CRJ-200
About CRJ 200 (Wikipedia)
The Bombardier CRJ200 (previously Canadair CRJ200) is regional jet designed and manufactured by Bombardier Aerospace between 1991 and 2006.
The 50 seat aircraft is powered by two GE CF34 turbofans, mounted on the rear fuselage. The CRJ200 has more efficient turbofan engines for lower fuel consumption, increased cruise altitude and speed. During the late 1990s, it was stretched into the CRJ700 series. Production ended in 2006 but many remain in service. In 2020, Mitsubishi Heavy Industries purchased the entire CRJ line from Bombardier, and will continue support for the aircraft.
Control
AG 1 - Thrust reverse (Works only on ground activated by pulling brakes).
AG 3 - Taxi light.
AG 4 - Logo light.
AG 5 - Landing light.
AG 6 - Strobe lights.
AG 7 - Navigation Lights.
AG 8 - Engines and beacon lights.
Speeds
SPEEDS MEASURED WITHOUT FLAPS OR TRIM
Stall: 125 knots.
Takeoff: 130 knots.
Landing: 130-155 knots.
Cruise: 335 knots.
Have a nice flight!
Specifications
General Characteristics
- Created On Android
- Wingspan 66.9ft (20.4m)
- Length 84.0ft (25.6m)
- Height 19.7ft (6.0m)
- Empty Weight 5,423lbs (2,459kg)
- Loaded Weight 26,935lbs (12,217kg)
Performance
- Power/Weight Ratio 1.752
- Horse Power/Weight Ratio 0.018
- Wing Loading 43.0lbs/ft2 (209.9kg/m2)
- Wing Area 626.4ft2 (58.2m2)
- Drag Points 6275
Parts
- Number of Parts 227
- Control Surfaces 9
- Performance Cost 1,428