Cessna CW-6

Following development of the four-seat Model A the company designed a six-seat aircraft, the Model CW-6. The aircraft first flew in November 1928, powered by a 220 hp (164 kW) Wright Whirlwind J-5 radial engine. The aircraft was displayed at the 1929 Auto Show in Wichita, Kansas. A scaled-down four-seat version, the Cessna DC-6, was also developed.

Data from Manufacturers Specifications on American Commercial Airplanes as Compiled by Aviation[1]

General characteristics

• Crew: 1
• Capacity: 5 passengers
• Length: 29 ft 4 in (8.94 m)
• Wingspan: 43 ft 4 in (13.21 m)
• Height: 8 ft 2 in (2.49 m)
• Wing area: 296 sq ft (27.5 m²)
• Empty weight: 2,175 lb (987 kg)
• Gross weight: 3,950 lb (1,792 kg)
• Fuel capacity: 80 US gal (67 imp gal; 300 L)
• Powerplant: 1 × Wright J-6 Whirlwind radial engine, 300 hp (220 kW)

Performance

• Maximum speed: 148 mph (238 km/h, 129 kn)
• Cruise speed: 120 mph (190 km/h, 100 kn)
• Range: 610 mi (980 km, 530 nmi)
• Service ceiling: 17,500 ft (5,300 m)
• Rate of climb: 900 ft/min (4.6 m/s)

Wikimedia Commons has media related to Cessna CW-6.

• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
• "Cessna Building Six Place Plane". Aviation. Vol. XXV, no. 21. November 17, 1928. p. 1568.
• "Manufacturers Specifications on American Commercial Airplanes as Compiled by Aviation". Aviation. Vol. 28, no. 3. January 18, 1930. pp. inside front cover.