The AN-2 was intended to have certification completed in the European Aviation Safety Agency Very Light Rotorcraft category by May 2010, and then again by the end of 2012 but, by January 2013, this does not seem to have been completed. Kits were intended to be ready for delivery in February 2010, but were not yet available as of January 2013. By late in 2011 there was no indication that the prototype had been flown.[3][4]
By 2012 the company website was redirected to Cicare Europe and all mention of the AN-2 had been removed. It is likely development had ended by that point.[5]
The aircraft fuselage is made from aluminium sheet. Its 6.99 m (22.9 ft) diameter two-bladed rotors both have chords of 18 cm (7.1 in). The aircraft has an empty weight of 390 kg (860 lb) and a gross weight of 600 kg (1,323 lb), giving a useful load of 210 kg (463 lb).[1]
aeris, naviter, enara, basque, swallow, spanish, helicopter, that, under, development, aeris, naviter, sebastián, first, shown, 2009, paris, show, paris, bourget, airport, aircraft, intended, supplied, amateur, construction, complete, ready, aircraft, enara, r. The Aeris Naviter AN 2 Enara Basque for Swallow is a Spanish helicopter that was under development by Aeris Naviter of San Sebastian The AN 2 was first shown at the 2009 Paris Air Show at Paris Le Bourget Airport The aircraft was intended to be supplied as a kit for amateur construction or as a complete ready to fly aircraft 1 2 An 2 Enara Role Helicopter National origin Spain Manufacturer Aeris Naviter First flight Pending Introduction 2009 Status Development ended 2012 The AN 2 was intended to have certification completed in the European Aviation Safety Agency Very Light Rotorcraft category by May 2010 and then again by the end of 2012 but by January 2013 this does not seem to have been completed Kits were intended to be ready for delivery in February 2010 but were not yet available as of January 2013 By late in 2011 there was no indication that the prototype had been flown 3 4 By 2012 the company website was redirected to Cicare Europe and all mention of the AN 2 had been removed It is likely development had ended by that point 5 Contents 1 Design and development 2 Specifications AN 2 Enara 3 References 4 External linksDesign and development editThe AN 2 Enara features a two rotor coaxial main rotor a two seats in tandem enclosed cockpit tricycle landing gear with suspension an H tail and a four cylinder four stroke 115 hp 86 kW BMW automotive engine Plans for other powerplants include the four cylinder air cooled four stroke dual ignition 115 hp 86 kW Lycoming IO 233 light sport aircraft engine 1 The aircraft fuselage is made from aluminium sheet Its 6 99 m 22 9 ft diameter two bladed rotors both have chords of 18 cm 7 1 in The aircraft has an empty weight of 390 kg 860 lb and a gross weight of 600 kg 1 323 lb giving a useful load of 210 kg 463 lb 1 Specifications AN 2 Enara editData from Bayerl 1 General characteristicsCrew one Capacity one passenger Empty weight 390 kg 860 lb Gross weight 600 kg 1 323 lb Powerplant 1 BMW 1200 four cylinder four stroke automotive engine 86 kW 115 hp Performance Maximum speed 170 km h 110 mph 92 kn Cruise speed 150 km h 93 mph 81 kn References edit a b c d Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 189 WDLA UK Lancaster UK 2011 ISSN 1368 485X Aeris Naviter 10 May 2009 AN 2 Enara Rollout Retrieved 22 January 2013 permanent dead link Aeris Naviter n d AN 2 Enara Archived from the original on 15 February 2013 Retrieved 22 January 2013 Jane s Information Group 11 October 2011 Aeris Naviter AN 2 Enara Spain Aircraft Rotary wing Civil Retrieved 22 January 2013 Aeris Naviter 2009 Aeris Naviter aerisnaviter com Archived from the original on 23 December 2011 Retrieved 28 November 2018 External links editOfficial website archives on Archive org Photo of the AN 2 Enara on Airliners net Retrieved from https en wikipedia org w index php title Aeris Naviter AN 2 Enara amp oldid 1149677329, wikipedia, wiki, book, books, library,
