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VS (stall speed): 45 kts | 52 mph | 83 kph
VC (cruise speed): 100 kts | 115 mph | 185 kph
VNE (never exceed speed) : 132 kts | 152 mph | 244 kph
Climb ratio: 500 ft/min | 3 m/s
Glide ratio: 10:1

Takeoff distance over 50ft (15m) obstacle: 650 ft | 198 m
Landing distance over 50ft (15m) obstacle: 546 ft | 166 m

MEW (manufacturers empty weight): 295 kg | 650 lbs
MTOW (maximum takeoff weight): 540 kg | 1190 lbs

Engine: jabiru 2200cc
Fuel consumption: 13lt/hr Cruise

The Jabiru J160-C aircraft has been developed as a new trainer aircraft that is bigger all round. It has a wider cockpit higher cabin and more leg room. Jabiru has an Australian Type Certificate in the primary category for the J160 as well as a production certificate.

Conventional configuration

  • Designed to JAR VLA European Airworthiness Standard
  • High-winged, strut-braced monoplane with wing flaps, mass balanced elevator and in-flight adjustable trim.
  • Cruise Speed @ 3050 rpm 100 knots
  • Range (nil reserve) - 1030 nautical miles
  • 4 stroke JABIRU 2200 cc engine designed specifically for the Jabiru aircraft.
  • Gentle and predictable stall characteristics, together with light and responsive controls, make JABIRU a true sport aircraft.
  • Stall speed with flaps at Gross Weight 45 KIAS
  • Fully enclosed, ergonomically designed cabin with 2 doors providing ease of entry and low noise levels.
  • Excellent visibility
  • Side-by side fixed seating with centre controls and panel mounted throttles. Ideal for training or recreation.
  • Tricycle undercarriage with steerable nosewheel and hand operated in line hydraulic disc brakes makes ground handling a breeze.
  • Excellent cross wind handling performance 14 knots
  • All composite construction removes the corrosion problem. Wing and power loadings provide high performance and handling, particularly in turbulence.
  • Comfortable seating with easily removed covers.
  • Designed for minimum maintenance. Upper and lower cowls easily removed.
  • Auxiliary electronic fuel pump for ease of starting and added security in flight.
  • All the engine management features of conventional GA light aircraft: Carburetor Air Heat, Dual Ignition, Pressure Compensating Carburetor - no mixture control!
  • Jabiru fixed pitch wooden propeller with composite cover and urethane leading edge Avionics include VHF Transceiver, PM501 Intercom and headsets Transponder Altitude Encoder optional.


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