Birdman Chinook

Airplanes

Length

5.34 m

Flat Wing Span

10.68 m

Height

1.78 m

Flat Wing Area

13 m²

Cruise Speed

81 km/h

Max Speed

97 km/h

Max Ceiling

4575 m

Number of Engines

Aircraft Engine

First Flight

1982-12-12

Entry Into service

1983-01-01

Number Built

1100

Maximum Take-Off Weight

0.283 t (paragliders: kg)

Maximum Range

324 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Birdman Chinook	0.283	324

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aérostructure Lutin 80		5.1	11		Compare
Adaridi AD 3		5.3	11.6		Compare
Aerodyne Systems Vector		5.4864	10.729		Compare
Albatros L 59		5.4	10.3		Compare
Albatros L 60	Siemens-Halske Sh 5	5.4	10.3	1	Compare
Midwest Questar Sport		5.334	10.1346		Compare

All data (23 fields)

Name: Birdman Chinook
Manufacturer: Aircraft Sales and Parts
Description: The Birdman Chinook is a family of single and two-place, pusher configuration, high-wing ultralight aircraft that was first flown on 12 December 1982 and produced by Birdman Enterprises of Edmonton, Alberta, Canada, starting in 1983.
First Flight: 1982-12-12
Entry Into service: 1983-01-01
Designer: Vladimir Talanczuk
Length (m): 5.34
Height (m): 1.78
Max Speed (km/h): 97
Cruise Speed (km/h): 81
Min Speed (km/h): 39
Max Ceiling (m): 4575
Rate of Climb (m/s): 3.6
Capacity Description: one passenger
National Origin: Canada
Number Built: 1100
Powerplant Description: 1 × Rotax 277, 21 kW (28 hp) each
Status: Kits in production
Wikipedia Article (URL): en.wikipedia.org/wiki/Birdman_Chinook
Flat Wing Span (m): 10.68
Flat Wing Area (m²): 13
Aircraft Engine: Rotax 277
Number of Engines: 1