LOGISTICS CENTER Industrial Park Miskolc Hungary Phone: +36 30 206 5953 (German) +36 70 354 4144 (English) mail@ideaaircraft.eu For productions, sales, logistics, marketing issues and press materials, please contact our office in Miskolc.
Miskolc
TRAINING FACILITY Hejőkeresztúr, Hungary N 470 57’ 00,66’’, E 200 51’.49,37’ Runway direction: 270 / 090 Runway dimensions: 1000/180 (L/W) Location: Hejőkeresztúr 200 degree 3,0 km Please visit our testing and training facility to see the IDEA Hydropteron on water, in the air or on the ground.
INTRODUCTION Thank you for your enquiry. We, at IDEA Aircraft Ltd. have set the target of designing an "all-in-one" aircraft that has outstanding features in every aspect. As a result of that, we have designed the two-seat and threeseat versions of Hydropteron which shows outstanding performance in terms of both travelling speed and efficiency range. One of the most excellent features of our aircraft is the facility to land on or take off from water so the nearest available runway may not only be a concrete or grassy airport but also the water surface of a beautiful lake or river.
Hydropteron is a very comfortable and reliable partner on ground, water and in air. Our excellent engineers have developed an interior that really makes the passengers feel comfortable. As a result of our efforts, our customers can leave the 2D space behind and enter the exciting universe of 3D travelling for the price of a premium category car.
TECHNICAL DATA two seats
Full length: Wing span: Weight: Height: Flying speed: Range:
6.9 m 10.9 m 560 Kg 2.2 m 180-220 km/h 700-900 km
SAFETY FEATURES Aircraft instrumentation: Altimeter, speedometer, variometer, magnetic compass, radio, transponder C and engine control instruments. Optional instrumentation: GPS system and EFIS - D10A flight control instrument or full IFR instrumentation. It ensures the safety of passengers with parachutes even in the most critical situations when the emergency landing system of the aircraft is activated.
COMFORT Comfort of the pilot and the passengers are provided by the heating and air conditioning (optional) system in the outstanding heat and sound insulating passenger space as well as the seats providing long-term comfort sitting position and the well-designed head and leg rooms.
OTHER FEATURES The Hydropteron A1 is manufactured with two constructions. The 2-seat version meets the requirements of microlight specified in the aviation rules of the USA while the 3-seat version is going to be licensed in the VLA category ( MTOW 750 Kg -1667 lbs.). Design of the luggage trunk makes this version suitable for transportation of fishing, hunting or diving equipment.
FLYING EXPERIENCE The most crucial points of an aircraft is the navigability. In this aspect, our amphibian is high above the standard of aircrafts of the similar size. Its simple navigability and outstanding maneuverability is combined with great flying stability. Therefore pilots can embrace the aircraft just after a few minutes and can confidently keep it under control in all situations. Members of the IDEA Pilot Club give picturesque testimonials on both meetings and online.
YOUR UNIQUE IDEA... With premium category cars, it is a well-tried practice that colors, interior materials and accessories are customized based on the customer's needs. The Hydopteron gives the same freedom of selection with a microlight. Color of the aircraft, the interior trim and materials used can be selected at the customer's option whether it is an Airbrush polish or an Alcantara trim.
Spread out your fantasy and design your dream aircraft! Do you have special concepts? Our colleagues are more than willing to assist you with the list of optional accessories, safety and comfort equipment.
TECHNICAL SPECIFICATIONS
Take – off distance to 15 m (50 ft.) from water: 500 m (1.640,4 ft.) Climbing rate: 3 m/sec (590,6 ft/min) Maximum speed (0 ft., IAS): VNE 210 Km/h (113,39 kts/h) Crusing speed 75 % MC, H= 6000 ft: 164 Km/h (88,55 kts/h) Manuever speed: VA 186 Km/h (100,43 kts/h) Stall speed, 0 degree flaps landing: 73 Km/h (39,42 kts/h) Stall speed, 30 degree flaps landing: 59,2 Km/h (31,86 kts/h) Engine: Manufacturer: Aprilia S. PA (Rotax) Ttype: PA Power max. take – off: 104 KW/140 HP / 3100 RPM Power max. continous: 88 KW/118 HP / 2950 RPM Crusing 75 % MC: 78,3 KW/105 HP / 2700 RPM Crusing 60 % MC: 62,64 KW/84 HP / 2500 RPM
two seats
Length: 6,9 m (19,69 ft.) Wing span: 10,9 m (32,81 ft.) Alpha bf: 30 Wing V position ( φvf): 1,70 Wing surface ( Wing A): 12,47 m2 Mean Aerodynamic Chord (MAC): 1,26 m Effective aspect ratio of wing (Alpha eff): 9,21 Height: 2,2 m (6,56 ft.) Weight details: Empty weight: Maximum take – off Weight: Crew 2 person Bagagge C/G position Load factors Fuel tank capacity:
350 kg (777,78 lbs.) 560 kg ( 1.244,4 lbs.) 2x 80 kg 2 x 177,8 lbs 20 kg ( 45 lbs) (24 – 40) % MAC + 4,5; - 1,5; 50 l (13,21 US. gall)
Take – off run: Take – off grand: 200 m (656,17 ft.) Take – off water: 250 m (820,2 ft.) Take – off distance to 15 m (50 ft.) from ground: 450 m (1.476,38 ft.)
Propeller: Manufacturer: Type: Number of blades: Diameter:
Woodcomp SR 3000/3 3 1.700 mm (66,93 inch)