Monocoupe 90
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The Monocoupe 90 was a two place, light cabin airplane built by Monocoupe Corporation, Robertson, Missouri.
[edit] Specifications (90)
[edit] General characteristics
- Crew: one, pilot
- Capacity: 1 passenger
- Length: 20 ft 10 in (6.35 m)
- Wingspan: 32 ft 0 in (9.76 m)
- Height: 6 ft 11 in (2.11 m)
- Wing area: ft² ( m²)
- Empty: 973 lb (441 kg)
- Loaded: 1,490 lb (676 kg)
- Maximum takeoff: lb ( kg)
- Powerplant: 1× Lambert R-266 radial, 90 hp (67 kW)
[edit] Performance
- Maximum speed: 115 mph (185 km/h)
- Range: 540 miles (869 km)
- Service ceiling: 15,000 ft (4,573 m)
- Rate of climb: ft/min ( m/min)
- Wing loading: lb/ft² ( kg/m²)
- Power/mass: 0.06 hp/lb (0.10 kW/kg)
[edit] Related content
Related development
Monocoupe 110 - Monocoupe 113
Comparable aircraft
Potez 36
Designation sequence
22 - 70 - 90 - 110 - 113 - 125
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