AD 2002-21-17

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines

AD Number
2002-21-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NE-11-AD
FR Citation
67 FR 65495

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney JT8D-200 Series Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines

Unsafe Condition

Reports of the flange between the fan duct case and the fan exit guide vane case separating due to a fan blade fracture event.

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

Required Actions

Install stops on the fan exit guide vane case to prevent the flange between the fan duct case and the fan exit guide vane case from separating due to a fan blade failure.

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

Affected Aircraft

Pratt & Whitney JT8D-200 series turbofan 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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