AD Amdt-39-10134

final rule
Data completeness: 70%

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

AD Number
Amdt-39-10134
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 96-ANE-35
FR Citation
62 FR 49135

Applicability

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

Unsafe Condition

Fracture of the high pressure turbine (HPT) shaft can result in uncontained release of engine fragments, engine fire, inflight engine shutdown, or possible aircraft damage.

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

Required Actions

Install and perform periodic inspections of temperature indicators on the No. 4 and 5 bearing compartment scavenge oil tube. Perform necessary corrective actions as identified.

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

Affected Aircraft

Pratt & Whitney JT8D-200 series turbofan engines, including those with containment hardware from AD 93-23-10.

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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