2008 Bombardier Challenger 300
The baseline Challenger 300 was launched at the 1999 Paris Air Show as the Bombardier Continental.[5] An all-new design, it received Transport Canada type approval on 31 May 2003, followed on 4 June by US FAR 25 certification and on 31 July by European JAR 25 approval.[6]Assembled in Wichita, Kansas, it entered commercial service on 8 January 2004 with Flexjet.[7] The new design is not developed from the Challenger 600 or its variants.
Its supercritical wings have a fixed leading-edge and a 27% sweep angle, its 1.15 m (3.8 ft) winglets reduce cruise lift-induced drag by 17%. It climbs to FL410 in 18 min with a 455 kg (1,003 lb) fuel burn at MTOW/ISA, where at a 14,330 kg (31,590 lb) weight it burns 680 kg (1,500 lb)/h at Mach 0.8/445 kn (824 km/h) tas, 875 kg (1,929 lb)/h at Mach 0.83/465 kn (861 km/h) tas.[6] In 2004, the unit cost of the Challenger 300 was US$17.4 million.[6]
The fuselage and the wing are semi-monocoque aluminum structures, the winglets are composite. Outboard ailerons are manually actuated, elevators and rudder are hydraulic with a mechanical backup, fly-by-wire spoilers augment roll control, act as speedbrakes and dump lift on the ground, hydraulic single-slotted fowler flap have four positions: 0/10/20/30°.[8] The Rockwell Collins Pro Line 21 avionics include four LCD displays, an EICAS and Maintenance Diagnostics Computer, an EGPWS, a TCAS II and an ELT.[9]
| Variant | Challenger 300[9] | Challenger 350[13] |
|---|---|---|
| Crew | two | |
| Capacity | eight to nine | nine (standard) |
| Length | 68.63 ft / 20.92 m | |
| Span | 63.84 ft / 19.46 m | 69 ft 0 in / 21.0 m |
| Height | 20.33 ft / 6.20 m | 20 ft 0 in / 6.1 m |
| Wing Area | 523 ft2 / 48.5 m2 | |
| Aspect ratio | 7.81 | 9.09 |
| MTOW | 38,850 lb / 17,622 kg | 40,600 lb / 18,416 kg |
| OEW | 23,500 lb / 10,659 kg | 24,800 lb / 11,249 kg |
| Fuel capacity | 14,150 lb / 6,418 kg | |
| Maximum payload | 3,500 lb / 1,588 kg | 3,400 lb / 1,542 kg |
| Wing loading | 74.3 lb/ft2/ 363.3 kg/m2 | 77.6 lb/ft2 / 379.7 kg/m2 |
| Turbofans (2×) | Honeywell HTF7000 | Honeywell HTF7350 |
| Thrust[a] | 6,826 lbf / 30.4 kN | 7,323 lbf / 33 kN |
| Maximum speed | Mach 0.83 / 477 kn / 882 km/h | Mach 0.83 / 477 kn / 882 km/h |
| Cruise speed | Mach 0.80 / 459 kn / 850 km/h | |
| Range[b] | 3,100 nmi / 5,741 km | 3,200 nmi / 5,926 km |
| Ceiling | 45,000 ft / 13,716 m | |
| Takeoff[c] | 4,810 ft / 1,466 m | 4,835 ft / 1,474 m |
| Landing[d] | 2,600 ft / 792 m | 2,710 ft / 826 m |
