Bombardier Challenger 300
| Bombardier Challenger 300 | |
|---|---|
|
|
| Type: | Business jet |
| Design country: | |
| Manufacturer: | |
| First flight: |
August 2001 |
| Commissioning: |
2004 |
| Production time: |
In series production since 2004 |
| Number of pieces: |
> 290 |
The Bombardier Challenger 300 (also known as the Bombardier BD-100-1A10 Challenger 300 by the manufacturer ) is a super-midsize business jet for transcontinental distances from the Canadian company Bombardier Aerospace .
history
The project was started in 1998 and presented on July 13, 1999 at the Paris Air Show under the name Bombardier Continental . After extensive studies, the jet was renamed to its current name in September 2002. It made its maiden flight in August 2001. It was approved by the Canadian Aviation Safety Authority in May 2003, followed by the FAA in June 2003, the JAA in July 2003, the European Joint Aviation Authorities in August 2003 and the first delivery in January 2004 followed. More than 230 aircraft of this type had been delivered by mid-2008, 51 of which left the final assembly line in Montreal in 2007 alone.
The aircraft is equipped with modern avionics e.g. B. the Rockwell Collins Pro Line 21 glass cockpit equipped with 4 LCD screens (30 × 25 cm), FADEC and a TCAS system, as well as the modern cabin management and inflight entertainment system nice system ( Networked Integrated Cabin Equipment ) from Lufthansa Technik . It is manufactured in conventional metal construction with a few composite components. At EBACE 2013, the manufacturer announced that it would bring the Challenger 350 onto the market as a further development of the Challenger 300.
Technical specifications
| Parameters | Challenger 300 (up to serial number 20500) | Challenger 350 (from serial number 20501) |
|---|---|---|
| crew | Two (captain and copilot) | Two (captain and copilot) |
| capacity | up to 16 passengers (usually 8 to 9) | 10 passengers |
| length | 20.92 m | |
| span | 19.46 m | |
| height | 6.2 m | |
| Wing area | 48.5 m² | |
| Empty mass | 10,591 kg | |
| Max. Takeoff weight | 17,463 kg (17,622 kg with modifications) | 18,416 kg |
| Max landing mass | 15,309 kg | 15,490 kg |
| Max. Payload | 1,588 kg | |
| Max. Amount of fuel | 6,418 kg | |
| Cabin length | 8.72 m | |
| Cabin height | 1.85 m | |
| Cabin width | 1.55 - 2.19 m (depending on the height) | |
| Engines | 2 × Honeywell HTF7000 turbofan engines with 30.4 kN thrust each (35.81 kN are also specified as an alternative) + Honeywell 36-150BD auxiliary engine |
|
| Price (as of 2003) | $ 17.4 million (approx. € 11 million) | |
| Cruising speed | 850 km / h (max. 870 km / h) | |
| Range | 5,741 km at Mach 0.80 (with eight people on board) | |
| Service ceiling | 13,716 m (45,000 ft) | |
| Rate of climb | 25.4 m / s / approximately 5000 fpm at 17,622 kg (38,850 pounds) maximum gross weight | |
| Wing loading | 359.5 kg / m² | |
| Takeoff route | 1,466 m | |
| Landing route | 792 m | |
| Fuel consumption | 920 l / h at Mach 0.8 |
Comparable types
Web links
- Manufacturer site
- EASA-TCDS-A.080 (PDF; 45 kB) - Type certification of the Challenger 300
- Datasheet at www.aerospace-technology.com
- Data sheet at the Flug-Revue (e.g. with noise values)
Individual evidence
- ↑ FlugRevue October 2008, pp. 40–41, endurance runner - First Challenger 300 serviced at Aero-Dienst
- ↑ bizjournals.com: Bombardier announces launch of Challenger 350 Jet , May 20, 2013
- ↑ EASA Type Certificate Data Sheet EASA.IM.A.080 . European Aviation Agency website. Retrieved March 18, 2015.