| Display title | Engineering:CFM International LEAP |
| Default sort key | CFM International LEAP |
| Page length (in bytes) | 47,153 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 525985 |
| 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>Nautica |
| Date of page creation | 22:50, 3 February 2024 |
| Latest editor | imported>Nautica |
| Date of latest edit | 22:50, 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 CFM International LEAP ("Leading Edge Aviation Propulsion") is a high-bypass turbofan engine produced by CFM International, a 50–50 joint venture between American GE Aerospace (formerly GE Aviation) and French Safran Aircraft Engines (formerly Snecma). It is the successor of the CFM56 and competes... |
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