|Role||Ten-seat transport monoplane|
|National origin||United States|
|Manufacturer||Atlanta Aircraft Corportation|
|Designer||George H. Prudden|
The Prudden-Whitehead monoplane (sometimes referred to as the Atlanta PW-1, PW-2 or the Prudden monoplane) is an American three-engined eight-seat commercial transport monoplane. Built by the Atlanta Aircraft Corporation and designed by George H. Prudden, Edward Whitehead was responsible for the sales of the aircraft.
Design and development
The Prudden-Whitehead monoplane is an all-metal low-wing cantilever monoplane with a monocoque fuselage and powered by three 240 hp (179 kW) Wright R-760 piston engines. It has a conventional fixed landing gear with a tailwheel. It has an enclosed passenger cabin for eight to ten passengers and a washroom and toilet. Only two of the trimotors were built.
- The first aircraft built registered N366W.
- The second aircraft built registered N280V.
Data from 
- Crew: 2
- Capacity: 8 to 10 passengers
- Length: 44 ft 10 in (13.67 m)
- Wingspan: 66 ft 6 in (20.27 m)
- Height: 14 ft 0⅞ in (4.29 m)
- Wing area: 662.5 ft2 (61.6 m2)
- Empty weight: 5200 lb (2359 kg)
- Gross weight: 7735 lb (3509 kg)
- Powerplant: 3 × Wright R-760 piston engine, 240 hp (179 kW) each
- Maximum speed: 145 mph (233 km/h)
- Cruise speed: 124 mph (199 km/h)
- Range: 620 miles (998 km)
- Endurance: 5 hours 0 min
- Service ceiling: 15000 ft ( m)
- Rate of climb: 1220 ft/min (76.2 m/s)
|Wikimedia Commons has media related to Prudden aircraft.|
- "American airplanes - Al - Av". www.aerofiles.com. 7 March 2009. Retrieved 7 July 2011.
- "The Prudden-Whitehead Monoplane - An American All-Metal Commercial Machine". Flight: 10–11. 2 January 1931.