AD 2008-07-01

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft Engines

AD Number
2008-07-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-21242
FR Citation
73 FR 15866

Applicability

TypeManufacturerModelDetails
engine Turbomeca Arriel 1B Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft Engines

Unsafe Condition

Failures of the 2nd stage turbine blades in Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines.

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

Required Actions

Add a 3,000 hour life limit to Arriel 1B 2nd stage turbine blades. Inspect and replace 2nd stage turbine blades as necessary to comply with the new life limit.

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

Compliance Time

Within 50 flight hours after 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 1B, 1D, 1D1, and 1S1 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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