Vultee V-1A

Crew: 2 crew members2 person <br />

Crew Type: pilot, co-pilot

Passenger Capacity: 8 passengers8 people <br />

Length: 37 ft11.278 m <br />

Wingspan: 50 ft15.24 m <br />

Height: 10.125 ft3.086 m <br />

Empty Weight: 5,332 lbs2.666 tons <br />2,418.553 kg <br />

Gross Weight: 8,500 lbs4.25 tons <br />3,855.532 kg <br />

Powerplant: 1 × Wright Cyclone R-1820-F2, 735 hp (548 kW)

Max Speed: 235 mph204.209 kts <br />435.22 km/h <br />

Cruise Speed: 215 mph186.83 kts <br />398.18 km/h <br />

Range: 1000 miles868.976 nm <br />1,852 km <br />

Service Ceiling: 20,000 ft6,096 m <br />

Summary

The Vultee V-1 was a 1930s American single-engined airliner built by the Airplane Development Corporation, designed by Gerard Vultee and financed by automobile manufacturer Errett Cord.

V-1A: Production variant with two crew and a 735 hp (548 kW) Wright Cyclone R-1820-F2 radial engine, 18-built and one converted from prototype.

CNAC Aircraft Data: Vultee V-1A

Below is all the known data available for this model of this aircraft used by C.N.A.C. They are sorted by: C.N.A.C. Service Start Date, Maker Number, C.N.A.C. Tail Number.

Tail #	Nickname	Maker #	Service Start	Service End	Crew	End Cause	Notes	Sources
44		23	2 July 1940			Unknown end date: From CAF. To CAF	Unsure of Makers number 23.
45		26	8 July 1940			Unknown end date: From CAF. To CAF	Unsure of Makers number 26.

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