2018 Pilatus PC-12 NG for sale, Switzerland

Elite Avionics Package, including:
Co-Pilot PFD
Co-Pilot Audio/Marker Panel
TAWS Class B & TCAS I
Smart View Synthetic Vision System
Wireless Connected Flight Deck
Stormscope (WX500)
2nd GPS
GPS WAAS/LPV Functionality Honeywell KGS200
ADS-B Out
2nd Mode S Transponder (Diversity)
Honeywell Dual ChartLink
RVSM (Reduced Vertical Separation Minimum)
Coupled VNAV
Iridium Antenna (antenna only)
Electronic Checklist Function

Avionics and instruments
Integrated Honeywell Primus Apex Suite
– 1 Primary Flight Display (PFD), Flat Panel Display Unit, 10.4” Diagonal
• ADI/HSI (Dual-channel Data Source for Air Data, Attitude and Heading Reference)
• 1 Radar Altimeter
• Engine Instruments
• 2 COM (8,33 KHz Spacing)
• 2 NAV (1 DME)
• 1 Mode S Transponder (Diversity)
• 1 ADF
– 2 Primary Flight Display (PFD) Controller
– 1 Elapsed Timer
– 1 Integrated GPS Receiver
– 1 Audio/Marker Panel
– 1 Flight Guidance Controller for Digital Three-Axes Autopilot System
– 1 Situational Awareness Multifunction Display (MFD), Flat Panel Display Unit, 10.4”
Diagonal
• Flight Management System (FMS)
• Weather Radar Indication
• Moving Map with Overlays
– 1 Systems Multifunction Display (MFD), Flat Panel Display Unit, 10.4” Diagonal
• Warnings, Cautions and Advisories (CAS
• Messaging)
• Gear, Trim and Flaps Indication
• Fuel Indication
• ECS/CPCS Indication
• Electrical Systems Indication
– 1 Multifunction Display (MFD) Controller (includes Alphanumeric Keyboard)
– 1 Cursor Control Device (CCD)
– 1 Central Maintenance System
Other Flight Instrumentation
– Dual Pitot Static System
– 1 RDR2000 Weather Radar
– 1 Integrated Electronic Standby Instrument System (ESIS)
– 1 ELT 406 MHz with Remote Switch
– 1 Nav Interface to 406 MHz ELT
– 1 Flight Time Recorder (“Hobbs Meter”)
– 1 Lightweight data recorder
Cabin:
– 9 Oval Cabin Windows with Internal Pull-down Shades
– Painted Composite Interior Panels
– Carpet
– Aft Baggage Storage Area including Baggage Net
– 2 Cabin Speakers
– 1 Document Holder
Cabin Lights
– 1 Passenger Door Flood Light
– 1 Cargo Door Flood Light
– 1 Cabin Light System
– Independent Reading Lights (1 per Seat)
– 1 Baggage Compartment Light
Cockpit compartment:
– 2 Crew Control Wheels, 2 Rudder Pedal Sets
– 2 Crew Seats – 8-way Adjustable, Reclining with Foldable Armrest, Headrest, and
4-point Torso Restraint System
– 2 Cockpit Speakers
– 2 Hand Microphones
– 2 Active Noise Reduction (ANR) Headsets
– Painted Composite Interior Panels
– Carpet
– 1 Cockpit/Cabin Bulkhead Divider with Curtain
– 2 Adjustable Sunvisors
– AFM/En-route Chart Storage Pockets
– Clipboard/Notepad, Pen Holders
– 2 Cup Holders
– 1 Direct Vision (DV) Window
Cockpit Lights
– 2 Ceiling Lights
– 4 Adjustable Panel Flood Lights
– 4 Adjustable Circuit-breaker Flood Lights
– 2 Map Reading Lights
– Internally Lighted Switch Panels
– Internally Lighted Cockpit Controllers

Structures:
– Aluminum Alloy for Primary Skin and Structure
– Epoxy Resin-based Composites for Secondary Parts
– Semi-monocoque Design Pressurized Fuselage
– Pilot/Passenger Airstair Door
– Cargo Door
– Overwing Emergency Exit
– 2 High-lift Wings
– T-tail Empennage
– Complete Internal and External Structure Corrosion Protection

Executive 6 Seat Interior
Quilted Seat Facings

Airconditioning System
Aerowave 100 In-flight Internet
Cargo Kit
Steep Approach Capability
RDR-2060 Radar

Aircraft systems:
Propulsion System
– 1 Pratt & Whitney Canada PT6A-67P Turboprop Engine
– 1 Hartzell Five-blade Composite Propeller
– Engine Chip Detector System
Electrical System
– 2 Starter/Generator Units 28 VDC, 300 Amps each
– Automatic Load Shedding
– 2 Lead Acid Batteries 24 VDC, 42 Amp Hours each
– 1 Emergency Power System (EPS), 24 DC, 5 Amp Hours
– 1 External Power Connector for 28VDC Power Source
Fuel System
– 2 Integral Fuel Tanks with Delivery and Transfer System
– 2 Motive-flow Delivery (Jet) Pumps
– 2 Electrical Boost Pumps
– 1 Engine-driven Pump
Flight Controls
– All-mechanical Primary Flight Controls
– Electrically Operated Flaps
– Electrical Trim in all Axes
Landing Gear
– Electromechanical Retractable Tricycle Landing Gear with
Trailing Link Main Gear
– Soft-field/Low-pressure Tires
– Emergency Gear Extension System
– Mechanical Nosewheel Steering
– Toe-operated Pedal Wheel Brakes
– Parking Brake
Cabin Pressurization Control System (CPCS)
– 1 Electronically Controlled Outflow Valve
– 1 Digital Controller
– 1 Pneumatic Safety Valve
– 2 Negative Pressure Relief Valves
Environmental Control System (ECS)
– Air Cycle System – using Engine Bleed Air to Provide Conditioned Air for
Pressurization, Heating and Cooling
– 1 Digital ECS Controller (for Air Cycle System, Auxiliary Heaters, Recirculation Fans
and Optional Vapor Cycle Cooling System)
– Dual Zone Temperature Control (Cockpit and Cabin)
– Auxiliary Electrical Heating System (2 Underfloor Heaters)
– Conditioned Air Distribution via 4 Cockpit Outlets (2 Floor, 2 Adjustable Chest
level) and Cabin Floor-level Outlets
– Re-circulated Air Distribution via Adjustable Overhead Cabin and Cockpit Outlets
(1 per Seat)
Oxygen System
– Supplemental Oxygen System
– 1 Oxygen Cylinder
– 2 Crew Diluter Demand Masks with Integral Connected Microphones
– 1 Constant-flow Mask per Passenger
– 1 Oxygen Quantity Indicator
Ice and Rain Protection
– Wing Leading Edge Pneumatic De-icing Boots
– Horizontal Stabilizer Pneumatic De-icing Boots
– Windshield Electrical Anti-icing
– Engine Inlet Exhaust Gas Heat Anti-icing
– Propeller Blades Electrical Anti-icing Boots
– Pitot-static Probe Electrical Anti-icing
– Stall Warning Sensors Electrical Anti-icing
Exterior Lights
– 2 LED Combined Wingtip Lights (Strobe and Nav)
– 2 LED Landing Lights
– 1 LED Taxi Light
– 1 Wing Icing Inspection Light (Left Side)
– 2 LED Red Flashing Beacons