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Airworthiness Directives; Pratt & Whitney Canada PW206B, PW206C, PW206E, PW207D, and PW207E Turboshaft Engines

airworthiness · Rule · Final rule; request for comments. · Published 2004-07-19 · Effective 2004-08-03 · 69 FR 42855

Document

Document number
04-16005
Federal Register citation
69 FR 42855
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2004-07-19
Effective date
2004-08-03
FAA docket
Docket No. FAA-2004-18585

Abstract

The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney Canada (PWC) PW206B engines that have incorporated PWC Service Bulletin (SB) No. 28119, and PW206C, PW206E, PW207D, and PW207E turboshaft engines. This AD requires checking the automatic low-cycle- fatigue (LCF) counting data made by the engine Data Collection Unit (DCU) on installed engines, and validating proper DCU automatic LCF counting before an engine is installed. This AD results from two reports of irregular LCF counting, observed between engines on the same helicopter, during weekly recording of LCF data in the engine log books. We are issuing this AD to prevent critical rotating parts from exceeding published life limits, which could result in uncontained engine failure and possible loss of the helicopter.

Source

Authoritative
Federal Register document
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