| A/C | Manufacturer | Sukhoi | Sources: | |||||||
| Aircraft type | Superjet 100 | [1] | https://www.flightglobal.com/download?ac=73559 | |||||||
| Total number of operating A/C | 131 | [1] | [2] | https://www.superjetinternational.com/wp-content/uploads/SSJ100_Datasheet.pdf | ||||||
| Option/Variant | SSJ100/95B | [2] | [3] | http://www.ssj100rightnow.com/download/SSJ100_DEP_WEB_2016.pdf | ||||||
| Engine | No. of Engines | 2 | [2] | Comments: | ||||||
| Model | SaM146 | [2] | ¹ ISA, zero wind, LRC, typical reserves policy | |||||||
| Max. Rated Takeoff Thrust, T_TO [kN] | 71,6 | [2] | ||||||||
| Equivalent Power, P [kW] | - | |||||||||
| Propeller | - | |||||||||
| Cabin | Length, l_CABIN [m] | 20,42 | [2] | |||||||
| Max. Height, h_CABIN [m] | 2,12 | [2] | ||||||||
| Max. Width, d_F,I [m] | 3,24 | [2] | ||||||||
| Passenger Compartment Volume, V_CABIN [m³] | N/A | |||||||||
| Fuselage | Height, h_F [m] | N/A | ||||||||
| Width, w_F [m] | N/A | |||||||||
| Total | Length, l_A/C [m] | 29,94 | [2] | |||||||
| Span, b_W [m] | 27,8 | [2] | ||||||||
| Height, h_A/C [m] | 10,28 | [2] | ||||||||
| Landing Gear | Track, l_T [m] | N/A | ||||||||
| Wheelbase, l_WB [m] | N/A | |||||||||
| Wing | Area, S_W [m²] | N/A | ||||||||
| Taper ratio, λ_W | 0,26 | [3] | ||||||||
| 1/4 Chord Sweep, φ_25,W [°] | 25 | [3] | ||||||||
| Vertical Tail | Area, S_V [m²] | N/A | ||||||||
| Height, b_V [m] | 5,47 | [3] | ||||||||
| Taper ratio, λ_V | 0,305 | [3] | ||||||||
| 1/4 Chord Sweep, φ_25,V [°] | 33,5 | [3] | ||||||||
| Horizontal Tail | Area, S_H [m²] | N/A | ||||||||
| Span, b_H [m] | 10 | [3] | ||||||||
| Taper Ratio, λ_H | 0,27 | [3] | ||||||||
| 1/4 Chord Sweep, φ_25,H [°] | 30 | [3] | ||||||||
| Cruise | V_MO [kt] | 488 | [2] | |||||||
| M_MO [Mach] | 0,81 | [2] | ||||||||
| Cruise Speed, M_CR [Mach] | 0,78 | [2] | ||||||||
| Max. Certified Flight Level, h_MCR [FL] | 400 | [2] | ||||||||
| Cruise Altitude, h_CR [FL] | N/A | |||||||||
| Fuel | Unusable Fuel [l] | N/A | ||||||||
| Optional Fuel [l] | N/A | |||||||||
| Max usable fuel [l] | 15805 | [2] | ||||||||
| Range | Max. Payload, R_MPL [nm] | N/A | ||||||||
| Max. Pax, R_M,pax [nm] | 1645 | ¹[2] | ||||||||
| Max. Range, R_PLMR [nm] | N/A | |||||||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | N/A | ||||||||
| Max. Take-Off, m_MTO (MTOM) [kg] | 45880 | [2] | ||||||||
| Max. Landing, m_ML (MLM) [kg] | 41000 | [2] | ||||||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | 40000 | [2] | ||||||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | N/A | |||||||||
| Max. Payload, m_MPL (MPL) [kg] | N/A | |||||||||
| Payload at Max. Range, m_PLMR [kg] | N/A | |||||||||
| Cargo | Volume, V_CARGO [m³] | 21,76 | [2] | |||||||
| Cargo Capacity | - | |||||||||
| Max. Pallet Underfloor | - | |||||||||
| Seats | Max. Seats, n_M,SEAT | 108 | [2] | |||||||
| Std. Layout, n_SEAT | 98 | [2] | ||||||||