| content | |||||||||||||||
| M-10 Cadet | |
|---|---|
| Role | Single engine aircraft |
| Manufacturer | Mooney |
| Designed by | Albert Mooney |
| First flight | 23 February 1968[1] |
| Number built | 59[2] |
| Unit cost | $11,310[2] |
The Mooney M-10 Cadet was a light aircraft manufactured by the Mooney Aircraft Company in the 1960s and '70s. The M-10 was similar in design to the A2A which was in production at the same time. Of the differences between the models, the M-10 had a traditional single tail vertical stabilizer while the A2A sported the dual vertical stabilizers. The basic design of the M-10 was based on the design of the ERCO Ercoupe which was purchased by Mooney in 1967.[1]
Specifications
General characteristics
- Length: 20 ft 8 in (6.3 m)
- Wingspan: 30 ft 0 in (9.1 m)
- Height: ft in (m)
- Wing area: ft² (m²)
- Empty weight: 950 lb (431 kg)
- Loaded weight: 1450 lb (658 kg)
- Useful load: 500 lb (227 kg)
- Max takeoff weight: lb (kg)
- Powerplant: 1× 90hp Continental C-90-16F, 90 hp (67.11 kW)
Performance
- Never exceed speed: 125 knots (144 mph, 232 km/h)
- Maximum speed: 103 knots (118 mph, 190 km/h)
- Cruise speed: 96 knots (111 mph, 179 km/h)
- Stall speed: 40 knots (46 mph, 74 km/h)
- Range: 484 nm (557 mi, 895 km)
- Service ceiling 12500 ft (3810 m)
- Rate of climb: 835 ft/min (4.24 m/s)
- Wing loading: lb/ft² (kg/m²)
- Power/mass: hp/lb (W/kg)
References
- ^ a b "Mid-Atlantic Air Museum - ERCO/SANDERS 415-G "ERCOUPE" Virtual Tour". Retrieved on 2007-01-30.
- ^ a b "Mooney Model Chronology". Retrieved on 2007-01-30.
- ^ "Type Certificate Data Sheet NO. A-787". Federal Aviation Administration (2005-07-14). Retrieved on 2007-01-30.
- ^ "Mooney M-10 Cadet Performance Information". Retrieved on 2007-01-30.
- ^ "Mooney". Retrieved on 2007-01-30.
