Bombardier CRJ-100 / 200
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Bombardier CRJ-100 / 200

Bombardier CRJ-100 / 200. Photo. Video. Driving salon.

 

The Bombardier CRJ-100 and CRJ-200 are the first and baseline aircraft in the Bombardier Canadair Regional Jet family of narrow-body passenger jet airliners for regional and local airlines. These aircraft were designed by the Canadian aircraft manufacturer Bombardier Inc. The CRJ-100/200 aircraft were built on the basis of the Canadair CL-600 regional business jet (Bombardier Challenger 600). The main visual difference between the CRJ-100/200 and the Challenger 600 executive jet is the fuselage lengthened by 6,09 meters and a larger wingspan.

Aircraft CRJ-100 / 200 have the form of a low-wing monoplane with swept-back shape. Aircraft engines located in the rear fuselage of circular cross section diameter 2,9 meters. The tail unit has a "T" -shaped.

 

CRJ-100 photo

Bombardier CRJ-100 fly

 

Officially, the work on the project «Canadair Regional Jet» began in March 1989 year, although preliminary research company for the construction of jet passenger aircraft for local airlines started in the two years prior to the announcement of the official program - in 1987 year.

The first model was built designation CRJ-100. On it were mounted engines General Electric CF34-3A1 with each thrust of 38.84 kN. Salon aircraft allowed to host 50 seats.

The first flight took place on CRJ-100 10 May 1991 years. Upon completion of all the tests in July 1992, the aircraft received a Canadian certificate of fitness for flight. And in January of next year, CRJ-100, was certified by the American (FAR) and European (JAR) lёtnym standards.

A version with an increased, up to 3000 kilometers, flight range was also released due to a larger supply of fuel. This version was designated CRJ-100ER. In 1992, the CRJ-100LR version was released, with a range of 3710 kilometers.

CRJ-100 photo salon

Bombardier CRJ-100 / 200 Salon

In 1995 Bombardier Inc. presented an improved modification of the aircraft - CRJ-200, with installed General Electric CF34-3B1 turbofan engines, each of which has a thrust of 38.81 kN. These engines have lower fuel consumption, which made it possible to increase the flight range of the basic version to 2700 kilometers. Also, thanks to new engines, the aircraft was able to operate in regions with hot climates and in high altitude conditions. During tests, the Bombardier CRJ-200 showed better flight characteristics than its predecessor, the CRJ-100. At the same time, the Bombardier CRJ-200 also had a passenger compartment with 50 seats.

The first production aircraft CRJ-200, were delivered in January 15 1996, the Austrian air carrier «Tyrolean Airways», based in the city of Innsbruck.

Almost immediately after the base model CRJ-200, versions of the CRJ-200ER and CRJ-200LR were released, with a flight range of 3045 and 3713 kilometers, respectively.

With the advent of new aircraft models CRJ-700 and CRJ-900, production of the CRJ-100 and CRJ-200 versions was suspended. According to official data, as of August 2006, a total of 938 CRJ-100 and CRJ-200 aircraft are in operation.

 

Best places of the cabin Bombardier CRJ 200 - Utair

 

CRJ 200 interior layout

Bombardier CRJ-100 / 200 scheme salon

 

Technical characteristics of the Bombardier CRJ-100 (CRJ-100 ER / LR) aircraft:

  • Bombardier CRJ-100 maiden flight: May 10, 1991
  • Start of production: c 1991 years
  • Length: 26,77 m.
  • Height: 6,22 m.
  • Wingspan: 21,21 m.
  • Empty weight: 13650 kg.
  • Wing area: 48,35 sq.m.
  • The diameter of the fuselage: 2,90 m.
  • Cruising speed: 786 km / h..
  • Maximum speed: 860 km / h..
  • Ceiling: 12500 m.
  • Flight range: 1850 km. (ER: 3000 km. / LR: 3710 km.)
  • Length of takeoff: 1600 m.
  • path length: 1450 m.
  • Engines: 2 x General Electric CF34-3A1 turbojet engine
  • Crew: 2 people
  • Number of seats: 50 places

 

Technical characteristics of the Bombardier CRJ-200 (CRJ-100 ER / LR) aircraft:

  • Start of production: c 1995 years
  • Length: 26,77 m.
  • Height: 6,22 m.
  • Wingspan: 21,21 m.
  • Empty weight: 13740 kg.
  • Wing area: 48,35 sq.m.
  • The diameter of the fuselage: 2,90 m.
  • Cruising speed: 786 km / h..
  • Maximum speed: 860 km / h..
  • Ceiling: 12500 m.
  • Flight range: 2700 km. (ER: 3045 km. / LR: 3713 km.)
  • Length of takeoff: 1770 m.
  • path length: 1480 m.
  • Engines: 2 x General Electric CF34-3B1 turbojet engine
  • Crew: 2 people
  • Number of passenger seats: 50 seats

 

Bombardier 200 videos

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