For Sale
Microlight / ULM
Ekolot KR-030 KR-030
108,000 €
plus VAT
Where this price stands
See these 231 adverts2 of these adverts are shares, each counted at the price of its whole aircraft.
In line with the market
13,000 € above the median
Among the 231 Microlight / ULM adverts from 2019 to 2026
Specifications
- Registration
- 9A-URS
- Year of manufacture
- 2024
- Engine
- Rotax 912 IS Sport 100 PS
- Based at
- Croatia
This model
The usual configuration for this model. This aircraft may differ.
- Type approval
- MFR.ekolot.kr-030-topaz — the manufacturer's own data, not an approval
Equipment
What the advert mentions, answered from the seller's list below.
- Autopilot yes
- Glass Cockpit yes
- ADS-B yes
- Transponder yes
- Airframe Parachute yes
As the seller listed it
- EFIS KANARDIA NESIS III 8.4" touch screen
- Magnetic compass
- Inclinometer - ball
- Electronic magnetic compass
- Transponder Funkwerk TRT 800 MODE S, MODE A/C ADS-B out
- VHF Radio Funkwerk ATR 833 II OLED DUAL WATCH 8.33 kHz
1 more item
- Autopilot - Kanardia 2-axle
The seller's description
Reproduced as published, in the original language.
EKOLOT TOPAZ
Meet the KR-030 Topaz
The strutless high wing created with attention to every detail.
Elegant - fast - comfortable
The KR-030 Topaz is a strutless high wing.
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.
Engine Rotax 912 IS Sport 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, redundant electronic fuel injection system, engine management system, integrated reduction gearbox.