| Display title | Engineering:Doak VZ-4 |
| Default sort key | Doak VZ-4 |
| Page length (in bytes) | 10,203 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 920887 |
| 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 |
| Page image |  |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Ohm |
| Date of page creation | 17:23, 4 February 2024 |
| Latest editor | imported>Ohm |
| Date of latest edit | 17:23, 4 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 Doak VZ-4 (or Doak Model 16) was an American prototype Vertical Takeoff and Landing (VTOL) aircraft built in the 1950s for service in the United States Army. Only a single prototype was built, and the U.S. Army withdrew it from active trials in 1963. |
