Stinson 108
From Wikipedia, the free encyclopedia
The Stinson 108 was a popular general aviation aircraft produced by the Stinson aircraft company from immediately after World War II to 1950, when the company was bought by Piper aircraft. Production continued for a few years under Piper.
[edit] Specifications (108, 108-1, 108-2, 108-3 Voyager/Voyager Station Wagon)
[edit] General characteristics
- Crew: one, pilot
- Capacity: 2-3 passengers
- Length: 25 ft 3 in (7.70 m)
- Wingspan: 34 ft 0 in (10.36 m)
- Height: 7 ft 6 in (2.29 m)
- Wing area: ft² ( m²)
- Empty: lb ( kg)
- Loaded: 2,400 lb ( kg)
- Maximum takeoff: lb (1,090 kg)
- Powerplant: 1x Franklin 6A4-165-B3, 165 hp (123 kW)
[edit] Performance
- Maximum speed: 133 mph (213 km/h)
- Range: 500 miles ( 800 km)
- Service ceiling: 13,000 ft (4,000 m)
- Rate of climb: 650 ft/min ( 200 m/min)
- Wing loading: lb/ft² ( kg/m²)
- Power/Mass: hp/lb ( kW/kg)
- Takeoff roll: 620 feet (190 m)
- Landing roll: 290 feet (85 m)
reference http://www.stinsonflyer.com/avphoto/stnad-1c.jpg
[edit] Related content
Related development:
Comparable aircraft:
Designation sequence: 76 - 105 - 106 - 108
Lists relating to