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 2200four-stroke powerplant.[1]
^ abcdefgTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 63-64. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External linksedit
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Official website
January 01, 1970
jabiru, j160, australian, ultralight, trainer, designed, produced, jabiru, aircraft, bundaberg, queensland, certified, australian, primary, aircraft, category, aircraft, supplied, complete, ready, j160, j160, role, ultralight, aircraft, national, origin, austr. 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 1 J160 J160 C Role Ultralight aircraft National origin Australia Manufacturer Jabiru Aircraft Status In production 2015 Variants Jabiru J170 Contents 1 Design and development 2 Variants 3 Specifications J160 4 References 5 External linksDesign and development editThe 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 1 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 1 The design was developed into the Jabiru J170 by adding the wing from the Jabiru J430 for the light sport aircraft category 1 Variants edit nbsp J160 C J160 C Early model 1 J160 D Certified version 1 Specifications J160 edit nbsp J160 Data from Tacke 1 General characteristicsCrew 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 edit a b c d e f g Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 63 64 Flying Pages Europe SARL 2015 ISSN 1368 485XExternal links edit nbsp Wikimedia Commons has media related to Jabiru J160 Official website Retrieved from https en wikipedia org w index php title Jabiru J160 amp oldid 1126156301, wikipedia, wiki, book, books, library,
