-NEW- Aircraft Superjet_100

Im not sure what the format to submit a new aircraft or to know if it has been submitted in the past, but I posted 2 links of the info of the aircraft and engine consumption. This aircraft is already well into its certification, whereas the 787-8, is well, delayed for its first flight. I hope it is enough. Thx!

http://en.wikipedia....ki/Superjet_100
http://en.wikipedia....PowerJet_SaM146

ENGINE: POWERJET SaM146
Maximum Thrust: 14,000 to 17,500 lbf (62.3 to 77.8 kN)
Specific fuel consumption: 0.629 lb of fuel/hour per pound of thrust at cruise
Power-to-weight ratio:

Aircraft: Superjet 100
Measurement Superjet 100-75 Superjet 100-95
Crew 2 Pilots
Passenger capacity (seat pitch 32"):
one class configuration 78 98

Cruise speed LRC, mach 0.78

Required takeoff field length (MTOW, ISA, SL)
Basic, ft (m)
LR, ft (m)
4970 (1515)
4980 (1520)
5033 (1534)
5915 (1803)
Maximum flight altitude, ft
echelon 41,000
400
Range, full passenger payload
Basic, nm(km)
: LR, nm(km)
1570 (2900)
2460 (4550)
1590 (2950)
2390 (4420)
Maximum takeoff weight:
basic, lb (kg)
LR, lb (kg)
85,585 (38,820)
93,210 (42,280)
93,740 (42,250)
101,150 (45,880)
Maximum landing weight: lb (kg) 77,160 (35,000) 86,860 (39,400)
Maximum payload: lb (kg) 20,130 (9,130) 26,995 (12,245)
Length, ft (m) 86.74 (26.44) 98.23 (29.94)
Wingspan, ft (m) 91.20 (27.80)
Height, ft (m) 33.73 (10.28)
Wheelbase, ft (m) 30.34 (9.25) 36.9 (11.25)
Wheeltrack, ft (m) 18.83 (5.74)
Landing category (ICAO) IIIA, (IIIB)*
Powerplants Two SaM146 turbofan engines
Volume of cargo compartments, cu ft (m³) 530.07 (15.01) 775.8 (21.97)
Cabin width, in (mm) 127.48 (3238)
Cabin height, in (mm) 83.46 (2120)
Aisle width, in (mm) 20.08 (510)
Seat width, in (mm) 18.31 (465)