AD 2014-04-06

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2014-04-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0381
FR Citation
79 FR 9990

Applicability

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

Unsafe Condition

Deterioration of the splines on the high pressure (HP)/low pressure (LP) pump assembly drive shaft of the hydro-mechanical metering unit (HMU), which eventually interrupted the fuel supply to the engine.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Perform initial and repetitive inspections of the HMU high-pressure pump drive gear shaft splines and sleeve assembly splines for wear, corrosion, scaling, or cracks. Clean and inspect the sleeve assembly splines. Replace the HMU if it fails inspection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within specified HMU operating hours after the effective date, depending on HMU operating history.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All Turbomeca S.A. Arrius 2B1, 2B1A, 2B2, and 2K1 turboshaft engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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