 |
 |
2 Piloti + 2 Adulti • Max. Fuel Capacity 490 lt 129 gals
• Max. Speed (Sea Level) 200 Kts
• Cruising Speed (75%Pwr, 6000ft) 175 Kts
• Max. Take Off Weight 1550 Kg 3417 lb
• Range (75%Pwr, 6000ft) 1200 NM
• Useful Load 570 Kg 1256 lb
• Max. Luggage Weight 65 kg 143 lb
AIRCRAFT DESIGN (Wing Data)
• Span 10.1 m 28 ft
• Surface 13.5 sqm 145 sqft
• Aspect Ratio 7.6
• Root Chord 1.780 m 5.84 ft
• Tip Chord 0.718 m 2.36 ft
AIRCRAFT DESIGN (Certifications)
EASA CS 23 / FAA FAR 23 Categoria Utility (n = +4.4 / -1.76) IFR Notturno ed Avvicinamenti in Cat 1 mediante ILS.
 |
 |
 |
AIRCRAFT DESIGN (Ergonometry)
STD Dummy 95o percentile M -5o percentile F Cabin Access Luggage Compartment Access Adjustable Front Seats from 5o F to 95o M (Same Downwards Visibility) Left / Right Hand Pilot in Command Accomodation Optional AirBags
 |
 |
AIRCRAFT DESIGN (Powerplant)
Engine TCM IOF -550 -N2B (with FADEC) 310 HP @ 2700 RPM Three Blade Hartzell Constant Speed Propeller Diameter 76 in McCauley Propeller Pitch Control
AIRCRAFT DESIGN (Main Features)
Advanced Instrument Panel (TAA) Full Composites Construction (Carbon Fibre Pre – preg Materials) All Electric Systems (Landing Gear, Flaps and Trim) Redundancy (Two Generators, Two Batteries and Duplicated Navigation Functions) Comfort (Cold / Hot Air, Air Conditioning System , Windshield Demister and Portable OX) Safety (Manual Landing Gear Extension, Fire Extinguishing System, Single Fuel Tank and Crash Impact Absorbing Structure)