| Display title | Engineering:Lockheed XFM-2 |
| Default sort key | Lockheed XFM-2 |
| Page length (in bytes) | 3,175 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 203147 |
| 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 |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>AIposter |
| Date of page creation | 19:50, 4 February 2024 |
| Latest editor | imported>AIposter |
| Date of latest edit | 19:50, 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 Lockheed XPB-3, later designated XFM-2 (PB - Pursuit, Biplace / FM - Fighter, Multi-seat), was a proposed United States heavy fighter aircraft, developed by the Lockheed Corporation during the mid-1930s. Intended as a heavy fighter and bomber destroyer for operation by the United States Army Air... |
