AD 2005-17-17

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Arrius 2F Turboshaft Engines

AD Number
2005-17-17
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-22039
FR Citation
70 FR 50164

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Arrius 2F Turboshaft Engines

Unsafe Condition

Excessive swelling of the O-ring on the check valve piston in the lubrication unit, caused by the class of oil used (STD or HTS) and engine operating time, can interrupt engine lubrication, leading to an uncommanded in-flight shutdown.

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

Required Actions

Replace the O-ring on the check valve piston in the lubrication unit at specified intervals based on oil class and engine operating time. Use Turbomeca Alert Service Bulletin No. A319 79 4802 for replacement procedures.

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

Compliance Time

Within 300 hours TSN or 50 hours after the effective date for HTS or unknown oil; within 450 hours TSN or 50 hours after the effective date for STD oil. Thereafter, replace the O-ring within 300 hours TSR for HTS oil or 500 hours TSR for STD oil.

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

Affected Aircraft

Turbomeca S.A. Arrius 2F turboshaft engines installed on, but not limited to, Eurocopter EC120B 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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