Bombardier Challenger 600 series
The Bombardier Challenger 600 series are business jets that have been in production since 1980. The aircraft was originally developed by Canadair, but at the beginning of production, the project was taken over and invested by Bombardier Aerospace.
Technically, it is a low-wing monoplane with jet propulsion, with two engines on the rear of the fuselage.
technical parameters Bombardier Challenger 650
| Manufacturer | Bombardier Aerospace |
| Role | Business jet |
| First flight | 8 November 1978 |
| Produced | 1980–present |
| Crew | Two (pilot and co-pilot) |
| Capacity | 2,200 kg (4,850 lb) and up to 19 passengers |
| Wingspan | 19.6 m (64 ft 4 in) |
| Length | 20.9 m (68 ft 5 in) |
| Height | 6.3 m (20 ft 8 in) |
| Wing area | 45.4 m2 (489 sq ft) |
| Aspect ratio | 8,46 |
| Max takeoff weight | 21,863 kg (48,200 lb) |
| Empty weight | 12,315 kg (27,150 lb) |
| Fuel capacity | 9,072 kg (20,000 lb) |
| Cabin | 1.83 m / 6 ft 0 in high, 2.41 m / 7 ft 11 in wide |
| Powerplant | 2 × General Electric CF34-3B turbofans, 41 kN (9,220 lbf) thrust each |
| Cruise speed | 854 km/h (531 mph, 461 kn) |
| Maximum speed | 854 km/h (531 mph, 490 kn) |
| Range | 7,408 km (4,603 mi, 4,000 nmi) |
| Service ceiling | 12,497 m (41,000 ft) |
| Wing loading | 481.6 kg/m2 (98.6 lb/sq ft) |
| Takeoff | 1,720 m / 5,640 ft (SL, ISA, MTOW) |
| Landing | 732 m / 2,402 ft (SL, ISA, typical) |
Bombardier Challenger 600 series
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