AD 2014-07-06

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2014-07-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2007-27009
FR Citation
79 FR 19812

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Unsafe Condition

Reports of ruptures on hydromechanical metering unit (HMU) constant delta pressure valves that have less than 2,000 hours in service.

Required Actions

Replace the HMU; reduce the compliance interval; and include the power turbine C2 cycle consumption rate when determining compliance times.

Compliance Time

Within 100 HMU C2 cycles after the effective date of this AD; thereafter, replace the HMU at every 1,000 HMU C2 cycles or 1,500 HMU operating hours, whichever comes first.

Affected Aircraft

Turbomeca S.A. Arriel 2B1 turboshaft engines that do not have modification TU157 incorporated.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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