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1.1 This specification addresses airworthiness requirements for the design and installation of electric propulsion systems for aeroplanes. Hybrid-electric propulsion systems are addressed implicitly unless explicitly stated otherwise. This specification was written with the focus on electric propulsion systems with conventional system layout, propulsion characteristics, and operation. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance.
Author | ASTM |
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Editor | ASTM |
Document type | Standard |
Format | File |
ICS | 49.050 : Aerospace engines and propulsion systems
49.060 : Aerospace electric equipment and systems |
Number of pages | 4 |
Replace | ASTM F3239-18 + Redline |
Year | 2019 |
Document history | ASTM F3239-18 + Redline |
Country | USA |
Keyword | ASTM 3239;ASTM F3239;ASTM F3239;10.1520/F3239-19 |