| A/C | Manufacturer | Airbus | Airbus | Airbus | Airbus | Airbus | Airbus | Sources: | |||||||||||||
| Aircraft type | A330-200 | A330-300 | A330-900 | A350-900 | A350-1000 | A380 | [1] | https://www.flightglobal.com/download?ac=73559 | |||||||||||||
| Total number of operating A/C | 502 | [1] | 707 | [1] | 47 | [1] | 321 | [1] | 43 | [1] | 237 | [1] | [2] | https://www.airbus.com/sites/g/files/jlcbta136/files/2021-11/Airbus-Commercial-Aircraft-AC-A330.pdf | |||||||
| Option/Variant | A330-203 | [5] | A330-303 | [5] | A330-941 | [5] | A350-941 | [7] | A350-1041 | [7] | A380-800 | [10] | [3] | https://aircraft.airbus.com/en/aircraft/a330/a330-200 | |||||||
| Engine | No. of Engines | 2 | [2] | 2 | [2] | 2 | [2] | 2 | [7] | 2 | [7] | 4 | [10] | [4] | https://aircraft.airbus.com/en/aircraft/a330/a330-300 | ||||||
| Model | CF6-80E1A3 | [5] | CF6-80E1A3 | [5] | 7000-72 | [5] | XWB-84 | [8] | XWB-97 | [8] | 970B-84 | [12] | [5] | https://www.easa.europa.eu/downloads/22146/en | |||||||
| Max. Rated Takeoff Thrust, T_TO [kN] | 304,84 | [5] | 304,84 | [5] | 323,98 | [5] | 374,5 | [17] | 431,5 | [17] | 348,31 | [12] | [6] | https://aircraft.airbus.com/en/aircraft/a350/a350-900 | |||||||
| Equivalent Power, P [kW] | - | - | - | - | - | - | [7] | https://www.airbus.com/sites/g/files/jlcbta136/files/2021-11/Airbus-Commercial-Aircraft-AC-A350-900-1000.pdf | |||||||||||||
| Propeller | - | - | - | - | - | - | [8] | https://www.easa.europa.eu/downloads/17736/en | |||||||||||||
| Cabin | Length, l_CABIN [m] | 45 | [3] | 50,36 | [4] | 50,36 | [16] | 51,04 | [6] | 58,03 | [9] | 49,9 | [11] | [9] | https://aircraft.airbus.com/en/aircraft/a350/a350-1000 | ||||||
| Max. Height, h_CABIN [m] | 2,4 | [2] | 2,4 | [2] | 2,4 | [2] | 2,49 | [7] | 2,49 | [7] | 2,44 | [10] | [10] | https://www.airbus.com/sites/g/files/jlcbta136/files/2021-11/Airbus-Aircraft-AC-A380.pdf | |||||||
| Max. Width, d_F,I [m] | 5,26 | [3] | 5,26 | [4] | 5,26 | [16] | 5,61 | [6] | 5,61 | [9] | 6,5 | [11] | [11] | https://www.airbus.com/sites/g/files/jlcbta136/files/2021-12/EN-Airbus-A380-Facts-and-Figures-December-2021_0.pdf | |||||||
| Passenger Compartment Volume, V_CABIN [m³] | 335 | [2] | 372 | [2] | 372 | [2] | 473,7 | [7] | N/A | 1305 | [10] | [12] | https://www.easa.europa.eu/downloads/8223/en | ||||||||
| Fuselage | Height, h_F [m] | 5,64 | [2] | 5,64 | [2] | 5,64 | [16] | 6,09 | [7] | 6,09 | [7] | 8,41 | [10] | [13] | https://www.fzt.haw-hamburg.de/pers/Scholz/dglr/hh/text_2008_01_31_A380.pdf | ||||||
