Airworthiness Directives; Honeywell International Inc. Turboprop Engines
airworthiness · Rule · Final rule. · Published 2018-11-05 · Effective 2018-12-10 · 83 FR 55255
Document
Document number
2018-23775
Federal Register citation
83 FR 55255
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Honeywell International Inc. Turboprop
Publication date
2018-11-05
Effective date
2018-12-10
FAA docket
Docket No. FAA-2018-0216
Abstract
We are superseding Airworthiness Directive (AD) 88-12-10 for certain Honeywell International Inc. (Honeywell) TPE331 turboprop engines. AD 88-12-10 required reducing the life limit for certain second stage turbine rotors. This AD requires removing certain second stage turbine rotors from service at a reduced life limit. This AD was prompted by report that a TPE331-11U engine experienced an uncontained rotor separation. In addition, cracks were discovered through eddy current inspection (ECI) in the bore of the second stage turbine rotor assembly after publication of AD 88-12-10. We are issuing this AD to address the unsafe condition on these products.