Guimbal Cabri Australia & New Zealand   |  Pacific Aircraft Services  |  © 2019

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 / Mogas