Mil Mi-24

General Data
First Flown:	1970	Length:	57 ft 5.5 in
Lift Capability:	n/a	Height:	13 ft
Range:	540 nm	Rotor Span:	56 ft 9 in
Top Speed:	208 mph	Empty Weight:	18,078 lb
Service Ceiling:	unknown	Max Gross Weight:	at take off 26,455 lb
Engines:	2 Kilmov TV3-117 series II turboshafts rated at 4,380 shp
Armament:	12.7 or dual 23 mm nose cannon, wire guided anti-tank missils, radio and laser guided anti-tank missiles, air to air missiles, free flight rocket pods,23 or 12.7 mm cannon pods, dual 30 mm cannon, 30 mm grenade launcher, bombs, mine dispensers
Accommodations:	1 Pilot, weapons operator, flight engineer, 8 troops	Cargo:	unknown
Operators:	Afghanistan, Algeria, Angola, Armenia, Azerbaijan, Belars, Bulgaria, Cambodia, Croatia, Czech Republic, Executive Outcomes, Ethiopia, Finland, Hungary, India, Iraq, Kazakhstan, Laos, Libya, Mongolia, Mozambique, Peru, Poland, Russia, Rwanda, Sierra Leone, Sierra Leone, Slovakia, Sri Lanka, Sudan, Syria, Tajikistan, Uzbekistan, Ukraine, Vietnam, Yemen, Georgia, USA

Similar Aircraft:
Other Features:	NATO reporting name is Hind


Notes

Jeff's Helicopter Philes