A/C	Manufacturer	Antonov			Sources:
	Aircraft type	AN-24		[1]	https://www.flightglobal.com/download?ac=73559
	Total number of operating A/C	97	[1]	[2]	https://www.antonov.com/en/history/an-24
	Option/Variant	RV	[3]	[3]	https://urga.com.ua/en/samolet-an-24.html
Engine	No. of Engines	2	[3]	[4]	http://aviaros.narod.ru/an-24.htm
	Model	AI-24	[3]	[5]	TAYLOR, John W.R., 1974. Jane's All The World's Aircraft 1974–75. New York, USA.
	Max. Rated Takeoff Thrust, T_TO [kN]	-			Comments:
	Equivalent Power, P [kW]	1875	[3]		¹ No further details
	Propeller	AV-72	[3]
Cabin	Length, l_CABIN [m]	9,69	[5]
	Max. Height, h_CABIN [m]	1,91	[5]
	Max. Width, d_F,I [m]	2,76	[5]
	Passenger Compartment Volume, V_CABIN [m³]	N/A
Fuselage	Height, h_F [m]	2,5	[5]
	Width, w_F [m]	2,9	[5]
Total	Length, l_A/C [m]	23,53	[2]
	Span, b_W [m]	29,2	[2]
	Height, h_A/C [m]	8,32	[2]
Landing Gear	Track, l_T [m]	7,9	[5]
	Wheelbase, l_WB [m]	7,89	[5]
Wing	Area, S_W [m²]	74,98	[5]
	Taper ratio, λ_W	0,34	[2]
	1/4 Chord Sweep, φ_25,W [°]	4,50	[2]
Vertical Tail	Area, S_V [m²]	N/A
	Height, b_V [m]	4,93	[2]
	Taper ratio, λ_V	0,445	[2]
	1/4 Chord Sweep, φ_25,V [°]	20	[2]
Horizontal Tail	Area, S_H [m²]	N/A
	Span, b_H [m]	9,08	[5]
	Taper Ratio, λ_H	0,405	[2]
	1/4 Chord Sweep, φ_25,H [°]	17	[2]
Cruise	V_MO [kt]	291	[4]
	M_MO [Mach]	N/A
	Cruise Speed, M_CR [Mach]	0,35	[4]
	Max. Certified Flight Level, h_MCR [FL]	295	[4]
	Cruise Altitude, h_CR [FL]	N/A
Fuel	Unusable Fuel [l]	N/A
	Optional Fuel [l]	-
	Max usable fuel [l]	4940	[4]
Range	Max. Payload, R_MPL [nm]	530	¹[4]
	Max. Pax, R_M,pax [nm]	N/A
	Max. Range, R_PLMR [nm]	1080	¹[4]
Mass	Max. Ramp, m_MR (MRM) [kg]	N/A
	Max. Take-Off, m_MTO (MTOM) [kg]	21800	[4]
	Max. Landing, m_ML (MLM) [kg]	N/A
	Max. Zero Fuel, m_MZF (MZFM) [kg]	20300	[4]
	Operating Empty, m_OE (OEM) (MZFM-MPL) [kg]	14800	[3]
	Max. Payload, m_MPL (MPL) [kg]	5500	[4]
	Payload at Max. Range, m_PLMR [kg]	N/A
Cargo	Volume, V_CARGO [m³]	N/A
	Cargo Capacity	-
	Max. Pallet Underfloor	-
Seats	Max. Seats, n_M,SEAT	52	[4]
	Std. Layout, n_SEAT	48	[3]