We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GEnx-1B54, -1B58, -1B64, -1B67, and -1B70 turbofan engine models. This AD was prompted by reports of two separate, single engine in-flight shutdowns (IFSDs) caused by high-pressure turbine (HPT) rotor stage 1 blade failure. This AD requires inspection and conditional removal of affected HPT rotor stage 1 blades. We are issuing this AD to prevent failure of the HPT rotor stage 1 blades, which could lead to failure of one or more engines, loss of thrust control, and damage to the airplane.
Document
Airworthiness Directives; General Electric Company Turbofan Engines
We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GEnx-1B54, -1B58, -1B64, -1B67, and -1B70 turbofan engine models. This AD was prompted b...
Legal Citation
Federal Register Citation
Use this for formal legal and research references to the published document.
81 FR 9751
Web Citation
Suggested Web Citation
Use this when citing the archival web version of the document.
“Airworthiness Directives; General Electric Company Turbofan Engines,” thefederalregister.org (February 26, 2016), https://thefederalregister.org/documents/2016-04031/airworthiness-directives-general-electric-company-turbofan-engines.