AD 2002-16-25

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Arriel Models 2 S1, 2 B, and 2 C Turboshaft Engines

AD Number
2002-16-25
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2001-NE-10-AD
FR Citation
67 FR 54338

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Arriel Models 2 S1, 2 B, and 2 C Turboshaft Engines

Unsafe Condition

Manufacturing investigation revealed pump bodies with below minimum material thickness, which could cause fuel leakage through thin, porous walls, reducing fuel pump fire resistance.

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

Required Actions

Conduct initial and repetitive visual inspections for fuel leaks. Replace fuel pumps found leaking fuel. Remove from service fuel pumps with pump wall thickness below minimum.

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

Compliance Time

Not specified in the provided text.

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

Affected Aircraft

Turbomeca S.A. Arriel models 2 S1, 2 B, and 2 C 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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