AD 2002-14-26

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Arriel Models 1A, 1A1, 1B, 1D, and 1D1 Turboshaft Engines

AD Number
2002-14-26
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NE-35-AD
FR Citation
67 FR 47682

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Arriel Models 1A, 1A1, 1B, 1D, and 1D1 Turboshaft Engines

Unsafe Condition

The cantilevered axis of the free turbine moving from its design position and inducing blade trajectories outside the current design free turbine containment area, which can lead to uncontainment of the free turbine during an overspeed event.

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

Required Actions

Install containment shield rings around the free turbine blade area. Install a double support around the gearbox free turbine bearing housing.

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

Compliance Time

Before further flight.

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

Affected Aircraft

Turbomeca S.A. Arriel models 1A, 1A1, 1B, 1D, and 1D1 turboshaft engines.

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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