Pilatus Centre Canada

Airframe/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

Aircraft Systems

Propulsion System

1 Pratt & Whitney Canada PT6A-67P Turboprop Engine

1 Hartzell Four-blade Metal Propeller

Electrical System

2 Starter/Generator Units 28 VDC, 300 Amps each

Automatic Load Shedding

2 Lead Acide Batteries 24 VDC, 42 Amp Hours each

1 Emergency Power System (EPS)

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

Hydraulic 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

Hydraulic Power

3'000 psi Hydro-pack Module - Electrical Motor/Variable-displacement Pump

Reservoir with Sight Gauge

Back-up Accumulator

Cabin Pressurization Control System (ECECS)

1 Electronically Controlled Outflow Valve

1 Digital Controller

1 Pneumatic Safety Valve

2 Negative Pressure Relief Valves

Environmental Control System (ECECS)

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 Sensor Electrical Anti-icing

Exterior Lights

2 Strobe Lights

2 Landing Lights

1 Wing Icing Inspection Light (Left Side)

1 Taxi Light

2 LED Nav Lights

1 LED Tail Light

2 Red Flashing Beacons

Avionics and Instruments

Integrated Honeywell Primus Apex Suite

1 Primary Flight Display (PFD), Flat Penl 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 (1DME), 1 Mode S Transponder (Non-diversity), 1 ADF

2 Primary Flight Display (PFD) Controllers

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

• Cautions and Warnings
• Gear, Trim and Flaps Indication
• Fuel Indications
• ECS/CPCS Indication
• Electrical Systems Indication

1 Multifunction Display (MFD) Controller (incl. Alphanumeric Keyboard)

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 Standby Magnetic Compass

1 Flight Time Recorder ("Hobbs Meter")

1 Digital Clock/Stopwatch

Cabin Compartment

9 Standard Passenger Seats - Quickly Removable, Reclining, 3-point Restraint System

9 Oval Cabin Windows with Internal Pull-down Shades

Painted Composite Interior Panels and Floor 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

1 Hand Microphone

1 Active Noise Reduction (ANR) Headset

Painted Composite Interior Panels, Floor 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

2 Map Reading Lights

Internally Lighted Switch Panels

Internally LIghted Cockpit Controllers

Miscellaneous

Internal/External Markings and Placards

1 Hand Fire Extinguisher

Cabin Door Lock and Keys

Nosewheel Steering Bar

Gust Lock - Control Column

Covers - AOA Transmitter, Pitot Tube, Engine Air Intake, Oil Cooler Intake, ECS Intake, Generator Intake, Engine Exhaust Stacks

Propeller Restraint

Publications/Subscriptions

Pilatus Documents (Free 2-year Revision Service)

Aircraft Flight Manual

Aircraft Maintenance Manual

Aircraft Illustrated Parts Catalog

Aircraft Service Letters

Aircraft Service Bulletins

Pilatus Documents (Other)

Aircraft Conformance Document

Wiring Diagram

Airframe Log Book

Engine Log Book

Propeller Log Book

Pratt & Whitney Canada (Free 2-year Subscription)

Engine Maintenance Manual

Engine Illustrated Parts Catalog

Hartzell (Free Subscription, No Charge for Renewal)

Propeller Operator's Manual

CAMP (Free 1-year Subscription)\

Digital Aircraft Maintenance Tracking

The Trend Group (Free 1-year Subscription)

Engine Trend Monitoring

Certification

US Federal Aviation Regulation (FAR) Part 23, Normal Category

EASA Certification to US FAR Part 23

Standard Warranty

Airframe - 7 years or 5,000 flight hours

Engine - 5 years or 2,500 flight hours (by Pratt & Whitney, Canada)

Vendor items and accessories supplied by Pilatus - 2 years or 2,000 flight hours

Propeller - 2 years or 2,500 flight hours (by Hartzell)

Avionics - 3 years by Honeywell Bendix/King

External paint - 2 years

Interior - 2 years

Training Entitlement

Includes two pilot training courses

Cabin Interior Standard Color Selection

Standard Nine Seat Interior: Fabric Flash 2735LS

Standard Paint Scheme

Base color - AKZO Eclipse "Snow White" painted pursuant to Pilatus Aircraft process specification #VV0600-52

Scheme - Polyurethane Paint Finish as per the Pilatus standard paint scheme