Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
863647 | Procedia Engineering | 2011 | 8 Pages |
Abstract
The methods of compliance presented here will enable improved verification technology to aero engines electrical and electronic control system. The approach is based on FAR 33.28, and the scope of this paper is to research the history of 33.28 and its amendments. Furthermore, combined with the current development of aircraft engine control system, this paper gives the compliance method to this regulation.
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