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Superjet 100-95LR Initial Operational Capability (IOC): 2014 Maiden Flight: 12 February 2013 Total Production: 33 Unitary Cost: USD$43 million Also Known As:SSJ100/95LR and Superjet 100-95 Long Range Origin:Russia Corporations: B/E Aerospace, Hamilton Sundstrand, Liebherr, Messier-Bugatti, Sukhoi Civil Aircraft Company (SCAC)* and Thales (*) lead contractor
Description: Sukhoi Civil Aircraft (SCA), a subsidiary of Sukhoi design bureau, is developing the Russian Regional Jet (RRJ) to fit into the regional and short-to-medium range routes market. The RRJ family of aircraft will be capable of seating 60, 75 or 95 passengers using a twin-engine airplane layout and varying the fuselage length while sharing the maximum number of components and systems among variants. The 95 percent of airframe, power plant, wing, flight deck and main systems commonality in the RRJ 60, RRJ 75 and RRJ 95 jetliners is the centerpiece of the RRJ. The program is projected to last over 10-15 years with first aircraft deliveries to western airlines scheduled for 2007/2008. The RRJ development is valued at $700 million.
Thales signed an agreement worth 70 million euros with Sukhoi Civil Aircraft to provide avionics for the new RRJ airplane on December 15, 2004. The avionics suite provided by Thales - which includes cockpit display, communication, navigation and surveillance systems - will be integrated into all RRJ models. The RRJ cockpit configuration will be similar to the Airbus A380 superjumbo. Boeing was providing support on the RRJ development. Liebherr-Aerospace SAS and many other suppliers have signed agreements on the RRJ program which is expected to boost the Russian aeronautic industry recovery. On 19 August 2005 Alenia Aeronautica, a Finmeccanica subsidiary, agreed to purchase at least 25 percent of SCA making possible a future RRJ production line in Italy.
The Sukhoi Superjet 100-95 Long Range, also known as SSJ100/95LR or originally RRJ 95LR, has a seating capacity for 98 passengers with the single-aisle cabin offering a high degree of comfort. The airplane is powered by two Powerjet SaM146 turbofan engines rated at 16,100-lb of thrust at takeoff each. Powerjet is a Safran (Snecma Group) and NPO Saturn joint venture and the SaM146 engines provides for easier and lower cost of maintenance. The Superjet 100/95LR jetliner has a maximum range in excess of 4,500 kilometers cruising at March 0.81 with a crew of four. Critical operations such as the take off and landing can be conducted on runways of 1,600 to 2,000 meters in length. The Long Range Superjet is 3,500 kilograms heavier than the Basic version. The SSJ100/95LR conducted its maiden flight on February 12, 2013, and is expected to enter revenue service by 2014/2015.
Superjet 100-95LR Specifications
Number of Engines: 2
Passengers: 98 Dimensions Cabin Height: 2.12 meter
Cabin Width: 3.24 meter
Height: 10.3 meter
Wingspan: 27.8 meter Performance Landing Run Distance: 1,630 meter
Max Range: 4,578 kilometer (2,472 nautical mile)
Take Off Run Distance: 2,052 meter Speed Cruise Speed: 0.81 mach (968 kph) Volume Fuel Tank Capacity: 15,805 liter Weight Max Landing Weight: 41,000 kilogram
Max Takeoff Thrust: 32,200 pound
Max Takeoff Weight: 49,450 kilogram (109,017 pound)
Max Zero Fuel Weight: 40,000 kilogram
CEP: Circular Error Probable
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Superjet 100-95LR News
There are 4 news between 8 Jul 2014 and 15 Jun 2015