Lockheed Hudson specs
| Manufacturer: | Lockheed |
| Country: |  United States of America |
| ICAO Type designator: | L14 |
| First flight: | 10 December 1938 |
| Production ended: | 1942 |
| Production total: | 2584 |
| Series: | A-28 Hudson: US Military version with R-1830-45 engines
A-28A Hudson: A-28 with convertible interiors as troop transports A-29 Hudson: A-28 powered by Wright R-1820-87 engines A-29A Hudson: A-29 with convertible interiors as troop transports Hudson I: Production aircraft for the RAF and RAAF Hudson II: Mk I with spinnerless constant speed propellers Hudson III: Production aircraft with retractable ventral gun position; 428 built. Hudson IIIA: Lend-lease variants of the A-29 and A-29A aircraft; 800 built. Hudson IV: Mk II with ventral gun removed Hudson IVA: A-28s delivered to the RAAF Hudson VI: A-28As under lend-lease |
| Propulsion: | 2 piston engines |
| Maximum number of passengers: | |
| Maximum take-off mass: | 8390 kg |
| ICAO Mass group: | 3 |
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