Antonov An-30

The Antonov An-30 is a twin-engined photographic / survey aircraft by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).

Crew	5-7
Propulsion	2 Turboprop Engines
Engine Model	Iwtschenko / Ivchenko AI-24WT / AI-24VT
Engine Power (each)	2075 kW	2783 shp
Speed	541 km/h	292 kts <I>  336 mph</I>
Service Ceiling	8.400 m	27.559 ft
Range	2.600 km	1.404 NM <I>1.616 mi.</I>
Empty Weight	15.990 kg	35.252 lbs
max. Takeoff Weight	23.000 kg	50.706 lbs
Wing Span	29,20 m	95,8 ft
Wing Area	75,0 m²	807 ft²
Length	24,26 m	79,6 ft
Height	8,32 m	27,3 ft
First Flight	21.08.1967
Production Status	out of production
Total Production	123
Developed from	An-24
NATO Code	CLANK
Data for (Version)	Antonov / Antonow An-30A
Variants	An-24FK, An-30A, An-30B, An-30D

Remarks
The An-30 is a development of the Antonov An-24. The An-30 is equipped with an additional turbojet engine Tumanski RU-19A-30 with 8,8 kN (1978 lbf) thrust.