-stage hubs and HPT 2nd-stage hubs. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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