Bombardier CRJ-200 RusLine VQ-BBW
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Aircraft Data
The twin-engined short to medium range Regional Jet family pioneered the 50 seater regional jet market. The prototype was based on the CL-601 business jet, but with stretched fuselage and new wings and undercarriage. An EFIS cockpit was also fitted.
The CRJ-200 became the main production version of the short fuselage family. It had more efficient engines, with improved hot and high performance. Also available as the 200LR, extended range edition.
| Country of Origin | First Flight | No. Built | No. In Service | Crew | Passengers |
|---|---|---|---|---|---|
| Canada | 1995 | 710 | 700 | 2 | 50 - 52 |
Power
Uses the CF34-3B1, rated at 9220lb thrust.
| Engine Count | 2 | |
| Engine Variations | ||
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Dimensions
| Length | 26.97 m. 88 ft. 6 in. |
| Wing Span | 21.31 m. 69 ft. 11 in. |
| Height | 6.38 m. 20 ft. 11 in. |
| Empty Weight |
13753 kg.
30292 lbs.
Weights and performance for 200LR version |
| Max Weight | 24062 kg. 53000 lbs. |
Performance
| Max Speed | 739 kph 459 mph |
| Cruise Speed | 682 kph 424 mph |
| Ceiling | 10668 m. 35000 ft. |
| Normal Range | 2500 1350 nm km. |
| Max Range |
3713
2005
nm
km.
Max range with reserves. |
Display data using: Metric Imperial
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