The innovative Calidus is unique and groundbreaking in design, engineering, comfort, and in-flight characteristics. Prepared for the most diverse demands and weather conditions, the Calidus copes easily with turbulence and proves that the air is its element.
With Calidus you can experience all of it. Thanks to the interchangeable open and closed canopies, any panorama can be enjoyed to the max.
The brand new Calidus product brochure is now available online. It features the latest product information round about the Calidus and the service that AutoGyro provides. Click the file name to download the brochure.
We look forward to hearing from you!
Product Brochure Calidus [19,7 MB]
| L x W x H: |
4,8 m x 1,7 m x 2,7 m |
| Empty weight: | 265-305 kg |
| MTOW: | 450-560 kg |
| Engine: | Rotax 912 ULS | 914 UL |
| Takeoff distance*1: | 90 m | 70 m |
| Max endurance*2: | 5,0 h | 4,4 h |
| Max range*2: | 600 km | 525 km |
| Cruise speed: | 140 km/h |
| Max speed: | 195 km/h |
| Fuel capacity: | 70 ltr |
| Compliant with: | BUT, Section T, ASRA |
Technical data can vary regarding country-specific legal requirements, and is also depending on propeller/rotor/fuel and aircraft configuration.
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• Closed, two seat autogyro in tandem configuration
• Monocoque cell with closed canopy fitted with emergency vision vent and 2 side vents (left and right)
• Patented Silent Block System
• Mast and tail boom electropolished
• Aluminum rotor system Naca 8H12 8,4m / 8,8m / TOPP
• Rotax 912ULS with 100 HP or Rotax 914 UL Turbo with 115 HP fitted complete with a slipper clutch and exhaust system
• Propeller HTC 3B CW172,5
• Pneumatic pitch trim and rotor brake
• Pneumatic pre rotator
• Hydraulic mainwheel brakes with parking lock
• 39ltr fuel tank
• Rotor tie down bag
• Fully painted body and all composite panels
• Pilot seat with angle and position adjustable seatback
• Seating position and angle adjustable for body size from 165 to 200 cm
• Seats include a four point harness
• Choivce of standard colours, or unlimited colours
• Ready for you, full inspected and test flown
Instrument Panel:
• Airspeed indicator
• Engine and rotor rpm
• Oil temperature
• Oil pressure
• Engine CHT
• Compass
• Hour (Hobbs) meter
• Electric fuel gauge
Additional Equipment*
Engine
• Second fuel pump (electrical) for Rotax 912 ULS
• Auxiliary tank 36ltr
• Electrical in-flight variable-pitch propeller IVO DL3-68 “3 sheet, 172 cm, switching position from 18 to 28 degrees
Color
Avionics
• ELT automatic radio beacon Kannad 406 AF-Compact
• Radio f.u.n.k.e. Avionics ATR833 incl. wiring harness
• Integral antenna in the tail or bow
• Transponder f.u.n.k.e. Avionics TRT800H incl. wiring harness
• Card compass in place of standard compass
School Equipment
• Flight instructor set consisting of throttle, brake, switches, rear seat stick
Lighting
• Landing lights LED (2 x 2,5 W) incl. wiring harness
• Strobes incl. navigation lights LED
Cockpit
• GPS cockpit variants for GPS devices and RAM mountings (according to catalogue)
• Climb indicator (VSI) 80 and/or 57 mm
Energy Supply
• 12V socket for energy supply
Special Equipment
• Roll trim
• Summer canopy (cut outs on left and right side)
• Painted sunroof
• Additional side-vent in the back
• Cockpit heating variable
• Spinner (painted) für HTC / IVO-Prop
• Wheel housings painted
• Heavy duty or sport tires
• Floats as kits (currently certified in Sweden)
• Fire Warning System
• Footmat (front and rear)
• Set of luggage bags (left and right
• Luggage bag pilot seat
*) Die Grund- und Zusatzausstattung ist länderspezifisch und zulassungsrelevant. Wir beraten euch gern persönlich.
