TECHNICAL SPECIFICATIONS
PERFORMANCE
Equipped empty weight
Maximum Gross Weight
Maximum Level Speed @ 90% (s.l. ISA)
Cruise Speed @ 80%
Vne @ SL
IGE Hovering Ceiling (2x77 kg + fuel 2 hours)
Range @ 85 % (15 min reserve)
Maximum Endurance @ 50 kt (no reserve)
Noise Level @ 100 % (certified)
420 kg (925 lb) approx.
700 kg (1,542 lb)
100 kt (185 km/h)
90 kt (166 km/h)
130 KIAS
7,500 ft
380 NM (700 km)
5 hr 40 min
75.7 dB SEL
MAIN ROTOR
Type
Number of Blades
Diameter
Chord
Speed
Articulated, soft-in-plane
3
7.2 m (23.6 ft)
180 mm (7.1 in)
530 RPM
TAIL ROTOR
Type
Number of Blades
Diameter
Chord
Speed
Fenestron
7
0.6 m (23.6 in)
42 mm (1.6 in)
5,148 RPM
TRANSMISSION
Primary Transmission
Main Gearbox
Tail Gearbox
Belt with a reduction rations of 0.855/1
Bevel spiral gear with a reduction ratio of 11/47
Bevel spiral gear with a multiplication ration of 25/11
POWERPLANT
Engine Model
Type
Displacement
Max Continuous Power
Take Off Power
Normal Speed
Cooling
Lycoming O360-J2A with STC EASA E.S.01001
Horizontally-opposed, four cynlinder, air cooled, carbureted, double ignition with one magneto and one electronic ignition
361 cu.in (5.9 litres)
145 hp @ 2,650 tr/min (108 kW)
160 hp @ 2,650 tr/min (108 kW)
2,650 RPM
Direct-drive squirrel-cage blower
IGNITION
Magneto
Electronic Ignition
Bendix
LSE Plasma II - HG Condenser discharge Variable spark advance
FUEL SYSTEM
Max Capacity
Unusable Quantity
Approved Fuel Type
170 litres (45 US Gal)
1.5 litres (0.4 US Gal)
Avgas 100 LL