AD 2013-15-09

final rule
Data completeness: 80%

Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

AD Number
2013-15-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0072
FR Citation
78 FR 49111

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

Unsafe Condition

Cracks in second-stage high-pressure turbine (HPT) air seals, which could lead to failure of the air seal and an uncontained engine failure, potentially causing damage to the airplane.

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

Required Actions

Inspect second-stage HPT air seals using eddy current inspection (ECI) or fluorescent-penetrant inspection (FPI). Remove from service any air seals that fail inspection. Disposition results according to the inspection criteria.

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

Compliance Time

Within five cycles after discovery of a failed inspection.

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

Affected Aircraft

Pratt & Whitney Division turbofan engines, models PW4074, PW4074D, PW4077, PW4077D, PW4084D, PW4090, and PW4090-3, with a certain second-stage HPT air seal part number installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.