2026 DEHAVILLAND DHC 6 300G TWIN OTTER CLASSIC




    Aircraft Summary


    General

    Year
    2026
    Manufacturer
    DEHAVILLAND
    Model
    DHC-6-300G TWIN OTTER CLASSIC
    Condition
    New
    Description
    Q4 2026 De Havilland DHC-6-300G Twin Otter Full Factory Warranty Full Factory Training Provisions Delivery in October 2026 Proven Twin Otter Performance with Updated Avionics.

    Airframe

    Total Time
    0
    Airframe Notes
    Certification Currently Operated – FAR Part 91 / Part 135 / EU OPS Entry into Service Date October 2026 Aircraft Weights Kgs Lbs Max Take Off Weight 5,670 12,500 Max Landing Weight 5,579 12,300 Operating Weight 3,175 7,000

    Engine 1

    Engine 1 Time
    0
    Engine 1 Time Since
    SNEW
    Engine 1 TBO
    4000
    Engine 1 Notes
    Pratt & Whitney Canada – PT6A-27 HSI Due / Overhaul Due 1,800 hr. Hot Section / 3,600 hr. Overhaul Program Coverage Pratty & Whitney ESP Program Available

    Engine 2

    Engine 2 Notes
    Pratt & Whitney Canada – PT6A-27 HSI Due / Overhaul Due 1,800 hr. Hot Section / 3,600 hr. Overhaul Program Coverage Pratty & Whitney ESP Program Available

    Props

    Prop Notes
    Left Propeller Right Propeller Serial Number(s) TBD TBD Total Hours Since New -- -- Overhaul Due 3,000 hr. Overhaul

    Avionics

    Avionics/Radios
    The BASE De Havilland DHC-6-300G is equipped with an integrated, Garmin G1000NXi avionics suite. A general summary of this aircraft’s avionics suite is as follows: Type of Unit - Pilot/Co-Pilot Primary Flight Displays (PDF) (10-inch) - Central Multi-Function Display (MFD) (15-inch) - FMS Controller - Flight Director Mode Controller - Dual Air Data, Attitude, Heading Reference System (ADAHRS) - Dual Magnetometers - Dual Integrated Avionics Units o Single VHF COM Transceiver o GNSS and SBAS certified receivers o VOR/ILS localizer o ILS glide slope receiver - Dual Engine & Airframe Units - Dual Audio Control Panels - Single Mode-S Diversity Transponder (ADS-B In/Out) - Electronic Standby Instrument System (ESIS) - One Magnetic Standby Compass - 406 MHz ELT with Navigation Interface - Combined Cockpit Voice and Flight Data Recorder with Recorder Independent Power Supply IPS) - Aural Warning System - Cockpit USB Charging Ports - Electronic Flight Bag (EFB)

    Additional Equipment

    Additional Equipment
    Float Provisions Stainless Steel Flight Control Cables Airstair Door Additional Corrosion Protection Optional Entry-Into-Service Packages are available Additional Avionics Warranty can be purchased directly with Garmin Additional Configurations available including VIP and Amphibious Floats STOL Capable Single or Dual pilot capable.

    Exterior

    Exterior Notes
    Base Paint Color(s) All-over White with black exhaust stacks Stripe Color(s) Available on request Last Painted Date New Delivery

    Interior

    Interior Notes
    Number of Passengers 19 Passenger Standard Configuration Forward Cabin Configuration 5 Rows of 1 x 2 Economy Seats Aft Cabin Configuration Single Economy Seat opp. Entry Door with Aft 3 Place Economy Seat Bench Other Notable Feature(s) Provisions for under seat stowage of hand baggage. Lap type safety belts, LED overhead lighting, and cabin air outlets are available at each seat position. Last Refurbished Date New Delivery

    Inspection Status

    Inspection Status
    Inspection Last Performed Next Due A Check n/a 125 Flight Hours B Check n/a 250 Flight Hours C Check n/a 500 Flight Hours D Check n/a 6,000 Flight Hours 5 Year Check n/a May 2030 10 Year Check n/a May 2035 Landing Gear Overhaul n/a May 2035 De Havilland Canada offers a comprehensive and fully transferable warranty generally outlined as follows: Expiration Aircraft Limited Warranty – De Havilland Canada 3-years or 3,000 flying hours Engines – Pratt & Whitney Canada 1,000 flight hours (regardless of calendar time) Propeller – Hartzell 2-years or 1,000 flight hours Propeller – Hartzell (de-ice boots) 18-months or 2,000 flight hours (upon original installation) Avionics – Garmin 2-years or 800 flight hours (upon certification of the aircraft)


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