Antonov An-124

The Antonov An-124 is a four-engined heavy cargo freighter with a payload of 150 tonnes (330700 lb) developed by the soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine). It was developed as a military strategic heavy airlift transport aircraft.

Crew	6
Propulsion	4 Turbofan Engines
Engine Model	Lotarew / Lotarev D-18T
Engine Power (each)	230 kN	51706 lbf
Speed	909 km/h	491 kts 565 mph
Mmo (max. Mach)	Mach 0.77
Service Ceiling	12.000 m	39.370 ft
Range	5.400 km	2.916 NM 3.356 mi.
Empty Weight	175.000 kg	385.809lbs
max. Takeoff Weight	405.000 kg	892.872lbs
Wing Span	73,30 m	240,5 ft
Wing Area	628,0 m²	6760 ft²
Length	69,10 m	226,7 ft
Height	20,78 m	68,2 ft
First Flight	26.12.1982
Production Status	in production
ICAO Code	A124
IATA Code	A4F
NATO Code	Condor
Data for (Version)	Antonov / Antonow An-124
Variants	An-124, An-124-100, An-124-100M-150, An-124-102, An-124-135, An-124-150

RemarksThe An-124 is equipped with nose and tail cargo doors. The shoulder-wing configuration in conjunction with the 24-wheel landing gear allows operations from semi prepared landing strips. The aircraft has the ability to kneel down for easier front loading.