Technical Specifications

To view the Cabri G2 specifications document (PDF) click here.

Performance
Equipped empty weight 420 Kg (925 lb)
Maximum Gross Weight 700 Kg (1,542 lb)
Maximum level speed @ 100% (s.l. ISA) 100 kt (185 km/h)
Cruise speed @ 85% 90 kt (166 km/h)
Vne (s.l.) 130 kt (240 km/h)
IGE hovering ceiling (@ 700 kg) 5,000 ft
Hovering ceiling (2×77 kg + fuel 2 hrs) 7,500 ft
Range @ 85 % (15 min reserve) 380 nm (700 km)
Maximum endurance @ 50 kt (no reserve) 5 hr 40 min
Noise level @ 100% (certified) 75.7 dB SEL
Main Rotor
Type Articulated, soft-in-plane
Number of blades 3
Diameter 7.2 m (23.6 ft)
Chord 180 mm (7.1 in)
Speed 530 RPM
Tail Rotor
Type Fenestron®
Number of blades 7
Diameter 0.6 m (23.6 in)
Chord 42 mm (1.6 in)
Speed 5,148 RPM
Transmission
Primary transmission Belt with a reduction ration of 0.855/1
Main gearbox Bevel spiral gear with a reduction ratio of 11/47
Tail gearbox Bevel spiral gear with a multiplication ration of 25/11
Powerplant
Engine model Lycoming O360-J2A with STC EASA E.S.01001
Type Horizontally-opposed, four cylinder, air cooled,
carbureted, double ignition with one magneto and
one electronic ignition
Displacement 361 cu.in (5.9 litres)
Max continuous power 145 shp @ 2,585 – 2,700 tr/min (108 kW)
Normal speed 2,650 RPM
Cooling Direct-drive squirrel-cage blower
Ignition
Magneto Bendix
Electronic ignition LSE Plasma II – HG Condenser discharge Variable spark advance
Fuel system
Max capacity 170 litres (45 US Gal)
Unusable quantity 1.5 litres (0.4 US Gal)
Approved fuel type Avgas 100 LL