Latécoère 225

Length
4.95 m
Flat Wing Span
8.03 m
Height
2.15 m
Flat Wing Area
11.85 m²
Flat Wing Aspect Ratio
5.4
Cruise Speed
85 km/h
Max Speed
120 km/h
Number of Engines
1
Aircraft Engine
First Flight
1984-07-18
Number Built
1
Maximum Take-Off Weight
0.258 t (paragliders: kg)
Total Fuel Capacity
23

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity
Latécoère 225 0.258 23

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All data (21 fields)
Name
Latécoère 225
Manufacturer
Latécoère
Description
The Latécoère 225 was an unusual single seat canard microlight amphibian, with a swept wing, and of pusher configuration.
First Flight
1984-07-18
Designer
Nono Larsen
Length (m)
4.95
Height (m)
2.15
Cockpit Crew
1
Max Speed (km/h)
120
Cruise Speed (km/h)
85
Min Speed (km/h)
45
Rate of Climb (m/s)
2.7
National Origin
France
Number Built
1
Powerplant Description
1 × JPX PUL 425 twin cylinder, horizontally opposed, air-cooled two-stroke, 18 kW (24 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Lat%C3%A9co%C3%A8re_225
Flat Wing Span (m)
8.03
Flat Wing Area (m²)
11.85
Flat Wing Aspect Ratio
5.4
Aircraft Engine
JPX PUL 425
Number of Engines
1