AutoGyro’s Calidus is a closed-cabin two-seat tandem model, certified as the world’s first factory-built gyroplane in 2009. Loved for its aesthetics and flight experience, Calidus is a popular choice for flight schools, sightseeing, and law enforcement.
The sharp aerodynamics mean that Calidus is a fast cruiser. With a fuel tank of 74 liter, it has a great range. The huge clear canopy gives both the pilot and passenger an amazing 360 view; yet keeping them both warm, dry, and comfortable.
Canopy options
full enclosed canopy with ventilation windows
open sided canopy, where large side windows allow plenty of air access
high-headroom canopy for very tall pilots
full open top canopy
The Calidus, AutoGyro’s sleek two-seat model, features an efficient heating system like all enclosed AutoGyro aircraft. So no matter where the aircraft is operating, or the season, there is always a way to keep warm, or keep cool!
As a workhorse, this aircraft has an excellent pedigree. With over 500 released to service since 2009, AutoGyro has a huge depth of reliability experience around the world, whether operated for fun or reward. We know that the work environment is a hard daily toil for aircraft and take pride in the ability of our aircraft to reach that standard. You can rely on exceptional support from the AutoGyro factory and partners, who provide backing worldwide.
Fantastic clear 360deg view for pilot and passenger
Fabulous fighter-style cockpit feel
Easily adjustable seat position, and rake angle
Heated cabin with variable flow rate
Huge options list of Garmin equipment, including ADSB in and out
Excellent payload, MTOM up to 560kg
Unique occupant safety cell concept
74ltr fuel tanks, safe 3hr hour range.
Safe and reliable design, as verified by numerous aviation authorities.
Optional auxiliary alternator to give plenty of onboard electrical energy.
Over 500 in service, meaning huge service experience around the world.
Technical Specifications
Technical Details
Model Details
L X W X H:
4,8 m x 1,7 m x 2,7 m (15.66 ft x 5.67 ft x 9.1 ft)
Rotor Diameter:
8.4 m / 8.6 m (27.3 ft / 27.95 ft )
Empty Weight:
265-305 kg
MTOW (Max Take Off Weight):
560 kg (1232 lbs) 914UL or 500kg (1100 lbs) 912ULS
Engine:
Rotax 914 UL | 912 ULS
Takeoff Distance *2:
70 m 914UL | 90 m 912ULS
Max Endurance *3:
up to 3,5 hours *
Max Range *3:
up to 500 km (315 miles) **
Cruise Speed:
140km/h (90 mph)
Fuel Capacity:
74 L (19.5 US Gallons)
Compliant With:
BUT, Section T, ASRA, CCAR-21, USA Primary Category
Technical data can vary regarding country-specific legal requirements *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
