avia.wikisort.org - Aeroplane

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.[1][2] Built by the Atlanta Aircraft Corporation and designed by George H. Prudden, Edward Whitehead was responsible for the sales of the aircraft.[2]

Prudden-Whitehead monoplane
Role	Ten-seat transport monoplane Type of aircraft
National origin	United States
Manufacturer	Atlanta Aircraft Corporation
Designer	George H. Prudden
First flight	1930
Number built	2

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.[2] 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.[2] Only two of the trimotors were built.[1]

Variants

PW-1

The first aircraft built registered N366W.[1]

PW-2

The second aircraft built registered N280V.[1]

Specifications

Data from [2]

General characteristics

• 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 0.88 in (4.29 m)
• Wing area: 662.5 sq ft (61.6 m²)
• Empty weight: 5,200 lb (2,359 kg)
• Gross weight: 7,735 lb (3,509 kg)
• Powerplant: 3 × Wright R-760 piston engine , 240 hp (179 kW) each

Performance

• Maximum speed: 145 mph (233 km/h, 126 kn)
• Cruise speed: 124 mph (199 km/h, 108 kn)
• Range: 620 mi (998 km, 540 nmi)
• Endurance: 5 hours 0 minutes
• Service ceiling: 15,000 ft (4,600 m)
• Rate of climb: 1,220 ft/min (76.2 m/s)

References

Notes

External links

• Media related to Prudden aircraft at Wikimedia Commons

---