| Width, w_F [m] | 5,64 | [3] | 5,64 | [4] | 5,64 | [16] | 5,96 | [6] | 5,96 | [9] | 7,14 | [10] | [14] | https://en.wikipedia.org/wiki/Airbus_A380 | |||||||
| Total | Length, l_A/C [m] | 58,82 | [3] | 63,66 | [4] | 63,66 | [16] | 66,8 | [6] | 73,79 | [9] | 72,73 | [10] | [15] | https://modernairliners.com/airbus-a380/airbus-a380-specs/ | ||||||
| Span, b_W [m] | 60,3 | [3] | 60,3 | [4] | 64 | [16] | 64,75 | [6] | 64,75 | [9] | 79,75 | [10] | [16] | https://aircraft.airbus.com/en/aircraft/a330/a330-900 | |||||||
| Height, h_A/C [m] | 17,39 | [3] | 16,79 | [4] | 16,79 | [16] | 17,05 | [6] | 17,08 | [9] | 24,1 | [11] | [17] | https://www.easa.europa.eu/downloads/7635/en | |||||||
| Landing Gear | Track, l_T [m] | 10,68 | [3] | 10,68 | [4] | 10,68 | [16] | 10,6 | [7] | 10,73 | [7] | 5,26 | [10] | Comments: | |||||||
| Wheelbase, l_WB [m] | 22,18 | [3] | 25,38 | [4] | 25,38 | [16] | 28,66 | [7] | 32,48 | [7] | 36,85 | [10] | ¹ ISA conditions | ||||||||
| Wing | Area, S_W [m²] | N/A | N/A | N/A | N/A | N/A | 845 | [11] | ² ISA conditions, with ACT | ||||||||||||
| Taper ratio, λ_W | 0,24 | [2] | 0,24 | [2] | 0,17 | [2] | 0,16 | [7] | 0,16 | [7] | 0,23 | [10] | ³ ISA conditions, typical international flight profile, no wind, 5% trip fuel allowance, 30 min holding, 200 nm diversion | ||||||||
| 1/4 Chord Sweep, φ_25,W [°] | 28,50 | [2] | 28,50 | [2] | 29,00 | [2] | 32,00 | [7] | 32,00 | [7] | 33,50 | [11] | ⁴ pre MOD: 9,3 | ||||||||
| Vertical Tail | Area, S_V [m²] | N/A | N/A | N/A | N/A | N/A | 122 | [13] | ⁵ pre MOD: 0,33 | ||||||||||||
| Height, b_V [m] | 8,8 | ⁴[2] | 8,3 | [2] | 8,3 | [2] | 9,42 | [7] | 9,42 | [7] | 14,59 | [10] | ⁶ front fuselage gear: 12,46 | ||||||||
| Taper ratio, λ_V | 0,36 | ⁵[2] | 0,4 | [2] | 0,4 | [2] | 0,39 | [7] | 0,39 | [7] | 0,39 | [10] | ⁷ front fuselage gear: 33,58 | ||||||||
| 1/4 Chord Sweep, φ_25,V [°] | 39 | [2] | 39 | [2] | 43,5 | [2] | 40 | [7] | 40 | [7] | 40 | [10] | |||||||||
| Horizontal Tail | Area, S_H [m²] | N/A | N/A | N/A | N/A | N/A | 205 | [13] | |||||||||||||
| Span, b_H [m] | 19,4 | [2] | 19,4 | [2] | 19,4 | [2] | 18,79 | [7] | 18,79 | [7] | 30,37 | [10] | |||||||||
| Taper Ratio, λ_H | 0,4 | [2] | 0,425 | [2] | 0,4 | [2] | 0,395 | [7] | 0,395 | [7] | 0,38 | [10] | |||||||||
| 1/4 Chord Sweep, φ_25,H [°] | 29 | [2] | 29,5 | [2] | 29 | [2] | 33,5 | [7] | 33,5 | [7] | 33,5 | [10] | |||||||||
| Cruise | V_MO [kt] | 573 | [3] | 573 | [4] | 573 | [16] | 593 | [6] | 593 | [9] | 593 | [15] | ||||||||
| M_MO [Mach] | 0,86 | [3] | 0,86 | [4] | 0,86 | [16] | 0,89 | [6] | 0,89 | [9] | 0,89 | [15] | |||||||||
