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turboprop engines (535 shaft horsepower), driving four-blade propellers. The wing is mounted atop a nearly-square fuselage, which has five windows per side. The trailing-link tricycle landing gear retracts into the nose section or pods on the lower fuselage. Expected maximum cruise speed is 220 knots
135:
In June 2018, its price was $ 4 million and two aircraft should finish development flights with 200 hours in 2016, for 500 total hours. Evektor secured enough investment to complete the certification process scheduled for 2017, with a minority investment from a
154:
conversion to fly in 2020, with only one PT6A-21 running a 400 kW (540 hp) generator in the rear compartment, for much lower noise, an 18% fuel saving and the same payload and performance: a 3 hours endurance and 40 minutes from electric power only.
123:
In 2004 the company announced its plan to design and construct a two-engined utility aircraft that would carry up to 14 passengers or 4000 lb (1800 kg) of cargo, and operate from unimproved fields and at high-altitude airports.
131:
in June 2011, with company pilot Josef
Charvat and military pilot Maj. Jiri Hana at the controls. It was estimated at $ 2.1 to $ 2.2 million in 2012. The first production-conforming aircraft flew from Kunovice in April 2016.
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The 5.02m x 1.61m cabin standard layout is five and four seats with a cargo compartment separated by a semi bulkhead and a L-410 sized double door at the rear. It is equipped with a full glass cockpit, Czech firm
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With nine passengers, range is 800nm (1,480km), it can take-off in 410m and land in 520m and with more speed, range and short take-off and landing capability, it can replace ageing piston-twins like the
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The project's development was suspended on 16 March 2017 due to "some uncertainties" with
Evektor's Malaysian investor.
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115:. The prototype first flew on 24 June 2011. The project's development was suspended in March 2017.
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1,713 km (1,064 mi, 925 nmi) , 2,000 lb (907 kg) payload
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4-bladed AVIA AV-844, 2.082 m (6 ft 10 in) diameter constant speed
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is not needed. The less expensive, unpressurised EV-55 won't compete with the
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2,597 kg (5,725 lb) , cargo, passengers: 2,658kg / 5,860lb
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119 km/h (74 mph, 64 kn) with flaps, 77 kn without
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is a twin-engine turboprop aircraft designed and built in the
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1 776 kg / 3 915 lb payload, 9 pax (14 if regulation allowed)
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The EV-55 is of conventional high-wing utility design with a
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The first prototype, an EV-55M (military version), flew from
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By
December 2018, it was touted as a basis for an EVE-55
546:(Press release). Evektor. 16 March 2017. Archived from
505:"SmartDeck panel added to Evektor's new turboprop twin"
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410 km/h (250 mph, 220 kn) at 10,000 ft
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Aircraft of comparable role, configuration, and era
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526:"Evektor flies first production-conforming EV-55"
481:. Evektor-Aerotechnik. June 2011. Archived from
140:company backed by the country's former premier
588:"EV-55 Outback : Technical Specification"
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8:
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473:
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571:"EVE-55 - The Future Strategy of Evektor"
437:"Can the Evektor EV-55 stay the course?"
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167:. The prototype aircraft is powered by
569:Dr. Gerd Berchtold (4 December 2018).
20:
7:
387:De Havilland Canada DHC-6 Twin Otter
216:makes the four-blade propellers and
144:, but not to begin full production.
544:"EV-55 Outback project information"
259:14.35 m (47 ft 1 in)
87:Development suspended (March 2017)
708:2010s Czech civil utility aircraft
456:"Evektor EV-55 Makes First Flight"
192:of a larger turboprop such as the
14:
303:, 399 kW (535 hp) each
361:
347:
29:
728:Twin-turboprop tractor aircraft
435:Murdo Morrison (14 June 2016).
454:Pope, Stephen (29 June 2011).
297:Pratt & Whitney Canada PT6
283:4,600 kg (10,141 lb)
1:
46:Twin-engined utility aircraft
723:Aircraft first flown in 2011
265:16.10 m (52.82 ft)
271:4.66 m (15.28 ft)
169:Pratt & Whitney PT6A-21
744:
188:single turboprop when the
97:2 + 1 for static testing
37:
28:
23:
152:hybrid electric aircraft
238:General characteristics
182:Britten-Norman Islander
38:EV-55 prototype (2011)
590:. Evektor-Aerotechnik.
402:Tecnam P2012 Traveller
224:Specifications (EV-55)
479:"Project information"
355:Czech Republic portal
105:Evektor EV-55 Outback
441:Flight International
654:Fixed-wing aircraft
289:1,656 kg (3,651 lb)
281:Max takeoff weight:
206:Beechcraft King Air
113:Evektor-Aerotechnik
70:Evektor-Aerotechnik
713:High-wing aircraft
550:on 11 October 2017
397:Let L-410 Turbolet
382:CASA C-212 Aviocar
220:the landing gear.
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485:on 11 August 2011
184:, or the smaller
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718:Evektor aircraft
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607:Official website
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576:. Evektor Group.
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532:. 14 April 2016.
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142:Mahathir Mohamad
129:Kunovice Airport
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48:Type of aircraft
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16:Utility aircraft
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511:. 5 March 2012.
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369:Aviation portal
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322:Maximum speed:
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287:Fuel capacity:
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218:Aero Vodochody
186:Cessna Caravan
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109:Czech Republic
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60:Czech Republic
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687:VUT100 Cobra
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552:. Retrieved
548:the original
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328:Stall speed:
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172:(407 km/h).
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93:Number built
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392:Dornier 228
315:Performance
307:Propellers:
293:Powerplant:
119:Development
702:Categories
554:11 October
415:References
198:Twin Otter
196:or Viking
178:Cessna 421
682:SportStar
489:22 August
301:turboprop
263:Wingspan:
251:Capacity:
229:Data from
138:Malaysian
662:EuroStar
647:aircraft
341:See also
232:Evektor.
677:Harmony
645:Evektor
269:Height:
257:Length:
84:Status
530:Flying
461:Flying
334:Range:
165:T-tail
159:Design
574:(PDF)
299:A-21
245:Crew:
194:L-410
43:Role
667:EPOS
556:2017
509:AOPA
491:2011
295:2 ×
214:Avia
180:and
103:The
208:.
204:or
111:by
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528:.
517:^
507:.
470:^
458:.
439:.
423:^
637:e
630:t
623:v
558:.
493:.
443:.
247:2
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