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Bombardier Challenger 300
The Challenger 300 is the original version of the BD-100, a midsize business jet with a T-tail and two Honeywell AS907-1-1A turbofans on the rear fuselage. The EASA data sheet gives a length of 20.9 meters, a wingspan of 19.4 meters, a height of 6.2 meters, a maximum takeoff weight of 17,463 kg, a ceiling of 45,000 feet and usable fuel of 7,934 liters. It treats later airplanes, from serial number 20501, as the Challenger 350. The sources read give the 300 no speed or range with a stated load, so those are left empty.
- Engines
- Two Honeywell AS907-1-1A turbofans at the tail
- Max takeoff weight
- 38,500 lb (17,463 kg)
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Specifications
| Length | 68 ft 7 in (20.90 m) |
|---|---|
| Wingspan | 63 ft 8 in (19.40 m) |
| Height | 20 ft 4 in (6.20 m) |
| Ceiling | 45,000 ft (13,700 m) |
| Fuel capacity | 2,100 US gal (7,934 L) |
| Status | In service |
| Type codes | ICAO CL30 |
Private aircraft show specs only. No flight data is shown for them.