AD Amdt-39-11029

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney JT9D Series Turbofan Engines

AD Number
Amdt-39-11029
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-ANE-28-AD
FR Citation
64 FR 6784

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney JT9D Series Airworthiness Directives; Pratt & Whitney JT9D Series Turbofan Engines

Unsafe Condition

Cracks in the rear skirt of the diffuser case can lead to diffuser case rupture during takeoff roll, resulting in an uncontained engine failure and damage to the aircraft.

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

Required Actions

Inspect the rear skirt of the diffuser case using fluorescent penetrant inspection (FPI) for cracks. If cracks are found, blend down to minimum wall thickness to remove cracks, followed by another FPI to verify crack removal. Polish and shotpeen the area. If cracks persist after re-inspection, remove the diffuser case from service and replace it with a serviceable part.

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

Pratt & Whitney JT9D series turbofan engines, as specified in the AD.

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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