| Cruise Speed, M_CR [Mach] | N/A | N/A | N/A | N/A | N/A | 0,85 | [11] | ||||||||||||||
| Max. Certified Flight Level, h_MCR [FL] | 414,5 | [5] | 414,5 | [5] | 414,5 | [5] | 431 | [8] | 414,5 | [8] | 430 | [15] | |||||||||
| Cruise Altitude, h_CR [FL] | N/A | N/A | N/A | N/A | N/A | N/A | |||||||||||||||
| Fuel | Unusable Fuel [l] | 279 | [5] | 279 | [5] | 279 | [5] | N/A | N/A | 1086 | [12] | ||||||||||
| Optional Fuel [l] | 41560 | [5] | 41560 | [5] | - | 25693 | [8] | - | - | ||||||||||||
| Max usable fuel [l] | 139090 | [3] | 139090 | [4] | 139090 | [2] | 140795 | [8] | 158791 | [8] | 324339 | [12] | |||||||||
| Range | Max. Payload, R_MPL [nm] | 4700 | ¹[2] | 4200 | ²[2] | 4800 | ¹[2] | 5800 | ¹[7] | 5600 | ¹[7] | 6600 | ³[10] | ||||||||
| Max. Pax, R_M,pax [nm] | 7200 | ¹[2] | 6150 | ²[2] | 6850 | ¹[2] | 8000 | ¹[7] | 8300 | ¹[7] | 8000 | ³[10] | |||||||||
| Max. Range, R_PLMR [nm] | 5300 | ¹[2] | 4800 | ²[2] | 5500 | ¹[2] | 8600 | ¹[7] | 8500 | ¹[7] | 8800 | ³[10] | |||||||||
| Mass | Max. Ramp, m_MR (MRM) [kg] | 242900 | [3] | 242900 | [4] | 251900 | [2] | 280900 | [6] | 319900 | [9] | 577000 | [10] | ||||||||
| Max. Take-Off, m_MTO (MTOM) [kg] | 242000 | [3] | 242000 | [4] | 251000 | [2] | 280000 | [6] | 319000 | [9] | 575000 | [10] | |||||||||
| Max. Landing, m_ML (MLM) [kg] | 182000 | [3] | 187000 | [4] | 191000 | [2] | 207000 | [6] | 236000 | [9] | 394000 | [10] | |||||||||
| Max. Zero Fuel, m_MZF (MZFM) [kg] | 170000 | [3] | 175000 | [4] | 181000 | [2] | 1957000 | [6] | 223000 | [9] | 369000 | [10] | |||||||||
| Operating Empty, m_OE (OEM) (MZFM-MPL) [kg] | 124000 | [2] | 129000 | [2] | 135000 | [2] | 1903000 | [7] | 156000 | [7] | 285000 | [10] | |||||||||
| Max. Payload, m_MPL (MPL) [kg] | 46000 | [2] | 46000 | [2] | 46000 | [2] | 54000 | [7] | 67000 | [7] | 84000 | [10] | |||||||||
| Payload at Max. Range, m_PLMR [kg] | 42000 | [2] | 42000 | [2] | 42000 | [2] | 25000 | [7] | 33000 | [7] | 35000 | [10] | |||||||||
| Cargo | Volume, V_CARGO [m³] | 132,4 | [2] | 158,4 | [2] | 158,4 | [2] | 170,22 | [7] | 206,02 | [7] | 175,2 | [10] | ||||||||
| Cargo Capacity | 27 LD-3 | [3] | 33 LD-3 | [2] | 33 LD-3 | [2] | 36 LD-3 | [6] | 44 LD-3 | [9] | 38 LD3 | [10] | |||||||||
| Max. Pallet Underfloor | 8 | [3] | 11 | [2] | 11 | [2] | 11 | [6] | 14 | [9] | 13 | [10] | |||||||||
| Seats | Max. Seats, n_M,SEAT | 406 | [3] | 440 | [4] | 440 | [5] | 440 | [6] | 480 | [9] | 868 | [12] | ||||||||
| Std. Layout, n_SEAT | 247 | [2] | 300 | [2] | 310 | [2] | 325 | [7] | 366 | [7] | 573 | [11] | |||||||||