| Display title | Engineering:Sonex Electric Sport Aircraft |
| Default sort key | Sonex Electric Sport Aircraft |
| Page length (in bytes) | 9,696 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 914757 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
| Number of redirects to this page | 0 |
| Counted as a content page | Yes |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Len Stevenson |
| Date of page creation | 16:19, 7 February 2024 |
| Latest editor | imported>Len Stevenson |
| Date of latest edit | 16:19, 7 February 2024 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
| Recent number of distinct authors | 0 |
Description | Content |
Article description: (description) This attribute controls the content of the description and og:description elements. | The Sonex Electric Sport Aircraft (ESA) was a two-place (one place with additional batteries) aircraft design that was under development by Sonex Aircraft, using the 80 hp (60 kW) Sonex e-Flight electric system for thrust. Sonex designed this aircraft as a part of an attempt to develop alternate... |