| Manufacturer |
Aeromere |
| Description |
The Falco F8L is an Italian-designed lightweight 2-seater aerobatic aircraft. |
| First Flight |
1955-01-01 |
| Designer |
Stelio Frati |
| Type |
Homebuilt aircraft |
| Length (m) |
6.5 |
| Height (m) |
2.27 |
| Max Speed (km/h) |
325 |
| Cruise Speed (km/h) |
250 |
| Min Speed (km/h) |
98 |
| Max Ceiling (m) |
6004.56 |
| Rate of Climb (m/s) |
4.9987 |
| Capacity Description |
one passenger |
| National Origin |
Italy |
| Number Built |
90 |
| Powerplant Description |
1 × Lycoming O-320-B1A air-cooled flat-four engine, 119 kW (160 hp) each |
| Status |
Production completed (2014) |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Falco_F8L |
| Flat Wing Span (m) |
8 |
| Flat Wing Area (m²) |
10 |
| Flat Wing Aspect Ratio |
6.4 |
| Aircraft Engine |
Lycoming O-320 |
| Number of Engines |
1 |