Canadair CL-84 Dynavert

· CANADAIR · 2 × Lycoming T53

Airplanes

Length

14.3256 m

Flat Wing Span

10.3632 m

Height

4.34 m

Flat Wing Area

21.6743 m²

Max Seating

Cruise Speed

484.4125 km/h

Max Speed

516.5994 km/h

Number of Engines

Aircraft Engine

First Flight

1965-05-07

Number Built

Maximum Take-Off Weight

6.5771 t (paragliders: kg)

Maximum Range

677.5338 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Canadair CL-84 Dynavert	6.5771	677.5338

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Learjet 25	General Electric CJ610	14.3256	10.668	8	Compare
HESA Yasin	General Electric J85	12.25	10.4		Compare
Learjet 24	General Electric CJ610	13.1064	10.668	6	Compare
Ryan XV-5 Vertifan	General Electric J85	13.56	9.09		Compare
North American Rockwell OV-10 Bronco		13.4112	12.192		Compare
AIDC T-5 Brave Eagle		14.5085	9.2354		Compare

All data (25 fields)

Name: Canadair CL-84 Dynavert
Manufacturer: CANADAIR
Description: The Canadair CL-84 "Dynavert", designated by the Canadian Forces as the CX-131, is a V/STOL turbine tiltwing monoplane designed and manufactured by Canadair between 1964 and 1972.
First Flight: 1965-05-07
Production End: 1972-01-01
Service End: 1974-01-01
Designer: CANADAIR
Type: Experimental VSTOL
Length (m): 14.3256
Height (m): 4.34
Cockpit Crew: 2
Max Seating: 12
Max Speed (km/h): 516.5994
Cruise Speed (km/h): 484.4125
Rate of Climb (m/s): 21.336
Capacity Description: 12 passengers
National Origin: Canada
Number Built: 4
Powerplant Description: 2 × Lycoming T53 shaft-turbines, 1119 kW (1500 hp) each
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/Canadair_CL-84_Dynavert
Flat Wing Span (m): 10.3632
Flat Wing Area (m²): 21.6743
Aircraft Engine: Lycoming T53
Number of Engines: 2