Challenger 800 • wp.archivoaereo.com

The Canadair CL-600-2B19 (Challenger 800) is a mid-range passenger aircraft designed for regional airlines. It was developed in 1995 by the Canadian company Canadair, which is part of Bombardier Aerospace. This model is a passenger variant of the Canadair CL-600 Challenger 601 business jet.

Its capacity ranges from 8 to 50 passengers, though in its business configuration, it can carry up to 19 occupants. It is distinguished by a fuselage lengthened by 6.09 meters and a larger wingspan, featuring vertical aerodynamic surfaces (winglets) installed at the wingtips.

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Performance and Engine Evolution

Initially, the Challenger 800 was equipped with CF34-3A1 turbofan engines, offering a range of more than 5,556 km and a maximum weight of 24,040 kg. Subsequent versions of the aircraft incorporated the CF34-3B1 engines.

These more advanced engines can develop a thrust of 8,364 kg at an air temperature of 35°C, increasing its range to 5,778 km. As a result, this modification allows the Challenger 800 to operate effectively in high-altitude conditions and hot climates.

Notable Operators

The Challenger 800 has been adopted by numerous regular airline operators. Among them are internationally renowned companies such as Lufthansa and Malev Hungarian Airlines, highlighting its reliability and versatility in the regional aviation sector.

Technical Specifications

Modification	Challenger 800
Wingspan, m	21.21
Aircraft length, m	26.77
Aircraft height, m	6.22
Wing area, m2	48.35
Empty weight	13740
Maximum takeoff weight	24040
Fuel capacity	8289
Engine type	2 General Electric CF34-3B1 Turbofan
Thrust, kN	2 x 38.84 (41 APR)
Maximum cruising speed, km/h	850
Normal cruising speed, km/h	820
Economical speed, km/h	786
Practical range, km	5778
Maximum rate of climb, m/min	1920
Practical ceiling, m	12497
Crew, чел	2+1
Payload:	14-19 passengers