airworthiness · Rule · Final rule. · Published 2016-12-30 · Effective 2017-02-03 · 81 FR 96362
Document
Document number
2016-31695
Federal Register citation
81 FR 96362
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Safran Helicopter
Publication date
2016-12-30
Effective date
2017-02-03
FAA docket
Docket No. FAA-2015-3753
Abstract
We are superseding airworthiness directive (AD) 2016-04-12, that applies to certain Safran Helicopter Engines, S.A. (formerly Turbomeca S.A.) Arriel 2B, 2B1, 2C, 2C1, 2C2, 2D, 2E, 2S1, and 2S2 turboshaft engines. AD 2016-04-12 required spectrometric oil analysis (SOA) inspection of the engine accessory gearbox (AGB), and, depending on the results, removal of the engine AGB. This AD requires initial and repetitive wear inspections of the engine AGB cover. This AD was prompted by a report of an uncommanded in-flight shutdown (IFSD) of an Arriel 2S2 engine caused by rupture of the 41-tooth gear, which forms part of the bevel gear in the engine AGB. We are issuing this AD to correct the unsafe condition on these products.