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Triavio Italo

October 21, 2023

The Triavio Italo (Italian) is an Italian ultralight aircraft, designed and produced by Triavio of Catania, introduced at the AERO Friedrichshafen show in 2013. The aircraft is intended to be supplied as a kit for amateur construction or complete and ready-to-fly.[1]

Italo
Role Ultralight aircraft and Light-sport aircraft
National origin Italy
Manufacturer Triavio SRL
Introduction 2013
Status Under development (2017)

Design and development Edit

The Italo was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft (LSA) rules. It will also be available as a homebuilt aircraft kit. It features a cantilever low-wing, an enclosed cockpit with two-seats-in-side-by-side configuration under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from sheet aluminum. Its 7.77 m (25.5 ft) span wing employs slotted flaps. Standard engines available will be the 100 hp (75 kW) Rotax 912ULS and 912iS four-stroke powerplants.[1]

The design was shown at the 2013 AERO Friedrichshafen show, but was still under development in 2015 and was not yet advertised for sale on the company website in March 2017.[1][2]

A future LSA version is planned, but as of March 2017, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[3]

Specifications (Italo) Edit

Data from Tacke[1][4]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.66 m (21 ft 10 in)
  • Wingspan: 7.77 m (25 ft 6 in)
  • Height: 2.45 m (8 ft 0 in)
  • Empty weight: 320 kg (705 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 100 litres (22 imp gal; 26 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 3-bladed composite

Performance

  • Maximum speed: 260 km/h (160 mph, 140 kn)
  • Cruise speed: 240 km/h (150 mph, 130 kn) 75% power
  • Stall speed: 65 km/h (40 mph, 35 kn) flaps down, engine off
  • Range: 1,600 km (990 mi, 860 nmi)
  • Service ceiling: 4,550 m (14,930 ft)
  • g limits: +4/-2
  • Rate of climb: 6.1 m/s (1,200 ft/min)
  • Landing run: 120 m (390 ft)

References Edit

  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 86. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ Triavio (2013). "Services". triavio.eu. Retrieved 23 March 2017.
  3. ^ Federal Aviation Administration (26 September 2016). "SLSA Make/Model Directory". Retrieved 23 March 2017.
  4. ^ Gunston, Bill (2015). Jane's All the World's Aircraft  : development & production : 2015-16. IHS Global. p. 461. ISBN 978-0-7106-3135-0.

External links Edit

  • Official website

October 21, 2023
triavio, italo, italian, italian, ultralight, aircraft, designed, produced, triavio, catania, introduced, aero, friedrichshafen, show, 2013, aircraft, intended, supplied, amateur, construction, complete, ready, italorole, ultralight, aircraft, light, sport, ai. The Triavio Italo Italian is an Italian ultralight aircraft designed and produced by Triavio of Catania introduced at the AERO Friedrichshafen show in 2013 The aircraft is intended to be supplied as a kit for amateur construction or complete and ready to fly 1 ItaloRole Ultralight aircraft and Light sport aircraftNational origin ItalyManufacturer Triavio SRLIntroduction 2013Status Under development 2017 Contents 1 Design and development 2 Specifications Italo 3 References 4 External linksDesign and development EditThe Italo was designed to comply with the Federation Aeronautique Internationale microlight rules and US light sport aircraft LSA rules It will also be available as a homebuilt aircraft kit It features a cantilever low wing an enclosed cockpit with two seats in side by side configuration under a bubble canopy retractable tricycle landing gear and a single engine in tractor configuration 1 The aircraft is made from sheet aluminum Its 7 77 m 25 5 ft span wing employs slotted flaps Standard engines available will be the 100 hp 75 kW Rotax 912ULS and 912iS four stroke powerplants 1 The design was shown at the 2013 AERO Friedrichshafen show but was still under development in 2015 and was not yet advertised for sale on the company website in March 2017 1 2 A future LSA version is planned but as of March 2017 the design does not appear on the Federal Aviation Administration s list of approved special light sport aircraft 3 Specifications Italo EditData from Tacke 1 4 General characteristicsCrew one Capacity one passenger Length 6 66 m 21 ft 10 in Wingspan 7 77 m 25 ft 6 in Height 2 45 m 8 ft 0 in Empty weight 320 kg 705 lb Gross weight 472 5 kg 1 042 lb Fuel capacity 100 litres 22 imp gal 26 US gal Powerplant 1 Rotax 912ULS four cylinder liquid and air cooled four stroke aircraft engine 75 kW 101 hp Propellers 3 bladed compositePerformance Maximum speed 260 km h 160 mph 140 kn Cruise speed 240 km h 150 mph 130 kn 75 power Stall speed 65 km h 40 mph 35 kn flaps down engine off Range 1 600 km 990 mi 860 nmi Service ceiling 4 550 m 14 930 ft g limits 4 2 Rate of climb 6 1 m s 1 200 ft min Landing run 120 m 390 ft References Edit a b c d e Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 86 Flying Pages Europe SARL 2015 ISSN 1368 485X Triavio 2013 Services triavio eu Retrieved 23 March 2017 Federal Aviation Administration 26 September 2016 SLSA Make Model Directory Retrieved 23 March 2017 Gunston Bill 2015 Jane s All the World s Aircraft development amp production 2015 16 IHS Global p 461 ISBN 978 0 7106 3135 0 External links EditOfficial websitePortals nbsp Italy nbsp Companies nbsp Aviation Retrieved from https en wikipedia org w index php title Triavio Italo amp oldid 1126753262, wikipedia, wiki, book, books, library,

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