EX-053 - INTRACOM GENERAL MACHINERY GM 17 VIPER

INTRACOM GENERAL MACHINERY

GM-17 VIPER

Used

EX-053

GM-17 “Viper” turboprop multy purpose aircraft was created by considerable modification of well known American made Piper PA-31P aircraft by request of a Swiss company INTRACOM GENERAL MACHINERY. The aircraft is produced by Smolensk aircraft plant. Two Lycoming engines of 425 hp were removed from the wings and one turboprop Walter M 601E of 750 hp engine was installed in the nose section of the fuselage. New navigational, hydraulic, heating and cabin pressuring systems were installed as well as a new fire alarm, oil, electrical and landing gear systems. Successful modification made reduced empty weight of the aircraft for more than 400 kg that improved its performance and commercial characteristics. GM-17 “Viper” aircraft can perform 6-7 passengers or cargo transportation (1200kg) with maximum range up to 2500 km, speed 430km/h, altitude of flight up to 7500 m, day or night time in normal and complex weather conditions. One or two pilots form a crew of the aircraft. GM-17 “Viper” is equipped with mini bar, toilet, has satellite telephone and fax connection and provides all the necessary conveniences for work and leisure. Using Piper PA-31 fuselage we have created a modern, highly competitive in Russian, European and other countries` market turboprop aircraft with high performance characteristics and low flight hour cost. New navigational, hydraulic, heating and cabin pressuring systems were installed as well as a new fire alarm, oil, electrical and landing gear systems

105.0

Ìàximum take-off and landing weight, kg 3300 Empty weight, êg 1750 Ìàximum commercial load, êg 1000 Fuel, kg 820 Crew 1-2 Passengers 6-7 Wing area, ì2 21.3 Cruise speed ( altitude 3000 ì), km/h 430 Cruise speed (altitude 6000 ì), km/h 405 Service ceiling, km 7.0 Range with full fuel tanks and commercial load 680 kg, altitude 6000 ì, fuel reserve for 40 min, kì 2760 Range with full fuel tanks and commercial load 680 kg, altitude 3000 ì, fuel reserve for 40 min, kì 2200 Ìàximum flight time, h 8 Take off power, maximum weight, continuous throttle, ì/ñ 8,6 Stall speed, flaps down, maximum weight, low gas, km/h 120 Run, ì 460 Run with reverse, ì 350

Engine M-601E Engine power, hp 750

Aircraft structures 1 – V- 510 propeller; 2 – M-601E engine; 3 – fire alarm system; 4 – fire protection partition; 5 – electrical equipment; 6 – battery 20ÍÊÁÍ-25; 7 – hydro system; 8 –pressurizing partition; 9 – instrument panel; 10 – control levers; 11 – passengers cabin; 12 – entrance door (left side); 13 – baggage compartment; 14 – air conditioner; 15 – oxygen system; 16 – avionics; 17 – tail; 18 – tail light BANO; 19 – main landing gear; 20 – nose landing gear.