ARJ21
Maiden Flight: 2008
IOC: 2009
Total Production: 186
ARJ21B
Origin
China
Contractor/s
AVIC1 Commercial Aircraft Co.
Family Members
ARJ21-700
ARJ21-900
ARJ21F
Power plant:
CF34-10A (2)
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Description:
The ARJ21 is a twin-engine regional jet intended for the Chinese market. The aircraft is being developed by AVIC I Commercial Aircraft Co. Ltd. (ACAC) in China with the assistance of foreign companies that will supply components and major subsystems such as the aircraft's turbofan engines. The ARJ21 aim is to satisfy the growing demands of Chinese aviation market as well as the growing number of passengers. Despite ARJ21 has not been marketed as an aircraft family there will be two versions. The ARJ21 aircraft family seating capacity will range from 78 to 105 passengers.
Two variants with a seating capacity of 70 and 90 passengers are called to be developed under the ARJ21 project. The 90-passenger aircraft would a stretched version. The first prototype was planned to enter flight testing in 2006 with an entry into revenue service date slated for 2007 or 2008. The ARJ21 airplane has been designed to operate from small airports and replace larger passenger aircraft. In addition to the passenger transport role, ARJ21 might transport freight. The aerodynamic design features a T tail and blended winglets with the two engines located side-by-side at the rear fuselage.
In November 2002, ACAC signed a letter of intent (LOI) with General Electric Aircraft Engines (GEAE) selecting GEAE's CF34-10A engine to power the ARJ21 airplane. Both companies anticipated a market prospect for 500 airplanes over the next 20 years in China.
The ARJ21B is a wide-body 20-passenger business jet derived from the AVIC1 Commercial Aircraft Co (ACAC) ARJ21 regional jet. It features office area, attaches area, and sleeping area as well as specific room. The ARJ21B cabin provides comfort, quiet, and personal jet atmosphere. This twin-engine jet has been designed to transport as many as 20 passengers over ranges of 3,300 nautical miles (6,000+ km) while cruising at 0.80 Mach.
Specifications
Accommodation: Crew 2, Passengers 20
Dimensions: Height 8.4 m, Length 33.5 m, Wing Area 80 square meter, Wingspan 27.3 m
Weights: Fuel Load 16,386 kg (36,124 lb), Max Landing Weight 40,455 kg (89,187 lb), Max Ramp Weight 43,589 kg (96,096 lb), Max Takeoff Weight 43,500 kg (95,899 lb), Max Zero Fuel Weight 28,755 kg (63,393 lb), Min Weight 25,755 kg (56,779 lb), Payload 3,000 kg (6,614 lb)
Engine/s Performance: Thrust 30,664 lb (13,909 kg)
Performance: Cabin Height 2 m (7 ft), Cabin Width 3 ft (1.0 m), Ceiling 11,900 m (39,042 ft) One Engine Inoperative Ceiling 7,200-m, Cruise Speed Mach 0.80 (956 kph), Landing Run Distance 1,650 m (5,413 ft), Max Range 6,112 km (3,300 nm), Take Off Run Distance 1,900 m (6,234 ft), Top Speed Mach 0.82 (980 kph)
Other: Number of Engines 2
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