CX-131 / CL-84 Dynavert
| model | CL-84 | CL-84-1/ CL-84A |
| Manufacturer | Canadair Ltd., Canada | General Dynamics |
| Wing Span | 34 ft 8 in (10.6 m) | 10,06 m |
| Area of the wing | 32.67 m2 | |
| Length | 53 ft 7 1/2 in (16.3 m) | 14,41 m |
| Height | 17 ft 1 1/2 in (5.2 m) | 4,34 m |
| Weight, Empty | 8,775 lb (3,980 kg) | 3818 kg |
| Weight, Gross | 14,500 lb (6,577 kg) | 6577 kg |
| maximum take-off | 5710 kg | |
| Engines | two Lycoming T.53 Model LTC 1K-4C, turboprop | 2 HPD Lycoming T.53 Model LTC 1K-4C |
| Power | 2 x 1500 hp | 2 x 1500 |
| Cruising Speed | 309 mph (497 km/h) | 497 km / h |
| Max Speed | 321 mph (517 km/h) | 517 km / h |
| Rate of Climb | 4,200 ft (1,280 m)/min | 1280 m / min |
| Range | 420 mi (677 km) | 677 km |
| Practical ceiling | 6800 m | |
| Crew, people | 2 | 2 + 12 passengers |
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
