Pipistrel Velis Electro

Electric • single engine • High Wing • Fixed gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

MOSAIC Eligibile Sport Pilot-flyable
88
KTAS
Cruise Speed
2
Occupants
85
nm
Max Range
-
lbs
Wet Payload

Estimated Ownership Costs

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About the Pipistrel Velis Electro

Overview

The Pipistrel Velis Electro is a two-seat, single-motor electric trainer built by Pipistrel (now part of Textron eAviation) of Slovenia. On 10 June 2020 it became the world’s first fully electric aircraft to receive a full EASA type certificate (EASA.A.573), and as of 2026 it remains the only type-certified electric aircraft in service. It is built on the certified Virus SW 128 airframe, swapping the Rotax piston engine for the 57.6 kW Pipistrel E-811 motor and a 20 kWh liquid-cooled battery system.

The aircraft is purpose-built for flight training, particularly the circuit work and repeated takeoffs and landings that dominate early instruction. It is quiet, produces no local emissions, and costs only a few dollars in electricity per flight. Endurance is around 50 minutes plus VFR reserve, so it suits local training sorties rather than cross-country flying. Since certification it has added validations from the UK CAA (2022), the FAA light-sport route (2024), Transport Canada (2025), and South Korea (2026).

Key Features for GA Buyers

  • Certified, not experimental. The only fully electric aircraft with a full type certificate, so it operates and is maintained under standard certified rules rather than experimental limitations.
  • Very low energy cost. A typical training flight draws only a few kWh; operators report roughly a dollar of electricity per short sortie, a fraction of avgas cost.
  • Quiet and zero local emissions. A low noise footprint eases operations at noise-sensitive fields and reduces community friction for busy flight schools.
  • Simple powerplant. The electric motor has far fewer moving parts than a piston engine, with no mixture, carb heat, or oil management for the student to learn.
  • Proven training airframe. Shares the well-understood Virus SW composite airframe, with benign handling suited to ab-initio students.

Trade-offs

  • Short endurance. Roughly 50 minutes plus reserve limits it to circuits and short local flights; it is not a cross-country machine.
  • Recharge downtime. A full charge takes around 1.5 to 2 hours, so high-utilization schools typically need spare battery packs or multiple airframes to maintain dispatch.
  • Battery replacement cost. The battery system is a major consumable; replacement runs over $20,000, and long-term cycle life is still being established by the manufacturer.
  • Scheduled motor service. The powertrain requires periodic service (bearing and seal work) that can involve returning components to the manufacturer.
  • Limited payload and conditions. Two seats, day VFR only, with a modest useful load that tightens further with two adults aboard.

See Also

Technical Specifications

Dimensions

Wingspan
35.14 ft
Length
21.23 ft
Height
6.23 ft
Parking area (ft2)
1184.02 ft2

Weights

Max Takeoff Weight
1,323 lbs
Max Landing Weight
1,323 lbs
Useful Load
380 lbs

Performance

Cruise Speed
88 KTAS
Never-Exceed (Vne)
108 KIAS
Max Structural Cruise (Vno)
98 KIAS
Approach Speed
58 KIAS
Stall, Clean (Vs1)
51 KIAS
Range
85 NM
Service Ceiling
12,000 ft
Rate of Climb
657 fpm
Takeoff over 50 ft obstacle
1,470 ft
Landing ground roll
1,342 ft

Engine

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