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english [/] deutsch russian home page e-mail to us site map OUR PLANES Yak-52 Yak-52 is a twin-seated primary training and aerobatics sports monoplane with low positioned wings and retractable undercarriage. The plane is equipped with M-14P powerplant ( 360 hp output) with В530ТА-D35 airscrew. The plane is manufactured for primary training of pilots. Technical specifications of the plane ensure mastering of elementary, intermediate and higher aerobatics by the pilots. The plane has two cockpits: the front cockpit to seat the pilot, the rear one- for the instructor. If necessary, the plane is controlled by a pilot from the front cockpit. Length 7.7 m Wingspan 9.3 m Plane 15 m ² Empty weight 1035 kg Max T/O 1315 kg Max horizontal speed 270 km/h Range 465 km Take-off run 180 — 200 m Path length 330 m. Stalling speed 120 km/h Max permissible speed 450 km/h Max permissible maintenance overloads: Positive 7 Negative 5 L – 410UVP Let Passenger plane for domestic airlines. Development started in 1966. the first sample plane was equipped with РТ6А-27 Pratt-Witney (Canada) (2 х 715 hp.) turboprop engines . Flight tests started April 16, 1969. In late 1971 the first L-41 OA production plane came into operation with “Slov-Air” Czech Airline. Total 31 planes were manufactured. In 1973 flight tests of L-410M plane began. The plane was equipped with Valter М 601А turboprop engines (Czech). The plane came into operation in 1976. Total 100 pieces of L-410M were built by “Let” Company. In 1979 г. The updated modification L-410UVP was produced. The model became the basic serial product (till the end of 1985 year total 512 planes were built). This plane was different from its predecessors: it has a longer hull, larger wingspans and vertical tail units. Also, the interceptors were installed here. The plane is equipped with Walter М 601 В (2 х 730 hp) turboprop engines. The aircraft was certified in the USSR and put into operation by AEROFLOT. In fact, it was the first foreign aircraft entered the national airlines. Further, a newer update of the plane, L-41 OUVP-E was equipped with more powerful М 601 Е turboprops. The first flight was on December 30,1984. The plane has better takeoff and landing characteristics and lower cockpit noise level. Flying tests commenced in November 1993. Equipment Standard avionics equipment of Soviet and Czech manufacture. Powerplants Walter М 601 Е (2х750 hp) turboprops. Five-bladed airscrews with diameter 2.3m Condition L-410 –type planes have been produced on mass scale since 1970. Dimensions 9.197 м Wingspan (m) 19,48/19,98 Length (m) 14,42 Height (m) 5,83 Wing area (sq.m.) 34,86 Maximum hull width (m) 2,08 Number of seats Crew 2 Maximal 19 Dimensions of passengers cockpit Length (m) 6,34 Maximum width (m) 1,96 Maximum height (m) 1,66 Capacity (cubic m) 17,9 Weights and loads T/O (tons) 6,6 Empty equipped (tons) 4,18 Without fuel (tons) 5,87 Payable load (tons) 1,71 Landing load (tons) 6,4 Fuel capacity (tons) 1290 Additional information Can be increased by 400l by mounting additional fuel tanks at the tips of wings Flight characteristics Range with ( number of passengers ) and cargo ( fuel reserves ) 19 is 670km 380 Maximal permissible altitude (m) 6460 Required takeoff /landing runway length (conditions of МСА, at the sea level ) (m) SМ-92 «Finist» SМ-92 «Finist» is a light single-engine monometallic semicantilever multi-purpose monoplane with high positioned wings and fixed undercarriage. The plane is equipped with М-14P air-cooled powerplant (output 360 hp) with three-bladed МТV-9-В-С/СL 250-27 airscrew. The plane is built for primary training of pilots, carrying passengers and cargos, and for landing parachute jumpers. Crew accommodation: single pilot. The plane has double control. If necessary, two pilots can operate the plane. Length 9.197 m Wingspan 14.6 m Plane 20.44 m² Empty weight 1500 kg Max T/O 2350 kg Max horizontal speed 260 km/h Range 615 — 1200 km Take-off run 250 — 470 m Path length 250 — 210 m. Stalling speed 100 — 115 km/h Max permissible speed 290 km/h Passenger seats 5 — 6 Number of parachute jumpers 6 — 7 L-29 «Dolphin» L-29 «Dolphin» — twin-seated training jet monoplane with middle wings position and retractable undercarriage. Equipped with М-701-с-500 powerplant. The plane is built for primary training of pilots in Norman and severe weather conditions both during the day and at night, as well as for regular training of pilots. Specifications of the plane ensure fulfillment of elementary, intermediate and higher aerobatics figures. The plane has two cockpits: front cockpit for the trainee and the rear one – for the instructor. Length 10.8 m Wingspan 10.3 m Plane 19.8 m² Empty weight 2384 kg Max T/O 3630 kg Max horizontal speed 625 km/h Max range 710 — 920 km Take-off run 600 — 650 m Path length 530 — 600 m. Stalling speed 170 km/h Max permissible speed 790 km/h Max permissible flight overloads: Positive 7 — 8 Negative 3.5 — 4 Ka-26 multi-purpose helicopter Multi-purpose helicopter. Developed by Kamov Designing Bureau. First flight on August 18,1965. The helicopter is built for aviation works in agriculture and forestry, for transportation , sanitary services etc. Year of design 1965 Maximal useful load 800 kg Maximal weight carried on the external mounting 900 kg Number of passengers 6-7 Cruise speed 120 kg/h Range at maximal load 400 km Range at maximal fueling 520 km Fuel consumption 110 kg/h Fuel type Petrol Dimensions of cargo cockpit 1,28*1,37*1,84 m Dimensions of cargo door 1,2*1,3 m Minimal size of landing ground 5*5 m T/O weight 3,3 tons AIRLINE CONTACTS SERVICE ORDER OUR AIRPLANES BUSINESS AVIATION AEROBATICS PILOTS' SCHOOL PARACHUTE JUMPS QUESTIONS AND ANSWERS © 2005 FLIGHTOCEAN info@flightocean.com