AD 2012-18-03

final rule
Data completeness: 70%

Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

AD Number
2012-18-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2012-0228
FR Citation
77 FR 54791

Applicability

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

Unsafe Condition

Cracked 1st stage high-pressure turbine (HPT) air seal rings, which could lead to an internal oil fire, uncontained engine failure, and damage to the airplane.

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

Required Actions

Remove and replace the 1st stage HPT seal support and inspect the 1st stage HPT air seal ring.

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

Compliance Time

The next time the HPT module is removed from the engine, unless already done.

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

Affected Aircraft

Pratt & Whitney Division PW4000-94'' and PW4000-100'' turbofan engines having a 1st stage HPT seal support, part number (P/N) 55K601 (contained within assembly P/N 55K602-01) or P/N 50K532 (contained within assembly P/N 50K530-01), installed.

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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