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Safety and Certifiability Evaluation of Distributed Electric Propulsion Airplane in EASA CS-23 Category
Author(s) -
Joël Jézégou,
Umair Sufyan
Publication year - 2021
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/1024/1/012076
Subject(s) - certification , context (archaeology) , propulsion , airplane , aviation safety , aeronautics , aviation , airworthiness , agency (philosophy) , engineering , safety standards , systems engineering , aerospace engineering , reliability engineering , political science , paleontology , philosophy , epistemology , law , biology
Distributed Electric Propulsion (DEP) is one of the unconventional airplane architectures of interest in the quest for decreasing aviation environmental footprint. This configuration integrates strong and innovative couplings between systems and aircraft design disciplines. To address limitations of the traditional approach for certification and of the associated means of compliance when certifying innovative products, the European Union Aviation Safety Agency (EASA) issues in 2017 a novel certification philosophy that relies on high-level objective-based safety requirements. In this context, this paper presents a safety and certifiability evaluation of DEP airplane in EASA CS-23 category, with a methodology for aircraft-level safety assessment during preliminary design, a certification gap analysis with regards to existing means of compliance, and some proposals to clear the certification path for DEP configuration.

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