AD 98-19-03

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines

AD Number
98-19-03
Status
final_rule
Effective Date
Product Category
engine
Docket
98-ANE-02-AD
FR Citation
Federal Register: September 10, 1998 (Volume 63, Number 175)

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division PW4052 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4056 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4060 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4060A Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4062 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4152 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4156A Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4158 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4164 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines
engine Pratt & Whitney Division PW4168 Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines

Unsafe Condition

Cracking of the 2nd stage high pressure turbine (HPT) rotating airseals could result 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 2nd stage HPT rotating airseals using fluorescent penetrant and eddy current methods for cracks, remove cracked parts, replace with serviceable parts, modify 2nd stage ring segments and vane clusters, and install improved airseals per specified service bulletins.

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

Compliance Time

At the next hot section shop visit after the effective date (November 9, 1998), and at each subsequent hot section shop visit. Modifications must be completed within 6 years after the effective date.

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

Affected Aircraft

Pratt & Whitney Models PW4052, PW4056, PW4060, PW4060A, PW4062, PW4152, PW4156A, PW4158, PW4460, PW4462, PW4164, and PW4168 turbofan engines with 2nd stage HPT rotating airseals, Part Numbers 50L156 or 50L195 installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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