EV-55 Outback

EV-55 Outback Logo
EV-55 Outback Cover Photo

A new generation twin turboprop utility aircraft is now available. Intended for transportation of 9-14 passengers or 1,776 kg of cargo. The EV-55 Outback offers a reliable and high-performance alternative for single-engine turboprop aircraft .   This versatile aircraft has high productivity, operational reliability, easy, and inexpensive maintenance – all available to operators worldwide. Order now.


Versatile Aircraft
The spacious cabin of the airplane offers its passengers a comfortable flight. Alternatively, the aircraft can be loaded with cargo. Convenient loading is ensured by the wide door in the rear part of the fuselage. This versatile airplane even has the ability to have amphibious floats installed, allowing the aircraft to be operated from the river or sea and still land on conventional airstrips. This is the perfect aircraft for parachute operation and special missions.

 Click here to see all EV-55 Aircraft Versions

Reliability and Safety
Two turboprop engines PT6A-21 together with the robust airframe from Al-alloys ensure an unprecedented level of reliability and safety.

ev-55-powerplantHigh Productivity
High speed along with the spacious cabin ensures significantly higher productivity than in piston engine airplanes

All-weather Operationev-55-promo-f4
The EV-55 Outback is not limited by high or low air temperatures or by airport altitude. The robust landing gears of the airplane enable take-off from unpaved or even sodden runways. The reliable de-icing system ensures flight safety even in icing conditions.

Inexpensive Maintenance
Airframe repairs are quick and simple thanks to the metal structure. All key components of the airplane are easily accessible due to large assembly holes. All is located together and in a well arranged manner either in the fuselage nose or in the landing gear nacelles.


Integrated Avionics
An integrated avionics system provides simple navigation, situational awareness and at the same time it provides the crew information on the other aircraft systems – all this is displayed on an LCD display with high resolution.


The EV-55 Outback has been designed for utility aircraft operators which are looking for:

  • Modern aerodynamic design reflecting the latest trends in General Aviation
  • Robust all metal airframe with composite materials used in non-structural parts of construction
  • Twin turboprop engine reliability and safety
  • High speed for high operation productivity
  • Spacious cabin for maximum comfort of passengers with fast change of configuration from 9 pax interior to combi or cargo version
  • Outstanding operation versatility; STOL characteristics, operation from unpaved airfields and also at hot & high conditions

 High productivity & versatility, low operation costs & twin engine reliability.

Max. Speed of Horizontal Flight at 10 000 ft 220 KTAS
Stall speed, flaps 0° 77 KEAS
Stall speed, flaps 38° 64 KEAS
Take-off performance (MTOW)
Take-off run ISA, H = 0 ft (SL) 1 122 ft 342 m
Total distance over 50 ft obstacle, ISA, H = 0 ft (SL) 1 378 ft 420 m
Total distance over 50 ft obstaclet, ISA, H = 0 ft (SL), STOL 1 124 ft 373 m
Take-off run ISA+20°C, H = 6 562 ft 1 624 ft 495 m
Total distance over 50 ft obstacle, ISA+20°C, H = 6 562 ft 2 000 ft 610 m
Climb performance
Both engines operating 1673 fpm 8.5 m/s
One engine non-operating 453 fpm 2.3 m/s
Landing performance (MLW)
Landing run ISA, H = 0 ft (SL) 1 014 ft 309 m
Total distance over 50 ft obstacle, ISA, H = 0 ft (SL) 1 673 ft 510 m
Total distance over 50 ft obstacle, ISA, H = 0 ft (SL), STOL 1 391 ft 424 m
Landing run ISA+20°C, H = 6 562 ft 1 394 ft 425 m
Total distance over 50 ft obstacle, ISA+20°C, H = 6 562 ft 2 133 ft 650 m

Engine Specs:

  • Manufacturer Pratt & Whitney
  • Model PT6A-21
  • Max. take-off power 2 x 535 hp
  • TBO 3,600 FH


  • Manufacturer Avia Propellers
  • Model AVIA AV-844
  • Type 4-blade, constant speed
  • Diameter 82 in 2.082 m



Primary flight display (PFD) 2 pcs Mode S Transponder
Multi-functional display (MFD) Automatic direction finder optional
Central console unit Distance measuring unit optional
Flight display controller 2 pcs TAWS system optional
Integrated digital autopilot TAS system optional
VOR/ILS/COM receivers 2 pcs Stormscope optional
GPS receivers 2 pcs Satellite weather receiver optional
Sensor reference system 2 pcs Synthetic vision system optional
Magnetometer 2 pcs Radar altimeter optional
Data concentrator unit 2 pcs Weather radar optional
Audio panel HF transceiver optional
MKR receiver


Information Displayed on the MFD:

Moving map Fuel indication – volume, flow, reserve
Map north indicator Engine parameters indication
Wind indicator Electronic charts (subscription fro Jeppesen required)
Range ring and compass TAS data optional
Ground track pointer TAWS data optional
Waypoint Satellite weather datalink data optional
Waypoint identifier Wheater radar data optional
Current leg in flight plan Lightning data optional
Airport and airport information DME hold mode indicator

Information Displayed on the PFD:

Airspeed Vertical deviation – glideslope with glidepath
Altitude Magnetic compass
Vertical speed Radar altimeter data optional
Attitude with slip/skid indication Synthetic vision feature optional
Horizontal situation indication Obstacle display

Dimensions and Weights:

External dimesions
Wing span 52.82 ft 16.10 m
Length 47.47 ft 14.35 m
Height 15.28 ft 4.66 m
HTU span 15.75 ft 4.80 m
Wheel track 9.58 ft 2.92 m
Wheel base 13.68 ft 4.17 m
Operating weights
Max. take-off weight 10 140 lb 4 600 kg
Basic empty weight (cargo version) 5 725 lb 2 597 kg
Basic empty weight (pax version) 5 860 lb 2 658 kg
Max. fuel 3 651 lb 1 656 kg
Max. payload 3 915 lb 1 776 kg
Max. weight in the rear baggage comp. 551 lb 250 kg
Max. weight in the front baggage comp. 221 lb 100 kg
Cabin specification
Number of passengers 9 (14)
Seating arrangement 1+1 (1+2)
Seat pitch 32.7 in 83 cm
Passenger cabin (excl. cockpit)
Length 197.6 in 5.02 m
Width 63.4 in 1.61 m
Height 54 in 1.37 m
Volume 334 cu.ft 9.47 m³
Baggage compartment volume
Rear (aft of pax. cabin) 95 cu.ft 2.7 m³
Front 18 cu.ft 0.5 m³
Entry and cargo door
Width – passenger part 28 in 0.71 m
Width – fully opened for cargo loading 49.2 in 1.25 m
Height 54 in 1.37 m

Year Interior:



Year 2017
Manufacturer EVEKTOR
For Sale Call
Location Tipp City, OH
Condition Used
Total Time 0 Hours
Flight Rules IFR
Number Of Seats 9

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