A/C |
Manufacturer |
Airbus |
|
Airbus |
|
Airbus |
|
Airbus |
|
Airbus |
|
Airbus |
|
|
Sources: |
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|
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] |
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