Falco F8L

· Aeromere · 1 × Lycoming O-320

Airplanes

Length

6.5 m

Flat Wing Span

8 m

Height

2.27 m

Flat Wing Area

10 m²

Flat Wing Aspect Ratio

6.4

Cruise Speed

250 km/h

Max Speed

325 km/h

Max Ceiling

6004.56 m

Number of Engines

Aircraft Engine

First Flight

1955-01-01

Number Built

Maximum Take-Off Weight

0.82 t (paragliders: kg)

Total Fuel Capacity

120

Maximum Range

1400 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Falco F8L	0.82	120	1400

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Aerotec A-122 Uirapuru	Lycoming O-320	6.6	8.5	Compare
Aerocar IMP		6.7056	8.8392	Compare
Coupé-Aviation JC-01	Continental O-200	6.4	8.35	Compare
Australian Lightwing SP-4000 Speed	Lycoming O-360	6.42	8	Compare
Blériot-SPAD S.25	Le Rhône	6.5	8.12	Compare
AESL Airtourer	Lycoming O-235	6.55	7.92	Compare

All data (24 fields)

Name: Falco F8L
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