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    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
    2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale2024 PILATUS PC-12 NGX Used Turboprop Aircraft for sale
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    2024 PILATUS PC-12 NGX

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    Aircraft Location:Camarillo, California

    Seller Information

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    Avex Aviation LLC

    Contact:Danielle Booth

    Camarillo, California

    General

    Year
    2024
    Manufacturer
    Model
    Serial Number
    2383
    Condition
    Used
    Registration #
    N250KK
    FlightRules
    IFR
    Description
    The Pilatus PC-12 has earned its reputation as one of the world’s most trusted and versatile business aircraft. From transporting families and business executives to supporting critical cargo missions, the PC-12 delivers an exceptional combination of performance, comfort, efficiency, and operational flexibility. With more than seven million flight hours and over 1,700 aircraft delivered, the PC-12 has established an outstanding legacy of safety, reliability, and proven performance. Strong residual values, low operating costs, and exceptional versatility make it one of the most compelling investments in business aviation. Discover why professionals like you trust AVEX!

    Airframe

    Total Time
    230
    Complete Logs
    Yes
    Winglets
    Yes
    Airframe Notes
    AIRFRAME - Aluminum alloy primary structure and skin panels - Epoxy resin composite secondary structures - Semi-monocoque pressurized fuselage - High-lift wing design with integral fuel tanks - Winglets for improved aerodynamic efficiency - T-tail empennage configuration - Complete internal and external corrosion protection - Retractable tricycle landing gear with electrohydraulic actuation - Trailing-link main landing gear - Emergency landing gear extension system - Low-pressure tires for unimproved runway operations - Mechanical nosewheel steering - Hydraulic wheel braking system - Pilot/passenger entry door with integrated airstair - Large aft cargo door for passenger and freight loading - Overwing emergency exit - Pressurized cabin with 5.75 PSI max differential - Digital cabin pressurization control - Dual integral wing fuel tanks - Automatic fuel transfer and balancing system - Dual electric fuel boost pumps - Certified for single-pilot IFR operations - Certified for flight into known icing conditions (FIKI) - Maximum operating altitude: 30,000 ft - Maximum takeoff weight: 10,450 lbs - Usable fuel capacity: 402 US gallons

    Engine Program

    Engine Maintenance Program
    ESP

    Engine 1

    Engine 1 Make/Model
    PRATT & WHITNEY PT6E-67XP
    Engine 1 Time
    250 SNEW
    Engine 1 TBO
    5000
    Engine 1 Notes
    - Dual-Channel Engine and Propeller Electronic Control System (EPECS) - Electronic Engine Control (EEC) - Data Collection and Transmission Unit (DCTU) - Fuel Control Unit (FCU) - Propeller Control Unit (PCU) - Single-Lever Throttle Quadrant Assembly (TQA) - Single-Crystal Compressor Turbine Blades - Optimized Turbine Cooling System - Digital Propeller Speed Management - Integrated Engine Diagnostics and Health Monitoring System - 5,000-Hour Time Between Overhaul (TBO) - 600-Hour Scheduled Maintenance Intervals CAMP Engine Monitoring Program ENGINE SPECS - Pratt & Whitney Canada PT6E-67XP turboprop engine - Rated thermodynamic power: 1,845 SHP - Normal takeoff power: 1,200 SHP - Climb flat rating: 1,200 SHP - Cruise flat rating: 1,100 SHP - Electronic Propeller and Engine Control System (EPECS) - Electronic Engine Controller (EEC) - Integrated digital engine and propeller management - Single-lever engine power control - Integrated digital autothrottle - Automatic engine start sequence management - Automatic engine temperature and torque limiting - Automatic propeller speed control - Hartzell five-blade composite propeller - Full-feathering and reversing propeller system - Normal propeller speed: 1,700 RPM - Low-speed propeller mode: 1,550 RPM - Integrated engine health and trend monitoring - Engine chip detection system - Engine data recording and transmission capability - Improved hot-and-high engine performance - Engine time between overhauls (TBO): 5,000 hours - Propeller overhaul interval: 4,000 hours

    Props

    Prop 1 Manufacturer
    HARTZELL
    Prop 1 Time
    230 SNEW
    Number of Blades
    5
    Prop Notes
    Hartzell Five-Blade Composite Propeller

