| A/C | Manufacturer | ATR | ATR | Sources: | ||||||
| Aircraft type | ATR 42 | ATR 72 | [1] | https://www.flightglobal.com/download?ac=73559 | ||||||
| Total number of operating A/C | 208 | [1] | 795 | [1] | [2] | https://perma.cc/UQ5K-LGE4 | ||||
| Option/Variant | 42-500/-600 | [5] | 72-212A/-600 | [4] | [3] | https://www.atr-aircraft.com/wp-content/uploads/2020/07/Factsheets_-_ATR_42-600.pdf | ||||
| Engine | No. of Engines | 2 | [3] | 2 | [4] | [4] | https://www.atr-aircraft.com/wp-content/uploads/2020/07/Factsheets_-_ATR_72-600.pdf | |||
| Model | PW127M | [3] | PW127M/N | [4] | [5] | https://www.easa.europa.eu/downloads/8249/en | ||||
| Max. Rated Takeoff Thrust, T_TO [kN] | - | - | [6] | https://perma.cc/J8MY-KVDC | ||||||
| Equivalent Power, P [kW] | 1589 | [3] | 1820 | [4] | Comments: | |||||
| Propeller | 568F | [3] | 568F | [4] | ¹ No further details | |||||
| Cabin | Length, l_CABIN [m] | N/A | N/A | |||||||
| Max. Height, h_CABIN [m] | 1,91 | [3] | 1,91 | [4] | ||||||
| Max. Width, d_F,I [m] | 2,57 | [3] | 2,57 | [4] | ||||||
| Passenger Compartment Volume, V_CABIN [m³] | N/A | N/A | ||||||||
| Fuselage | Height, h_F [m] | 2,63 | [6] | 2,63 | [2] | |||||
| Width, w_F [m] | 2,87 | [6] | 2,87 | [2] | ||||||
| Total | Length, l_A/C [m] | 22,67 | [3] | 27,17 | [4] | |||||
| Span, b_W [m] | 24,57 | [3] | 27,05 | [4] | ||||||
| Height, h_A/C [m] | 7,59 | [3] | 7,65 | [4] | ||||||
| Landing Gear | Track, l_T [m] | 4,1 | [3] | 4,1 | [4] | |||||
| Wheelbase, l_WB [m] | 8,78 | [3] | 10,77 | [4] | ||||||
| Wing | Area, S_W [m²] | 54,5 | [3] | 61 | [4] | |||||
| Taper ratio, λ_W | N/A | 0,47 | [2] | |||||||
| 1/4 Chord Sweep, φ_25,W [°] | N/A | 3,5 | [2] | |||||||
| Vertical Tail | Area, S_V [m²] | 12,48 | [6] | N/A | ||||||
| Height, b_V [m] | 4,53 | [6] | 4,43 | [2] | ||||||
| Taper ratio, λ_V | N/A | 0,65 | [2] | |||||||
| 1/4 Chord Sweep, φ_25,V [°] | N/A | 29 | [2] | |||||||
| Horizontal Tail | Area, S_H [m²] | 11,73 | [6] | N/A | ||||||
| Span, b_H [m] | 7,31 | [6] | 7,31 | [2] | ||||||
| Taper Ratio, λ_H | N/A | 0,525 | [2] | |||||||
| 1/4 Chord Sweep, φ_25,H [°] | N/A | 5,5 | [2] | |||||||
| Cruise | V_MO [kt] | 300 | [6] | 275 | [4] | |||||
| M_MO [Mach] | 0,55 | [6] | 0,55 | [2] | ||||||
| Cruise Speed, M_CR [Mach] | N/A | N/A | ||||||||
| Max. Certified Flight Level, h_MCR [FL] | 250 | [6] | 250 | [2] | ||||||
| Cruise Altitude, h_CR [FL] | N/A | N/A | ||||||||
| Fuel | Unusable Fuel [l] | 26 | [5] | 37 | [5] | |||||
| Optional Fuel [l] | - | - | ||||||||
| Max usable fuel [l] | 5700 | [5] | 6360 | [5] | ||||||
| Range | Max. Payload, R_MPL [nm] | N/A | N/A | |||||||
| Max. Pax, R_M,pax [nm] | 703 | ¹[3] | 758 | ¹[4] | ||||||
| Max. Range, R_PLMR [nm] | N/A | N/A | ||||||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | 18770 | [5] | 23170 | [5] | |||||
| Max. Take-Off, m_MTO (MTOM) [kg] | 18600 | [3] | 23000 | [4] | ||||||
| Max. Landing, m_ML (MLM) [kg] | 18300 | [3] | 22350 | [4] | ||||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | 17000 | [3] | 21000 | [4] | ||||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | 11550 | [3] | 13010 | [4] | ||||||
| Max. Payload, m_MPL (MPL) [kg] | 5300 | [3] | 7550 | [4] | ||||||
| Payload at Max. Range, m_PLMR [kg] | N/A | N/A | ||||||||
| Cargo | Volume, V_CARGO [m³] | N/A | N/A | |||||||
| Cargo Capacity | - | - | ||||||||
| Max. Pallet Underfloor | - | - | ||||||||
| Seats | Max. Seats, n_M,SEAT | 60 | [5] | 74 | [5] | |||||
| Std. Layout, n_SEAT | 48 | [5] | 72 | [4] | ||||||