| Display title | Engineering:Saturn AL-31 |
| Default sort key | Saturn AL-31 |
| Page length (in bytes) | 31,613 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 526033 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
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| 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>WikiG |
| Date of page creation | 23:11, 3 February 2024 |
| Latest editor | imported>WikiG |
| Date of latest edit | 23:11, 3 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 Saturn AL-31 is a family of axial flow turbofan engines, developed by the Lyulka design bureau in the Soviet Union, now NPO Saturn in Russia , originally as a 12.5-tonne (122.6 kN, 27,560 lbf) powerplant for the Sukhoi Su-27 long range air superiority fighter. The AL-31 currently powers... |
