| Display title | Engineering:Gribovsky G-23 |
| Default sort key | Gribovsky G-23 |
| Page length (in bytes) | 6,414 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 201295 |
| 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>WikiEditor |
| Date of page creation | 04:04, 10 July 2022 |
| Latest editor | imported>WikiEditor |
| Date of latest edit | 04:04, 10 July 2022 |
| 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 Gribovsky G-23 Komsomolyets 2 (Russian: Грибовский Г-23 Комсомолец 2) was a two-seat, single aircraft originally intended to explore the potential of a car-derived, water cooled inline engine for light aviation. It was built in the USSR in the 1930s. A second example was fitted with two different... |
