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!Specifications
Year2024
ManufacturerPILATUS
ModelPC-12 NGX
Serial Number2383
ConditionUsed
Registration #N250KK
FlightRulesIFR
Total Time230
Complete LogsYes
WingletsYes
Airframe NotesAIRFRAME
- 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 Maintenance ProgramESP
Engine 1 Make/ModelPRATT & WHITNEY PT6E-67XP
Engine 1 Time250 SNEW
Engine 1 TBO5000
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
Prop 1 ManufacturerHARTZELL
Prop 1 Time230 SNEW
Number of Blades5
Prop NotesHartzell Five-Blade Composite Propeller
Flight Deck Manufacturer/ModelHONEYWELL PRIMUS APEX
ADS-B EquippedYes
SVTYes
Avionics/RadiosThe 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 EquipmentELECTRICAL 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
Year Painted2024
Exterior NotesNGX Launch Paint Scheme:
-Cobalt Blue Metallic
-Nouvelle White Pearl
-Pepper Gray Pearl
-Cumulus Grey Metallic
-Dark Blue Mist Metallic
Year Interior2024
Number of Seats10
ConfigurationPassenger
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
Dual Aft Body StrakesYes
AirworthyYes
Year2024|
ManufacturerPILATUS|
ModelPC-12 NGX|
Serial Number2383|
ConditionUsed|
Registration #N250KK|
FlightRulesIFR|
Total Time230|
Complete LogsYes|
WingletsYes|
Airframe NotesAIRFRAME
- 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 Maintenance ProgramESP|
Engine 1 Make/ModelPRATT & WHITNEY PT6E-67XP |
Engine 1 Time250 SNEW |
Engine 1 TBO5000|
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|
Prop 1 ManufacturerHARTZELL|
Prop 1 Time230 SNEW |
Number of Blades5|
Prop NotesHartzell Five-Blade Composite Propeller|
Flight Deck Manufacturer/ModelHONEYWELL PRIMUS APEX |
ADS-B EquippedYes|
SVTYes|
Avionics/RadiosThe 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 EquipmentELECTRICAL 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|
Year Painted2024|
Exterior NotesNGX Launch Paint Scheme:
-Cobalt Blue Metallic
-Nouvelle White Pearl
-Pepper Gray Pearl
-Cumulus Grey Metallic
-Dark Blue Mist Metallic|
Year Interior2024|
Number of Seats10|
ConfigurationPassenger|
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|
Dual Aft Body StrakesYes|
AirworthyYes|
