A/C	Manufacturer	Airbus		Airbus		Airbus		Airbus		Airbus		Airbus		Airbus			Sources:
	Aircraft type	A220-300		A319ceo		A319neo		A320ceo		A320neo		A321ceo		A321neo		[1]	https://www.flightglobal.com/download?ac=73559
	Total number of operating A/C	72	[1]	1243	[1]	0	[1]	4132	[1]	1009	[1]	1591	[1]	355	[1]	[2]	https://www.airbus.com/sites/g/files/jlcbta136/files/2022-02/Airbus-techdata-AC_A319_0322.pdf
	Option/Variant	-		-		-		-		-		-		-		[3]	https://www.easa.europa.eu/downloads/16507/en
Engine	No. of Engines	2	[13]	2	[3]	2	[3]	2	[3]	2	[3]	2	[3]	2	[3]	[4]	https://aircraft.airbus.com/en/aircraft/a320/a319ceo
	Model	PW1521G	[13]	CFM56-5A5	[3]	LEAP-1A26	[3]	CFM56-5B4	[3]	LEAP-1A29	[3]	CFM56-5B1	[3]	LEAP-1A32	[3]	[5]	https://www.acj.airbus.com/en/exclusive-aircraft/acjneo
	Max. Rated Takeoff Thrust, T_TO [kN]	97,73	[14]	104,53	[3]	120,64	[3]	120,1	[3]	130,29	[3]	133,44	[3]	143,05	[3]	[6]	https://www.airbus.com/sites/g/files/jlcbta136/files/2022-02/Airbus-techdata-AC_A320_0322.pdf
	Equivalent Power, P [kW]	-		-		-		-		-		-		-		[7]	https://aircraft.airbus.com/en/aircraft/a320/a320ceo
	Propeller	-		-		-		-		-		-		-		[8]	https://aircraft.airbus.com/en/aircraft/a320/a321ceo
Cabin	Length, l_CABIN [m]	27,5	[11]	23,78	[4]	23,78	[4]	27,51	[7]	27,51	[7]	34,44	[9]	34,44	[9]	[9]	https://aircraft.airbus.com/en/aircraft/a320/a321neo
	Max. Height, h_CABIN [m]	2,13	[12]	2,25	[5]	2,25	[5]	2,25	[5]	2,25	[5]	2,25	[5]	2,25	[5]	[10]	https://www.airbus.com/sites/g/files/jlcbta136/files/2022-02/Airbus-techdata-AC_A321_0322.pdf
	Max. Width, d_F,I [m]	3,28	[12]	3,7	[4]	3,7	[4]	3,7	[7]	3,7	[7]	3,7	[4]	3,7	[4]	[11]	https://aircraft.airbus.com/en/aircraft/a220/a220-300
	Passenger Compartment Volume, V_CABIN [m³]	N/A		120	[2]	120	[2]	139	[6]	139	[6]	155	[10]	155	[10]	[12]	https://eservices.aero.bombardier.com/wps/wcm/connect/eServices/e541c413-b25a-4d2c-8855-9fbfdc069f76/A220-300APP-Issue028-00-14apr2022.pdf?MOD=AJPERES&CVID=o0EtI6o&CVID=nEpwCZe&CVID=nEpwCZe&CVID=nDRB7Pn&CVID=nDRB7Pn&CVID=ndnIvYh&CVID=n8iXu7i&CVID=n8iXu7i&CVID=n8iXu7i&CVID=mVHwufA&CVID=mVHwufA
Fuselage	Height, h_F [m]	3,72	[12]	4,14	[2]	4,14	[2]	4,14	[6]	4,14	[6]	4,14	[10]	4,14	[10]	[13]	https://www.easa.europa.eu/downloads/20964/en
	Width, w_F [m]	3,51	[12]	3,95	[2]	3,95	[2]	3,95	[6]	3,95	[6]	3,95	[9]	3,95	[9]	[14]	https://www.easa.europa.eu/downloads/20863/en
Total	Length, l_A/C [m]	38,7	[11]	33,84	[2]	33,84	[2]	35,57	[6]	35,57	[6]	44,51	[3]	44,51	[3]		Comments:
	Span, b_W [m]	35,1	[11]	35,8	⁶[6]	35,8	[2]	35,8	⁶[6]	35,8	[6]	35,8	⁶[10]	35,8	[10]		¹ ISA conditions
	Height, h_A/C [m]	11,5	[11]	11,76	[3]	11,76	[3]	11,76	[7]	11,76	[7]	11,76	[3]	11,76	[3]		² ISA conditions, with ACT, no winglets
Landing Gear	Track, l_T [m]	6,73	[12]	7,59	[2]	7,59	[2]	7,59	[6]	7,59	[6]	7,59	[3]	7,59	[3]		³ ISA conditions, with ACT
	Wheelbase, l_WB [m]	15,31	[12]	11,04	[2]	11,04	[2]	12,64	[6]	12,64	[6]	16,91	[9]	16,91	[9]		⁴ ISA conditions, with 2 ACT, no winglets
Wing	Area, S_W [m²]	112,3	[12]	N/A	[2]	N/A	[2]	N/A		N/A		N/A		N/A			⁵ ISA conditions, with 2 ACT
