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Airworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines

airworthiness · Rule · Final rule. · Published 2018-07-05 · Effective 2018-08-09 · 83 FR 31325

Document

Document number
2018-14340
Federal Register citation
83 FR 31325
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Safran Helicopter
Publication date
2018-07-05
Effective date
2018-08-09
FAA docket
Docket No. FAA-2013-0024

Abstract

We are superseding Airworthiness Directive (AD) 2013-11-09 for all Safran Helicopter Engines, S.A., Arrius 2B1 and 2F turboshaft engines. AD 2013-11-09 required the repetitive replacement of the fuel injector manifolds and privilege injector, or only the privilege injector. This AD retains the repetitive hardware replacement requirements of AD 2013-11-09, but only allows replacement pipe injector preferred assembly, part number (P/N) 0 319 73 044 0, on the Arrius 2F engines. This AD was prompted by reports of engine flameouts as a result of reduced fuel flow due to the presence of coking. We are issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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