AD 2005-11-01

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Arrius 1A Turboshaft Engines

AD Number
2005-11-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-21273
FR Citation
70 FR 30613

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Arrius 1A Turboshaft Engines

Unsafe Condition

A malfunction of the Free Turbine Overspeed Protection System can exist despite the DECU passing all functional tests specified in the Engine Maintenance Manual.

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

Required Actions

Initial testing of the DECU Free Turbine Overspeed Protection System must be conducted within 25 flight hours after the effective date. If the system fails the test, the DECU must be replaced before further flight. Repetitive testing must be conducted at each functional test of the DECU Free Turbine Overspeed Protection System.

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

Compliance Time

Within 25 flight hours after the effective date of the AD.

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

Affected Aircraft

Turbomeca S.A. Arrius 1A turboshaft engines, installed on, but not limited to, Eurocopter AS355N Twinstar helicopters.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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