L-410UVP/UVP-E, 1979/1985
			A reliable, economical and versatile aircraft boasting a full IFR and de-icing equipment. L-410 is in service world-wide thanks to its low cost operation and maintenance, excellent hot and high capabilities, a large passenger/cargo cabin. The sturdy landing gear and the low pressure tyres enable the L-410 to operate efficiently even on most hazardous surfaces. Of particular interest are its climbing speed and power-to-weight ratio making the L-410UVP-E an aircraft of choice for parachuting centers, especially for high altitude (from 4000 m) sky-diving. UVP is a STOL version and UVP-E its re-motorized update, mostly sought for.
						Propellers: Two 3-/5- blade AVIA Hamilton V508/V510 propellers equipped with a feathering system and electric de-icing.
	Engines: Two free M-601D (UVP) or E (UVP-E) twin-shaft turboprops, maximum power 730/751 hp (544/560kW) each. Dimensions: Span Length Height Wings area Passenger cabine volume Luggage compartment volume 19,98 m 14,42 m 5,83 m 35,18 m2 17,9 m3 1,37 m3 65,51 ft 42,28 ft 19,11 ft 378,2 ft2 630,9 ft3 48,3 ft3 Weights: Maximum takeoff weight Maximum landing weight: Empty weight Total fuel capacity 6400 kg 6200 kg 3985 kg 1300 kg 14112 lb 13671 lb 8787 lb 2866,5 lb Performances: 216 kt 205 kt 1416 fpm 354 fpm 20721 ft 1134 nm 378 nm 617 lb/h 2246 ft 1574 ft 20 min Maximum speed Maximum cruise speed @ 4200 m Maximum rate of climb, 2 engines Maximum rate of climb, 1 engine Service ceiling Maximum range with tip tanks Maximum payload range Fuel consumption Take off run to 11 m (sea level) Landing run from 9 m (sea level) Rotation to 4000m / 33000ft, 19 pax 400 km/h 380 km/h 7,2 m/s 1,8 m/s 6320 m 2100 km 700 km 280 kg/h 685 m 480 m 20 min