AD 2000-20-01

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines

AD Number
2000-20-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-11-AD
FR Citation
65 FR 58640

Applicability

TypeManufacturerModelDetails
engine Turbomeca Arriel 1 Series Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines

Unsafe Condition

Reports of gas generator rear bearing failures, which could lead to an uncommanded engine shutdown.

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

Required Actions

Install a chip detector with electronic warning on the rear bearing oil return system in accordance with Turbomeca Service Bulletin No. 292 72 0163, Revision 1, dated April 3, 1996.

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

Compliance Time

Within 30 days from the effective date of this AD.

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

Affected Aircraft

Turbomeca Arriel 1 A, -1 A1, -1 A2, -1 B, -1 C, -1 C1, -1 C2, -1 D, -1 D1, -1 K, -1 K1, -1 S, and -1 S1 turboshaft engines installed on, but not limited to, Eurocopter AS 356 C, AS 356 C1, AS 356 N2, AS 350 B, AS 350 B2N, AS 350 D, AS 550 U2, Augusta A109K2, Sikorsky S76A, S76A+, S76A++, and S76C 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.