| Display title | Engineering:Klemm Kl 105 |
| Default sort key | Klemm Kl 105 |
| Page length (in bytes) | 3,435 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 924028 |
| 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>S.Timg |
| Date of page creation | 14:14, 30 May 2022 |
| Latest editor | imported>S.Timg |
| Date of latest edit | 14:14, 30 May 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 Klemm Kl 105 was a two-seat sport aircraft developed in Germany in 1938. It was a low-wing cantilever monoplane of conventional design with fixed, tailskid undercarriage, and side-by-side seating for two within an enclosed cockpit. Construction throughout was of wood, with the fuselage built using... |
