Meet the Piro LC500

✈︎

Meet the Piro LC500 ✈︎

Faster resupply without risk to aircrew

  • Autonomous runway-to-runway

  • 500lb+ payload over a 500+ mile range

  • Rugged, fixed-wing design allows for transporting cargo in, over, around, or through various weather conditions

  • Combustion fuel with ability to build all-electric variant

  • Efficiently transports cargo for multi-mission use without risk to human life

  • Piloted product is already in flight; uncrewed product available Q4 2025

  • NAICS Codes: 336411 - 511210 - 541715

Features:

  • Corrosion resistant

  • Reduce emissions output

  • Payload protection

  • Reduce downtime and lower repair costs

  • Increase durability in-situ

  • Satellite communication-based

    Minimal training required to operate

  • Fully redundant propulsion, controls, & sensor suite

    Robust lost link procedures

  • GPS and Laser/RADAR based navigation

  • Complete aircraft load / unload within five minutes

    Flexible handling & configuration

    Top-entry loading

    Improved cargo protection

  • Fully autonomous operation (uncrewed)

    Flight plan programming by single on-ground pilot

    Dynamic rerouting via satellite link

    On-ground battery swap (approx. 20 min)

    Short 3-week pilot training

Specs & Performance:

  • Motors: Rotax 916iS, 4 Cylinder, Turbo Charged, Air and Liquid Cooled Engine

    Power: 160 hp / Takeoff, 137 hp- Cruise

    Fuel: Avgas or Mogas

  • Wing Span: 30 ft / 9.144 m

    Wing Area: 125 sq ft / 11.61 m²

    Length: 23ft 4in / 7.112 m

    Height: 7ft 9in / 2.362 m

  • Operating Empty Weight (OEW): 992 lbs / 449.06 kg

    Maximum Takeoff Weight (MTOW): +1,500 lbs / 680.39 kg

    Maximum Landing Weight (MLW): +1,500 lbs / 680.39 kg

  • Maximum Payload: +500lbs / 226.80kg

    Cargo Volume: 2 m³ / 75 ft³

    Top Cargo Access Door: 1 m x 1 m / 34” x 34”

  • Cruise Speed: +150 kts / 172.62mph

    Range w/ Maximum Payload: 804 km / 500 miles (+30 min reserve)

    Service Ceiling: 3,048 m / 10,000 ft density altitude (estimated)

  • Take-off run with Max Payload: 304 m / 1,000ft

    Required Runway: 250 m x 8 m / 820 ft x 27 ft

    Surface: Paved, gravel, dirt, grass

    Maximum Demonstrated Crosswind: 30 knots / 15.43m/s

  • Trailer Transportation: Standard size, custom holding brackets. Requires simple wing removal

    Hangar Storage: 40 ft HC sea container

    Disassembly / Assembly: under 20 minutes

  • Total Maintenance Cost: $12.50 per flight hour

    250-hour inspection interval

    Battery: Contact Anatra Sales for details

    Motor / Propeller: On condition

    Landing Gear: On condition

  • FAA - experimental exemption: Q4 2023

    UK CAA - BVLOS approval: Q1 2026

  • First Flight: December 2023

    Demo Flights: 1H2025

    Entry into Service: Q4 2025

Flying Prototype Available Now