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Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

airworthiness · Rule · Final rule. · Published 2014-04-10 · Effective 2014-05-15 · 79 FR 19812

Document

Document number
2014-08008
Federal Register citation
79 FR 19812
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Turbomeca S.A. Turboshaft
Publication date
2014-04-10
Effective date
2014-05-15
FAA docket
Docket No. FAA-2007-27009

Abstract

We are superseding airworthiness directive (AD) 2007-19-09R1 for all Turbomeca S.A. Arriel 2B1 turboshaft engines that do not have modification TU157 incorporated. AD 2007-19-09R1 required replacement of the hydromechanical metering unit (HMU) with a serviceable HMU. This AD requires HMU replacement; reduction of the compliance interval; and inclusion of the power turbine C2 cycle consumption rate when determining compliance times. This AD was prompted by reports of ruptures on HMU constant delta pressure valves that have less than 2,000 hours in service. We are issuing this AD to prevent failure of the HMU, which could lead to damage to the engine, and damage to the aircraft.

Source

Authoritative
Federal Register document
Machine
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