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AD FAA-2008-1095

Airworthiness Directives; Pratt & Whitney (PW) Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for Pratt & Whitney (PW) PW2037, PW2037(M), and PW2040 turbofan engines with certain fan blades with a cutback leading edge, installed. This AD was prompted by reports from PW that fan blade leading edge erosion can result in a fan thrust deterioration mode (FTDM) condition, a condition that cannot be detected by the crew, and that reduces the engine's capability of producing required thrust. This AD requires initial and repetitive maintenance to the leading edge of cutback fan blades or applying performance decrements as specified in the Airplane Flight Manual. We are issuing this AD to correct undetectable fan thrust deterioration on these PW products.

Directive Details

AD Number

FAA-2008-1095

Document Number

2012-6500

Type

Rule

Publication Date

March 20, 2012

Effective Date

April 24, 2012

Affected Manufacturer

Pratt & Whitney (PW) Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2008-1095

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Pratt & Whitney (PW) Turbofan →

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