    Avionics

    Flight Deck Manufacturer/Model
    HONEYWELL PRIMUS APEX
    ADS-B Equipped
    Yes
    SVT
    Yes
    Avionics/Radios
    The PC-12 NGX further enhances this technology with upgraded processors, touchscreen controllers, and immersive 3D audio, improving overall functionality, efficiency, and the pilot experience. - 2D Airport Maps+ ADS-B IN (SURF) - Co-Pilot PFD with Audio/ Marker Panel - Second GPS - Second Mode S Transponder (Diversity & ADS-B Out) - KMA-29A Audio Panel Upgrade - Cockpit Display of Traffic Information - Wireless Connected Flight Deck - Honeywell Dual Charts - Stormscope® (WX500) - SmartRunway & SmartLanding (RAAS) - VHF Data link with AFIS - Electronic Checklist with CAS Linking - Iridium® Antenna and Port - Auto-throttle - Graphical Weather (VDL M2) - ATN-B1 CPDLC - USB Charging Ports in Cockpit Type A & C -XM Radio & Weather - Four 10-inch high-resolution LCD flight displays - Primary Flight Display (PFD) - Multifunction Display (MFD) - Integrated engine indication and crew alerting system - Dual Flight Management System (FMS) - SmartView synthetic vision system - Interactive Navigation (INAV) system - Touchscreen avionics controller - Cursor Control Device (CCD) - Integrated GPS navigation - Air Data and Attitude Heading Reference System (ADAHRS) - Integrated electronic flight instrumentation - Digital engine torque and temperature indication - Propeller RPM and engine performance indication - Fuel quantity and fuel system monitoring - Landing gear position and status indication - Flap and trim position indication - Cabin altitude and differential pressure indication - Electrical system voltage and current monitoring - Crew Alerting System (CAS) - Master caution and warning annunciation - Integrated autopilot flight mode annunciation - Emergency standby instrument system - Traffic Alert and Collision Avoidance System (TCAS I/II, configuration dependent)

    Additional Equipment

    Additional Equipment
    ELECTRICAL EQUIPMENT - 28 VDC electrical distribution system - Dual 28 VDC, 300-amp starter/generator units - Automatic electrical load shedding - Dual 24 VDC, 42 Ah main batteries - Independent 24 VDC, 5 Ah emergency power supply - Essential and main electrical distribution buses - External 28 VDC ground power receptacle - Overhead electrical power control panel - Integrated electrical system monitoring and alerting - LED navigation and position lights - LED anti-collision beacon lights - Wing-mounted landing and taxi lights - LED cockpit and cabin lighting - Adjustable instrument panel illumination - Electrically actuated wing flaps - Electrically operated trim systems - Electrohydraulic landing gear actuation - Electrically heated windshield system - Electrically heated pitot-static probes - Electrically heated propeller blade anti-icing - Electrically heated angle-of-attack sensor ICE PROTECTION - Certified Flight Into Known Icing (FIKI) - Pneumatic wing leading-edge de-icing boots - Pneumatic horizontal stabilizer de-icing boots - Electrically heated propeller blade anti-icing - Electrically heated engine inlet anti-icing system - Electrically heated pilot/ copilot windshield - Electrically heated pitot probes - Electrically heated static ports - Electrically heated angle-of-attack sensor - Integrated engine inlet ice protection - Ice protection system controls on cockpit panel - Ice protection system status and warning indications

    Exterior

    Year Painted
    2024
    Exterior Notes
    NGX Launch Paint Scheme: -Cobalt Blue Metallic -Nouvelle White Pearl -Pepper Gray Pearl -Cumulus Grey Metallic -Dark Blue Mist Metallic

    Interior

    Year Interior
    2024
    Number of Seats
    10
    Configuration
    Passenger
    Interior Notes
    - BMW Designworks-inspired executive cabin interior - Eight-seat executive cabin configuration - Optional additional passenger seating configurations - Fully reclining executive passenger seats - Increased executive seat back height - Premium European leather upholstery - Custom leather stitching and trim finishes - Adjustable passenger headrests and armrests - Executive club seating arrangement - Coat hanger - Foldable cabin table - Internally accessible aft baggage compartment - Baggage compartment volume: 40 cu ft - Large aft cargo loading door - Private forward lavatory compartment CONFIGURATION Executive 8-Seat Interior - Five 115V AC Power Outlets (2 Cockpit/ 3 Cabin) - USB cabin charger ports (8 seats - 6 chargers) (Type A & C) MAIN INTERIOR PACKAGE - Tundra Design Seat Front, Seat Back & Shroud - Seat Accent & Seat Upper Armrest in Leather INTERIOR OPTIONS - Crew Seats: Light Package - Crew Seat Leather: Volaero Berlin (Light) - Crew Seat Armrest: Aeronappa Aplomado (Light) - Crew Seat Sheepskin: Aerolamb Taupe (Light) ADDITIONAL CABIN COMPONENTS - Pillows (Custom Design) and Plisse - Cockpit Curtain (Mountain Design) in Mira X Alpbach CARPET AND METAL COMPONENTS - Carpet (Canyon Design) Material Tisca Sonoma 1002 - Plating (Canyon Design) Material HT405 Nickel Light Aged TABLES AND CABINETS - Veneer (Mountain Design) Material Smoked Oak Recon 12.68 - Gloss Table Inserts (Tundra Design), Material Leather, Rangali AN-W-0304

    Modifications/Conversions

    Dual Aft Body Strakes
    Yes

    Inspection Status

    Airworthy
    Yes
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