• Source: Jabiru J160

The Jabiru J160 is an Australian ultralight trainer, designed and produced by Jabiru Aircraft of Bundaberg, Queensland. Certified in the Australian primary aircraft category, the aircraft is supplied complete and ready-to-fly.




Design and development


The J160 features a strut-braced high-wing, an enclosed cabin with two-seats-in-side-by-side configuration accessed by doors, fixed tricycle landing gear and a single engine in tractor configuration.
The aircraft is made from composite materials. Its 8.12 m (26.6 ft) span wing has an area of 8.04 m2 (86.5 sq ft) and mounts flaps. The standard engine available is the 80 hp (60 kW) Jabiru 2200 four-stroke powerplant.
The design was developed into the Jabiru J170, by adding the wing from the Jabiru J430, for the light-sport aircraft category.




Variants



J160-C
Early model
J160-D
Certified version




Specifications (J160)



Data from TackeGeneral characteristics
Crew: one
Capacity: one passenger
Wingspan: 8.12 m (26 ft 8 in)
Wing area: 8.04 m2 (86.5 sq ft)
Empty weight: 300 kg (661 lb)
Gross weight: 540 kg (1,190 lb)
Fuel capacity: 135 litres (30 imp gal; 36 US gal)
Powerplant: 1 × Jabiru 2200 four cylinder, air-cooled, four stroke aircraft engine, 60 kW (80 hp)
Propellers: 2-bladed wooden, fixed pitch
Performance

Cruise speed: 185 km/h (115 mph, 100 kn)
Stall speed: 84 km/h (52 mph, 45 kn)
Wing loading: 67.2 kg/m2 (13.8 lb/sq ft)




References






External links



Official website

Kata Kunci Pencarian:

• Jabiru J160
• Jabiru 2200
• Jabiru Aircraft
• Jabiru J170
• Jabiru J250
• Jabiru (disambiguation)
• Bowden cable
• List of civil aircraft
• List of aircraft (J)
• List of RA-Aus certified aircraft types