| Display title | Engineering:Grob G 109 |
| Default sort key | Grob G 109 |
| Page length (in bytes) | 15,602 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 42606 |
| 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>OrgMain |
| Date of page creation | 16:53, 5 March 2023 |
| Latest editor | imported>OrgMain |
| Date of latest edit | 16:53, 5 March 2023 |
| 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 Grob G109 is a light aircraft developed by Grob Aircraft AG of Mindelheim Mattsies in Germany. It first flew (G109 prototype and then production G109A form) in 1980. The G109B followed in 1984. It is a two-seat self-launching motor glider in which the pilot and passenger or student sit side by side... |
