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AD FAA-2012-0228

Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for certain Pratt & Whitney Division PW4000-94" and PW4000-100" turbofan engines having a 1st stage high-pressure turbine (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. This AD was prompted by 58 reports of cracked 1st stage HPT air seal rings, including 15 in-flight engine shutdowns. This AD requires removal and replacement of the 1st stage HPT seal support and inspection of the 1st stage HPT air seal ring. We are issuing this AD to prevent failure of the 1st stage HPT air seal ring, which could lead to an internal oil fire, uncontained engine failure, and damage to the airplane.

Directive Details

AD Number

FAA-2012-0228

Document Number

2012-21821

Type

Rule

Publication Date

September 6, 2012

Effective Date

October 11, 2012

Affected Manufacturer

Pratt & Whitney Division Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2012-0228

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Pratt & Whitney Division Turbofan →

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