Alpha 2000

Airplanes

Length

7.1 m

Flat Wing Span

8.33 m

Height

2.135 m

Flat Wing Area

13 m²

Flat Wing Aspect Ratio

5.34

Cruise Speed

234 km/h

Max Speed

257 km/h

Max Ceiling

3800 m

Number of Engines

Aircraft Engine

First Flight

1976-01-15

Maximum Take-Off Weight

1 t (paragliders: kg)

Maximum Range

796 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Alpha 2000	1	796

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cook Challenger	Lycoming O-320	6.7056	8.2296	3	Compare
ANF Les Mureaux 190		7.2	8.38		Compare
Aero A.19		7	8.4		Compare
Dalotel DM-165	Continental IO-346	6.96	8.4		Compare
Auster Aiglet Trainer	De Havilland Gipsy Major	7.0104	9.7536		Compare
Avro Type F	Viale 35 hp	7.01	8.53		Compare

All data (21 fields)

Name: Alpha 2000
Manufacturer: Alpha Aviation Co
Description: The Alpha Aviation Alpha 2000 is a two-seat, all-metal training and general aviation aircraft, designed by Chris Heintz and built in Hamilton, New Zealand.
First Flight: 1976-01-15
Designer: Chris Heintz
Type: Multipurpose civil aircraft
Length (m): 7.1
Height (m): 2.135
Cockpit Crew: 2
Max Speed (km/h): 257
Cruise Speed (km/h): 234
Min Speed (km/h): 85
Max Ceiling (m): 3800
Rate of Climb (m/s): 5.2
Powerplant Description: 1 × Avco Lycoming O-320-D2A air-cooled flat-four piston engine, 119 kW (160 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Alpha_2000
Flat Wing Span (m): 8.33
Flat Wing Area (m²): 13
Flat Wing Aspect Ratio: 5.34
Aircraft Engine: Lycoming O-320
Number of Engines: 1