	Taper ratio, λ_W	0,26	[12]	0,25	[2]	0,27	[2]	0,25	[6]	0,27	[6]	0,25	[10]	0,27	[10]		⁶ without wingtip: 34,1
	1/4 Chord Sweep, φ_25,W [°]	26	[12]	23,5	[2]	23,5	[2]	23,5	[6]	23,5	[6]	23,5	[10]	23,5	[10]
Vertical Tail	Area, S_V [m²]	28,2	[12]	N/A		N/A		N/A		N/A		N/A		N/A
	Height, b_V [m]	6	[12]	5,87	[2]	5,87	[2]	5,87	[6]	5,87	[6]	5,87	[10]	5,87	[10]
	Taper ratio, λ_V	0,35	[12]	0,33	[2]	0,33	[2]	0,33	[6]	0,33	[6]	0,33	[10]	0,33	[10]
	1/4 Chord Sweep, φ_25,V [°]	35,5	[12]	35	[2]	35	[2]	35	[6]	35	[6]	35	[10]	35	[10]
Horizontal Tail	Area, S_H [m²]	36,6	[12]	N/A		N/A		N/A		N/A		N/A		N/A
	Span, b_H [m]	12,26	[12]	12,45	[2]	12,45	[2]	12,45	[6]	12,45	[6]	12,45	[10]	12,45	[10]
	Taper Ratio, λ_H	0,375	[12]	0,375	[2]	0,375	[2]	0,375	[6]	0,375	[6]	0,375	[10]	0,375	[10]
	1/4 Chord Sweep, φ_25,H [°]	30,5	[12]	28	[2]	28	[2]	28	[6]	23,5	[6]	23,5	[10]	23,5	[10]
Cruise	V_MO [kt]	489	[13]	488	[3]	488	[3]	488	[3]	488	[3]	488	[3]	488	[3]
	M_MO [Mach]	0,82	[11]	0,82	[3]	0,82	[3]	0,82	[3]	0,82	[3]	0,82	[3]	0,82	[3]
	Cruise Speed, M_CR [Mach]	N/A		N/A		N/A		N/A		N/A		N/A		N/A
	Max. Certified Flight Level, h_MCR [FL]	410	[13]	410	[3]	410	[3]	410	[3]	410	[3]	410	[3]	410	[3]
	Cruise Altitude, h_CR [FL]	N/A		N/A		N/A		N/A		N/A		N/A		N/A
Fuel	Unusable Fuel [l]	125	[11]	82	[2]	82	[2]	82	[3]	82	[3]	46	[3]	46	[3]
	Optional Fuel [l]	-		8250	[2]	8248	[2]	8250	[3]	8250	[3]	8200	[3]	8200	[3]
	Max usable fuel [l]	21381	[11]	15609	[2]	15477	[2]	15609	[3]	15609	[3]	15500	[3]	15380	[3]
Range	Max. Payload, R_MPL [nm]	2000	¹[12]	2500	²[2]	2700	³[2]	2100	²[6]	2450	³[6]	2300	⁴[10]	3050	⁵[10]
	Max. Pax, R_M,pax [nm]	3100	¹[12]	3000	²[2]	3500	³[2]	2850	²[6]	3150	³[6]	2950	⁴[10]	3600	⁵[10]
	Max. Range, R_PLMR [nm]	3350	¹[12]	3950	²[2]	4300	³[2]	3300	²[6]	4000	³[6]	2900	⁴[10]	3500	⁵[10]
Mass	Max. Ramp, m_MR (MRM) [kg]	71300	[13]	75900	[3]	75900	[3]	78400	[6]	79400	[6]	93900	[9]	97400	[9]
	Max. Take-Off, m_MTO (MTOM) [kg]	70900	[13]	75500	[3]	75500	[3]	78000	[6]	79000	[6]	93500	[9]	97000	[9]
	Max. Landing, m_ML (MLM) [kg]	58800	[13]	62500	[3]	63900	[3]	66000	[6]	67400	[6]	77800	[9]	79200	[9]
	Max. Zero Fuel, m_MZF (MZFM) [kg]	55800	[13]	58500	[3]	60300	[3]	62500	[6]	64300	[6]	73800	[9]	75600	[9]
	Operating Empty, m_OE (OEM) (MZFM-MPL) [kg]	43500	[12]	35400	[3]	39600	[3]	43500	[6]	45800	[6]	47500	[9]	46600	[9]
	Max. Payload, m_MPL (MPL) [kg]	12300	[12]	23100	[2]	20700	[2]	19000	[6]	18500	[6]	26300	[9]	29000	[9]
	Payload at Max. Range, m_PLMR [kg]	6350	[12]	9800	[2]	11000	[2]	13000	[6]	12000	[6]	20000	[9]	22000	[9]
Cargo	Volume, V_CARGO [m³]	27,46	[12]	27,66	[2]	27,66	[2]	37,42	[6]	37,42	[6]	51,72	[10]	51,72	[10]
	Cargo Capacity	-		4 ULD	[2]	4 ULD	[2]	7 LD3-45W	[6]	7 LD3-45W	[6]	10 LD-3-45W	[9]	10 LD-3-45W	[9]
	Max. Pallet Underfloor	-		-		-		7	[6]	7	[6]	10	[9]	10	[9]
Seats	Max. Seats, n_M,SEAT	149	[13]	160	[2]	160	[2]	180	[7]	194	[7]	220	[9]	244	[9]
	Std. Layout, n_SEAT	140	[12]	156	[2]	156	[2]	170	[7]	180	[7]	210	[9]	220	[9]