Similar to aerial counterparts, the Aero Freyr aircraft possesses a high-wing configuration. In its latest model year, standard compass openable windows have been incorporated to enhance overall comfort. Propelled by the 180 hp Lycoming IO-360-M1A engine, it has the versatility to run on AvGas or alternative fuels. Tailoring to owner preferences, the aircraft provides the choice between a constant pitch propeller and, optionally, a fixed pitch propeller.
The four-seat cabin is exceptionally utilitarian, featuring three doors and a dedicated luggage compartment with a capacity of 40 kg (88lb). Deliberate cockpit design ensures that all commands, switches, and circuit breakers are ergonomically positioned for the pilot, minimizing parallax errors.
For cutting-edge avionics, the preferred standard package includes a state-of-the-art IFR cockpit equipped with a Garmin G500 Txi, paired with a GTN650 unit. Additionally, the Aero Freyr aircraft holds utility category classification, signifying an expansion of its ambitious capabilities.
In response to customer input, Aero Freyr has enhanced the new Aero Freyr aircraft, making it even more versatile and adaptable for training. It now boasts a plethora of new features and options to cater to the diverse operational profiles and requirements of different flight schools.
| Engine: Lycoming IO-360-M1A rated 180 Hp at 2700 rpm | ||
| Max Take-Off Weight | 1155 kg | 2546 lb |
| Typically Equipped Empty Weight | 763 kg | 1682 lb |
| Maximum Useful Load | 392 kg | 864 lb |
| Usable Fuel Capacity | 190 lt | 50 gal |
| Maximum Seating Capacity | 4 | 4 |
| Max Luggage Weight | 40 kg | 88 lb |
| Cruise speed @75%, ISA, 6000 ft, MTOW | 237 km/h | 128 ktas |
| Range – 3 persons of 77 kg, 45-min reserve, 60% power, 10,000 ft | 1065 km | 575 nm |
| Rate of climb at MTOW, ISA conditions, at Sea Level | 222 m/min | 730 ft/min |
| Service Ceiling | 4500 m | 14700 ft |
| Take-Off Distance to clear 50 ft, MTOW, ISA | 427 m | 1400 ft |
| Landing distance over 50ft obstacle, MLM, ISA, full flap | 427 m | 1400 ft |
| Fixed pitch propeller option available | ||
| Alternative Fuels, Mogas (EN 228) |
Crafted for resilience, the Aero Freyr aircraft prioritizes robust metal over disposable plastic materials. Aligning with Aero Freyr’s design principles centered on durability, safety, and outstanding value, the single-engine piston aircraft mirrors the company’s extensive expertise in crafting intricate certified multi-engine aircraft. Utilizing this wealth of experience, Aero Freyr introduces an attractively priced single-engine aircraft, aiming to welcome a greater number of pilots into the Aero Freyr family.
Boasting outstanding performance, employing modern manufacturing techniques, featuring advanced avionics, and offering remarkable cost-effectiveness in terms of acquisition, the Aero Freyr aircraft emerges as a compelling option in the current piston single-engine aircraft landscape. The fuselage is meticulously crafted, featuring a front section with an open truss structure composed of high-strength steel tubing intricately welded into triangular shapes for enhanced strength and rigidity. Covered with riveted skin, the rear section adopts a semi-monocoque construction, incorporating frames and four main stringers with riveted skin.
The wing comprises two strutted half-wings, constructed with all-metal stressed-skin, full cantilever, metallic leading edges, and composite wing tips. The aircraft’s empennages, including the vertical fin, rudder, and stabilator, follow an all-metal stressed-skin, full cantilever design.
