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| General characteristics UC-64A | |||
| Prime function | Light transport aircraft | ||
| Contractor | Noorduyn Avaition, Ltd., Montreal, Canada | ||
| Power plant | One Pratt&Whitney R-1340-AN-1 engine | ||
| Thrust | 590 HP | 440 kW | |
| Speed | max. | 162 mph | 260 km/h |
| cruising | 148 mph | 238 km/h | |
| Ceiling | 17,000 ft | 5,180 m | |
| Range | 597 miles | 960 km | |
| Freight | 10 seats | ||
| Crew | One or two (depending on mission) | ||
| First flight | 1935 | ||
| Cost | $28,000 | ||
Source: David Hanson´s American Aircraft of World War II
Jirka Wagner
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Last updated 01.10.2008