| Display title | Engineering:Irkut MC-21 |
| Default sort key | Irkut MC-21 |
| Page length (in bytes) | 82,492 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 541664 |
| 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 | 13:05, 4 February 2024 |
| Latest editor | imported>Ohm |
| Date of latest edit | 13:05, 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 Irkut MC-21 (Russian: Иркут МС-21) is a single-aisle airliner, developed in Russia by the Yakovlev Design Bureau and produced by its parent Irkut, a branch of the United Aircraft Corporation (UAC), itself a 92%-owned subsidiary of Russia's state-owned aviation giant Rostec.
The program was launched... |
