Commercial Aircraft Directory - Aircraft Specification

Bombardier - CRJ200 Series

The CRJ200 series, equipped with improved CF34-3B1 turbofans providing increased thrust and a 2.8% improvement in specific fuel consumption was launched on 18 September 1995 with an order from Tyrolean Airways, who took delivery of their first aircraft on 15 January 1996. The Series 200 supplanted the CRJ100 in production and is also available in ER and LR versions, which essentially mirror their 100 series counterparts, apart from the powerplant, the introduction of an improved flight management system and the installation of GPS equipment. The CRJ200B is optimised for hot and high performance and features more powerful CF34-3B1 turbofans. Corporate-configured versions of the CRJ were also offered, including the 18-30 passenger Corporate JetLiner and the more luxurious 15-19 passenger, longer range, Special Edition (SE). Production of the CRJ200 was closed in October 2005 and the Dorval production line switched over from April 2006, to the Challenger 850 corporate jet.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date:	10 May 1991
Certification date:

PRINCIPAL DIMENSIONS

Fuselage width:	2.69 m
Fuselage height:	6.22 m
Fuselage length:	24.38 m
Cabin length:	14.76 m
Cabin width:	2.57 m
Cabin height:	1.87 m
Cabin volume:	57 m³
Hold volume:	9 m³

WEIGHTS

Empty operating:	13,835 kg
Max zero fuel:	19,142 kg
MTOW:	21,523 kg
MLW:	20,276 kg
Standard fuel capacity:	8,081 kg
Max fuel capacity:	8,081 kg

SPEEDS

Normal cruise:	786 km/h
Max cruise:	860 km/h

PERFORMANCE

Long Range Cruise alt:	11,887 m
Max ceiling:	12,497 m
Take off field length:	2,110 m
Landing field length:	1,478 m
Max Payload Range:
Range notes:	Max Fuel calculated at 8081 litresl weighing 0.785kg/litre.
Max passengers:	52
Typical passengers:	50