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Special Conditions; Soloy Corporation, Soloy Dual Pac Engine (Formally Soloy Dual Pac, Inc.)

other · Rule · Final special conditions. · Published 1997-02-19 · 62 FR 7335

Document

Document number
97-4067
Federal Register citation
62 FR 7335
Type
Rule
Action
Final special conditions.
Category
other
Publication date
1997-02-19
FAA docket
Docket No. 93-ANE-14

Abstract

These special conditions are issued for the Soloy Corporation, Soloy Dual Pac engine (formally Soloy Dual Pac Inc.). This engine will have a novel design feature associated with its configuration. The Soloy Dual Pac engine is a propulsion system in which two Pratt & Whitney Canada (PWC) Model PT6 turbine engines are combined through a common gearbox to drive a single output propeller shaft. The Soloy Dual Pac engine is intended to provide a degree of continuous operation following the failure of one of the PWC Model PT6 engines. The applicable regulations do not contain adequate or appropriate safety standards for such a configuration. These special conditions contain the additional safety standards which the Administrator considers necessary to establish a level of safety equivalent to that established by the airworthiness standards of part 33 of the Federal Aviation Regulations (FAR).

Source

Authoritative
Federal Register document
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