| Display title | Engineering:Rolls-Royce RB.203 Trent |
| Default sort key | Rolls-Royce RB.203 Trent |
| Page length (in bytes) | 7,496 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 525400 |
| 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>Wincert |
| Date of page creation | 21:40, 26 June 2023 |
| Latest editor | imported>Wincert |
| Date of latest edit | 21:40, 26 June 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 Rolls-Royce RB.203 Trent was a British medium-bypass turbofan engine of around 10,000lb thrust designed for production in the late 1960s, bearing no relation to the earlier Rolls-Royce RB.50 Trent turboprop or the later high-bypass Rolls-Royce Trent turbofan. |
