| Display title | Engineering:Weslake A80 |
| Default sort key | Weslake A80 |
| Page length (in bytes) | 3,760 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 925638 |
| 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>Rtextdoc |
| Date of page creation | 18:29, 4 February 2024 |
| Latest editor | imported>Rtextdoc |
| Date of latest edit | 18:29, 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 Weslake A80 is a liquid cooled, two-stroke, opposed piston, 1332cc diesel aircraft engine, produced by Weslake. |
