| A/C | Manufacturer | Saab | Sources: | ||||||||
| Aircraft type | Saab 340 | [1] | https://www.flightglobal.com/download?ac=73559 | ||||||||
| Total number of operating A/C | 188 | [1] | [2] | https://www.saabaircraftleasing.com/prod/dataSheets/340Brochure.pdf | |||||||
| Option/Variant | 340B | [2] | [3] | https://www.saabaircraftleasing.com/prod/datasheets/340b_jar.pdf | |||||||
| Engine | No. of Engines | 2 | [2] | [4] | https://www.easa.europa.eu/downloads/7388/en | ||||||
| Model | GE CT7-9B | [4] | [5] | https://perma.cc/UVV9-E9EE | |||||||
| Max. Rated Takeoff Thrust, T_TO [kN] | - | [6] | https://perma.cc/AKV8-BKHE | ||||||||
| Equivalent Power, P [kW] | 1395 | [4] | Comments: | ||||||||
| Propeller | 14 RF-19 | [4] | ¹ ISA standard day, zero wind, 10 min maneuvering, 45 min holding at 5000 ft, 100 nm alternate | ||||||||
| Cabin | Length, l_CABIN [m] | 10,4 | [2] | ² without wingtips: 21,44 | |||||||
| Max. Height, h_CABIN [m] | 1,8 | [2] | ³ without wingtips: 41,8 | ||||||||
| Max. Width, d_F,I [m] | 2,2 | [2] | ⁴ without wingtips: 0,4 | ||||||||
| Passenger Compartment Volume, V_CABIN [m³] | 33,4 | [3] | |||||||||
| Fuselage | Height, h_F [m] | 2,31 | [5] | ||||||||
| Width, w_F [m] | 2,31 | [5] | |||||||||
| Total | Length, l_A/C [m] | 19,73 | [3] | ||||||||
| Span, b_W [m] | 22,7 | ²[3] | |||||||||
| Height, h_A/C [m] | 6,97 | [3] | |||||||||
| Landing Gear | Track, l_T [m] | 6,7 | [5] | ||||||||
| Wheelbase, l_WB [m] | 7,14 | [5] | |||||||||
| Wing | Area, S_W [m²] | 43,11 | ³[6] | ||||||||
| Taper ratio, λ_W | 0,37 | ⁴[5] | |||||||||
| 1/4 Chord Sweep, φ_25,W [°] | 4,5 | [5] | |||||||||
| Vertical Tail | Area, S_V [m²] | 10,4 | [6] | ||||||||
| Height, b_V [m] | 3,74 | [6] | |||||||||
| Taper ratio, λ_V | 0,38 | [5] | |||||||||
| 1/4 Chord Sweep, φ_25,V [°] | 32 | [5] | |||||||||
| Horizontal Tail | Area, S_H [m²] | 14,57 | [6] | ||||||||
| Span, b_H [m] | 9,24 | [5] | |||||||||
| Taper Ratio, λ_H | 0,4 | [5] | |||||||||
| 1/4 Chord Sweep, φ_25,H [°] | 5 | [5] | |||||||||
| Cruise | V_MO [kt] | 283 | [2] | ||||||||
| M_MO [Mach] | 0,47 | [2] | |||||||||
| Cruise Speed, M_CR [Mach] | N/A | ||||||||||
| Max. Certified Flight Level, h_MCR [FL] | 250 | [4] | |||||||||
| Cruise Altitude, h_CR [FL] | 190 | [5] | |||||||||
| Fuel | Unusable Fuel [l] | 60 | [5] | ||||||||
| Optional Fuel [l] | - | ||||||||||
| Max usable fuel [l] | 3220 | [4] | |||||||||
| Range | Max. Payload, R_MPL [nm] | 330 | ¹[5] | ||||||||
| Max. Pax, R_M,pax [nm] | 470 | ¹[3] | |||||||||
| Max. Range, R_PLMR [nm] | 1220 | ¹[5] | |||||||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | 13740 | [4] | ||||||||
| Max. Take-Off, m_MTO (MTOM) [kg] | 13605 | [4] | |||||||||
| Max. Landing, m_ML (MLM) [kg] | 12930 | [4] | |||||||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | 12020 | [4] | |||||||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | 8620 | [2] | |||||||||
| Max. Payload, m_MPL (MPL) [kg] | 3400 | [2] | |||||||||
| Payload at Max. Range, m_PLMR [kg] | 2450 | [2] | |||||||||
| Cargo | Volume, V_CARGO [m³] | 11 | [2] | ||||||||
| Cargo Capacity | - | ||||||||||
| Max. Pallet Underfloor | - | ||||||||||
| Seats | Max. Seats, n_M,SEAT | 37 | [4] | ||||||||
| Std. Layout, n_SEAT | 34 | [3] | |||||||||