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AD FAA-2010-0594

Airworthiness Directives; Pratt & Whitney JT8D-209, -217, -217A, -217C, and -219 Turbofan Engines

Summary

We are superseding an existing airworthiness directive (AD) for Pratt & Whitney (PW) JT8D-209, -217, -217A, -217C, and -219 turbofan engines. That AD currently requires revisions to the engine manufacturer's time limits section (TLS) to include enhanced inspection of selected critical life-limited parts at each piece-part opportunity. This new AD modifies the TLS of the manufacturer's engine manual and an air carrier's approved continuous airworthiness maintenance program to incorporate additional inspection requirements. This AD was prompted by PW developing, and the FAA approving, improved inspection procedures for the critical life-limited parts. The mandatory inspections are needed to identify those critical rotating parts with conditions, which if allowed to continue in service, could result in uncontained failures. We are issuing this AD to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.

Directive Details

AD Number

FAA-2010-0594

Document Number

2011-3347

Type

Rule

Publication Date

February 15, 2011

Effective Date

March 22, 2011

Affected Manufacturer

Pratt & Whitney JT8D-209, -217, -217A, -217C, and -219 Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2010-0594

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Pratt & Whitney JT8D-209, -217, -217A, -217C, and -219 Turbofan →

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