Stinson Junior (SM-2, SM-7, SM-8, R, S, W)
Light Utility Aircraft
The Stinson Junior is a series of single-engine three-to-four-seat touring and corporate aircraft produced by the US-American manufacturer Stinson Aircraft.
Crew | 1-2 | |
Passengers | 2-3 |
Propulsion | 1 Radial Engine | |
Engine Model | Lycoming R-680 | |
Engine Power | 160 kW | 215 hp |
Speed | 202 km/h | 109 kts 125 mph |
Service Ceiling | 4.115 m | 13.500 ft |
Range | 926 km | 500 NM 575 mi. |
Empty Weight | 1.021 kg | 2.250 lbs |
max. Takeoff Weight | 1.449 kg | 3.195 lbs |
Wing Span | 12,70 m | 41 ft 8 in |
Wing Area | 21,9 m² | 236 ft² |
Length | 8,81 m | 28 ft 11 in |
Height | 2,67 m | 8 ft 9 in |
First Flight | 1928 | |
Production Status | out of production | |
Total Production | > 500 | |
Developed from | Stinson SM-1 Detroiter |
Data for (Version) | Stinson SM-8A Junior | |
Variants | SM-2, SM-2AA, SM-2AB, SM-2AC, SM-7A, SM-7B, SM-8A, SM-8B, SM-8D, S, W, R, R-2, R-3, R-3-S |
[Photo-ID: 12338] © Karsten Palt 2016-04-10 | |
![]() | Stinson SM-8A Reg.: N408Y c/n: M-4243 built in 1932 |
EAA AirVenture Museum [Oshkosh, WI] |