The KR-030 Topaz is a strutless high wing design. All major airframe assemblies have a shell structure made of composites based on glass or carbon fibre. The fuselage in the form of a self-supporting shell stiffened locally with 3D material, houses a double cockpit in the front part with places next to each other. Cockpit width 1.2 m. The shell is technologically divided into two symmetrical halves with stiffeners, and an integrated floor - trunk plate, glued in when connecting the halves. Seats with a shell structure made of composites. Cockpit cover - a wind-up glass made of ultraviolet-resistant acrylic glass (PMMA polymethyl methacrylate), side door also made of acrylic glass (PMMA), 3 mm thick, on a composite frame. Vertical stabilizer integral with the fuselage. Tricycle landing gear with a front wheel. The main landing gear legs self-supporting, made of composite. Main wheels braked together, front wheel controlled, coupled to the rudder. Optionally, the wheels are covered with laminated fairings. The wing is made entirely, rectangular, mounted on four bolts. The NN-1817 profile was used for its resistance to contamination of the leading edge, with very favorable aerodynamic characteristics - tested on the PW - 5 "SMYK"glider. The wing structure is shell, sandwich, with a load-bearing girder. Slotted flaps of shell construction, hung to the wing on outriggers, driven by the fuselage - electric, control on a joystick. The aileron is made of carbon laminate due to the necessary high torsional stiffness, with the smallest possible mass (anti-flutter requirements) with a mass balance fixed at its end. Classic horizontal tail with a rectangular contour, shell structure made of composites. Shell rudder. Pusher control systems. Elevator trimmer - spring-loaded, electrically adjustable, control on the joystick 100 l fuel tanks mounted in the wings
Ekolot KR-030 Topaz
Type: Ultralight
SKU: C762175
Maximum Range
Passengers
Max Speed
Rotax 912 ULS 100 PS 4- stroke, 4-cylinder liquid/air cooled engine with opposed cylinders, dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets, integrated reduction gearbox. - additionally, the second fuel pump - electrical Oil thermostat It shortens the oil warm up time to working temperature Allows to maintain working temperature during operation at low ambient temperatures. Carburetor heating system with coolant, controlled from cockpit Coolant thermostat It shortens the engine warm up time to working temperature Allows to maintain working temperature during operation at low ambient temperatures.
EFIS KANARDIA NESIS III 8.4 ", touch screen, Artificial horizon Synthetic view Speedometer, altimeter, variometer, compass, Wind force and direction (Magu required) Navigation: free or subscription maps Possibility to add your own points, routes, airports Log all available parameters (every 1 sec.) Visual and voice alarms (in headphones) for engine, fuel, speed, etc. online - weather radar, METAR, TAF, (Internet connection required) radio standby with ATR 833 radio Engine Monitor: Oil temp, fluid temp Oil pressure, fuel pressure RPM, hour meter CO concentration in the cockpit (CO sensor required) Fuel level, momentary and average fuel consumption MAP Engine board comput VHF Radio Funkwerk ATR 833=II OLED DUAL WATCH 8,33 kHz Supported directly from the EFIS Nesis III menu. - frequency entry - selection of frequencies saved in navigation Magnetic compass 57 mm. Inclinometer - ball Airspeed scaled in km/h, 57 mm Electronic compass - accessories for Nesis. Indicates a magnetic course and allows you to determine the strength and direction of the wind through Nesis III Transponder Funkwerk TRT 800 MODE S , MODE A/C ADS-B out Autopilot - Kanardia 2-axle autopilot system (elevator and ailerons) (the aircraft must be equipped with trim of rudder) Control modes: Level flight - using ailerons and elevator keep the plane in horizontal flight Heading - using ailerons it maintains set course relativ to the ground Vertical speed - using elevator it maintains the set vertical speed (ascent or descent) Altitude - using the rudder it reaches and then maintains the set altitude Flight Director - using ailerons, it §ies to the destination set in navigation
Interior
Two sets of seat belts with logo. Pattern - sport Seat and backrest sport profil Upholstery leather and alcantary Painting inside - dark graphite - sport version Cockpit equipment Exclusive package Mesh containers for trinkets 2 pcs Mats on the floor Armrest-container for trinkets glove compartment Instrument panel - carbon panels or wood imprinted graphics Sun visors for the pilot and passenger USB socket Hanger for headphones Stick - leather Made of carbon fiber, leather covered - sport version Additional control stick for training, teaching Parachute rescue system-Galaxy to 472 kg Fuel system Two combined tanks with a total capacity of 78 liters built in the wings of the aircraft and two small sump tanks in the bottom of the fuselage a total capacity of 8 liters (reserve), optionally available sump tanks of 20 liters. A total of 86 or 98 liters of fuel. Fuel valve on the central console integrated with the starter button -prevents to engine running with the fuel valve closed. Fuel separator and fuel drain valve. Auxiliary electrical fuel pump. Electrics in the cockpit Master power switch Key switch 2 ignition switches - with protection Polymer automatic fuses protecting the power supply Switches for electrical circuits with shielding and signaling of failure of a circuit. Dashboard illumination with smooth saturation regulation 12V socket or dual USB socket Headphone jack 2 sets. Flaps, elevator trimmer, PTT Flaps with electric drive. Trimmer elevator - spring with electric drive Control of §aps and trimmer from the stick Flap and trim position indicators on the NESIS III display PTT button on the stick Electric trim of the rudder An electrically adjustable rudder trimmer. trimmer position indicator on EFIS Nesis III
Exterior
Tinted windows Side and front windows slightly dimmed with PMMA 3mm Ventilation - cab heating Two adjustable air inlets on side windows. Blowing air on the windscreen with variable speed. Adjustable heating of the cab. Engine cover with Cam-Lock fasteners Engine cowling made from carbon fiber with Cam-lock fastners. Inspection flap allows control of the oil level without removing the engine cowling. Trunk-two large luggage compartment on left and right side. Can be loaded through larger holes behind the seats. Wheel fairings of the main wheels and front wheel, painted white Propeller DUC Swirl-3 3 - blade, adjustable on the ground, Swirl-3, carbon Marker lights and stroboscope Standard marker lights: red and green at the ends of the wings. White stroboscope on the vertical fin Standard landing light - LED Exterior painting Sport Brake system - standard Tires with tubes, Aluminium wheels,Kaspar calipers and discs, Kaspar brake pump, plastic brake hoses Cabin cover Protective cover for the cabin of the aircraft (fit to shape) fastened with Velcro.
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| Type | Ultralight |
| Year | 2021 |
| Location | Romania Aerodrom Fratauti, SV |