Flying means freedom. Flying gyros means pure freedom. But flying the MTOnautic is limitless. Equipped with floats, the MTOnautic lands and takes off from water connecting the elements like no other. Maximizing fun and flexibility, the adaptation of the MTOsport is just as free and versatile as technically thought-through. The Nautic gives access to completely new fields of application. No matter if it’s in Scandinavia or the United Arabic Emirates, if on private or commercial basis – the MTOnautic takes you where you want to go.
True 360deg view for maximum observation capability.
Sea or inland water operation, take off and landing .
Nose mounted camera capability.
Stainless steel unpainted airframe; easy to inspect and no corrosion.
Rear seat observer/camera operator.
Superb safety for off-shore operations.
Long range 96ltr fuel tank.
Can be supplied with dual or multiple radio systems for combined aerial and marine communications.
No need for a lifeboat; you are flying in one!
A friendly face for serious coastal patrol missions.
Prices are as is at June 2024 and subject to change without notice.
Prices are ex-works and do not include taxes, shipping cost, import- or customs duties or fees
Technical Overview
Technical Details
Model Details
L x W x H (exlude rotor)
5.25 m x 1.9 m x 2.8 m (17.06 ft x 5.85 ft x 9.1 ft)
Rotor Length
8.4 m | 8.6 m | 8.8 m (27.3 ft | 27.95 ft | 28.6 ft)
Empty Weight
350 kg (772 lbs) Depending on options chosen
MTOM (Max. Take-Off Mass)
560 to 650 kg (1235 to 1433 lbs) Depending on market limitations
Engine
Rotax 912 ULS | 914 UL | 915 iS | 916 iS
Take-off distance
70 to 110 m (230 to 361 ft)
Take-off distance, to clear 15 m (45 ft) obstacle
260 m (854 ft)
Climb rate
Up to 6.0 m/s (1170 fpm)
Max. endurance
Up to 4.5 hours
Max. range
Up to 550 km (330 miles)
Cruise speed
90 to 185 km/h (55 to 115 mph)
Max. speed (Vne)
195 km/h (120 mph)
Fuel capacity
65 to 96 L (17 to 25 US gallons)
Comply with
Swedish EASA Flight Certification, USA Experimental Category
All performance indicators shown in the table above reflect the basic aircraft capability. Means of measurement, defined performance and actual performance
limitations vary from region to region, depending on individual country airworthiness requirements and resultant limitations, and may vary from that shown.
Consult your country partner to learn more.
*2: typical aircraft configuration, 1 pilot (80kg), 40 ltr fuel, 2000 ft MSL
*3: typical aircraft configuration, 1 pilot (80kg), max fuel, 2000 ft MSL