General description
The Bombardier CRJ200 aircraft is designed to hold 50 passengers in a 4-abreast configuration with a lavatory and galley as standard equipment. There are two versions of the CRJ200: the CRJ200 ER and the CRJ200 LR. The Extended Range (ER) variant has a maximum take-off weight of 51,000 pounds (23,134 kg) and range of 1,345 nm (1,548 sm / 2,491 km). The Long Range (LR) model has a maximum take-off weight of 53,000 pounds (24,041 kg) and a range of 1,700 nm (1,956 sm / 3,148 km). The CRJ200 has outstanding performance, capable of max cruise speeds of Mach 0.81 (464 kts / 534 mph / 860 kph), and cruise altitudes up to 41,000 feet.
The Bombardier CRJ200 is powered by two General Electric CF34-3B1 turbofan engines that are flat rated to produce 9,220 pounds (41.01 kN) of take-off thrust. Originally developed for the United States Air Force, the CF34 family has over 20 million flight hours and is highly regarded as one of the most reliable and efficient powerplants built. The Bombardier CRJ200 Series' powerplant delivers a performance envelope comparable to that of a mainline jet. The aircraft is available with an engine option that provides exceptional high-altitude, hot-weather airfield performance for increased payload and profitability.
The CRJ200 is 87 feet, 10 inches (26.7 m) long with a wing span of 69 feet, 7 inches (21.2 m). The aircraft requires a radius of only 75 feet (22.86 m) to negotiate a 180-degree turn; a valuable asset at increasingly congested airports.
General
Flight Crew 2
Cabin Crew 1
Passengers 50
Engines
Number Two General Electric CF34-3B1 turbofans
Thrust 8,729 pounds (38.83 kN) thrust at take-off
Flat rating
- standard
- optional 9,220 pounds (41.01 kN) thrust APR*
73° F (ISA+8°C)
86° F (ISA+15°C)
* Uninstalled
Avionics
Collins Pro Line 4 six-tube EFIS
Two-screen EICAS
Dual attitude heading reference systems (AHRS)
Traffic alert and collision avoidance system (TCAS)
Collins digital weather radar
Dimensions
External:
Length overall 87 ft 10 in 26.77 m
Wingspan 69 ft 7 in 21.21 m
Wing area (net) 520.4 ft2 48.35 m2
Height overall 20 ft 5 in 6.22 m
Fuselage maximum diameter 8 ft 10 in 2.69 m
Turning Circle 75 ft 22.86 m
Internal:
Cabin length (excluding cockpit) 40 ft 6 in 12.34 m
Cabin maximum width (centreline) 8 ft 4 in 2.53 m
Cabin width (floor level) 7 ft 2 in 2.18 m
Maximum height 6 ft 1 in 1.85 m
Cabin floor area (excluding cockpit) 290.25 ft2 26.97 m2
Cabin volume 1,687 ft3 47.80 m3
Baggage volume (checked and on-board) 473 ft3 13.39 m3
Doors and exits:
Passenger door (LH, fwd)
Height 5 ft 10 in 1.78 m
Width 3 ft 0.91 m
Height to sill 5 ft 4 in 1.61 m
Baggage door (LH, aft)
Height 2 ft 9 in 0.84 m
Width 3 ft 7 in 1.09 m
Height to sill 5 ft 4 in 1.61 m
Service door (RH, fwd)
Height 4 ft 1.22 m
Width 2 ft 0.61 m
Height to sill 5 ft 4 in 1.61 m
Weights
Maximum ramp weight (CRJ200 ER) 51,250 lb 23,247 kg
Maximum ramp weight (CRJ200 LR) 53,250 lb 24,154 kg
Maximum take-off weight (CRJ200 ER) 51,000 lb 23,134 kg
Maximum take-off weight (CRJ200 LR) 53,000 lb 24,041 kg
Maximum landing weight 47,000 lb 21,319 kg
Maximum zero fuel weight 44,000 lb 19,958 kg
Operating weight empty 30,900 lb 13,835 kg
Maximum fuel load 14,305 lb 6,489 kg
Maximum payload 13,100 lb 5,942 kg
Performance
Range:
Maximum range at LRC, 220 lb. pax (100 kg. pax) NM SM KM
CRJ200 ER FAA 121 (50 pax) 1,345 1,548 2,491
CRJ200 LR FAA 121 (50 pax) 1,700 1,956 3,148
Speeds:
Mach kts. mph km/h
High cruise speed 0.81 464 534 860
Normal cruise speed 0.74 424 488 786
Airfield Performance:
CRJ200 ER
FAR take-off field length (SL, ISA) at MTOW 5,800 ft 1,768 m
FAR 121 landing field length (SL) at MLW 4,850 ft 1,479 m
CRJ200 LR
FAR take-off field length (SL, ISA) at MTOW 6,290 ft 1,918 m
FAR landing field length (SL) at MLW 4,850 ft 1,479 m
Fuel consumption per hour (cruise average) 325 U.S. gal/
271 Imp. gal 1,230 L
Ceiling:
Maximum operating altitude 41,000 ft 12,496 m
Noise Level:
Take-off
EPNdB
77.6 FAR 36
EPNdB
89
Approach 92.1 98
Sideline 82.4 94