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Airworthiness Directives; Pratt & Whitney PW4090 and PW4090-3 Turbofan Engines

airworthiness · Rule · Final rule. · Published 2009-02-17 · Effective 2009-03-24 · 74 FR 7304

Document

Document number
E9-3041
Federal Register citation
74 FR 7304
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pratt & Whitney PW4090 and PW4090-3 Turbofan
Publication date
2009-02-17
Effective date
2009-03-24
FAA docket
Docket No. FAA-2007-29110

Abstract

The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney (PW) PW4090 and PW4090-3 turbofan engines with front turbine hub, part number (P/N) 53L601, installed. This AD reduces the published life limit of those front turbine hubs, from 12,000 cycles- since-new (CSN) to 9,370 CSN. This AD also removes from service those front turbine hubs using a drawdown schedule. This AD results from PW updating the low-cycle-fatigue (LCF) life analysis for front turbine hubs, P/N 53L601. We are issuing this AD to prevent an uncontained failure of the front turbine hub, resulting in an in-flight engine shutdown and possible damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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