2023 Leonardo AW169

Airframe structure including nose radome, cockpit, main cabin with flat floor and baggage compartment, tail boom, vertical fin,
horizontal stabilizers, fuel tank housing

Airframe

• Attachments for main gearbox and engines
• Upper deck cowlings
• Landing gear attachments
• Heated Pitot tubes (2)
• Forced fan ventilation
• Bleed air heater and defroster with air noise suppression
• Cockpit air adjustable outlets
• Cockpit instrument panel, overhead panel and inter-seat console
• Cockpit Windshields
• Pilot and co-pilot windshield wipers
• Overhead cockpit windows
• Lower cockpit windows
• Lockable pilot doors with emergency exit windows and “storm window” on pilot side
• Lower pilot/co-pilot doors windows
• Lockable plug-in sliding doors (2) for passengers’ cabin access with four emergency exit windows
• Baggage compartment (one door access from left hand side)
• Baggage compartment cargo tiedown fittings Lockable baggage compartment door

Landing Gear

• Wheeled fixed tricycle landing gear with two wheels on nose gear, one wheel with brakes on main landing gears and mooring rings

• Main Rotor System with composite blades
• Tail Rotor System with composite blades
• Rotating M/R and T/R flight controls
• Pilot fixed flight controls (cyclic, collective, anti-torque pedals)
• Co-pilot fixed flight controls (cyclic, collective, anti-torque pedals)
• Force trim system
• Four parallel actuators (4-axis autopilot)

• Two Pratt & Whitney Canada 210A1 High Power turboshaft engines (Phase 7)
• APU mode on left hand side engine
• Two anti-icing fuel systems and two magnetic chip detectors (one per engine)
• Two independent dual-channel FADEC systems (one per engine)
• Engines Control Panel
• Engine bay group (engine mounts, firewalls, cowlings, drains, exhausts)
• Fire detection system
• Fire extinguisher system
• Fire Detection and Extinguisher Control Panel (1)
• Crashworthy fuel cells
• Filler port for gravity refuelling (on left hand side)
• Fuel quantity gauging system

• Main transmission gearbox with two direct drive engine inputs, lubrication system with oil ducts integrated in the casing and oil cooling system
• Three main transmission chip detectors/debris collectors with burning capability
• Intermediate gearbox with sight gauge and magnetic drain plug/chip detector with burning capability
• Tail gearbox with sight gauge and magnetic drain plug/chip detector with burning capability
• Dual independent, redundant hydraulic system
• Two hydraulic Power Control Modules (PCMs)
• Two main transmission driven hydraulic mechanical pumps for controls and wheel brake actuation
• Three Main Rotor dual servo actuators
• One Tail rotor dual servo actuator
• One Tail Rotor actuator shut off valve

• DC primary power generation system: 28 V DC provided by two independent 300 A starter generators
• One heavy duty battery (33 Ah)
• One auxiliary battery (13 Ah)
• 28 V DC External Power Receptacle
• DC Power Distribution System (including bus bars, circuit breaker panels and controls)

Lighting System 

• Internal Lighting
  • Instrument cockpit panel lighting
  • Inter seat cockpit console lighting
  • Overhead cockpit console lighting
  • Cockpit dome light (1)
  • Cockpit utility Light (2)
  • Cockpit storm lights (2)
  • Baggage compartment light
• External Lighting
  • Anti-collision 1 light (1)
  •  Navigation lights (red, white, green)
  • Retractable swivelling
  • Landing / taxiing lights (2)
  • External emergency lights (2)
  • External lights Night Vision Goggles friendly

• Cockpit Display System (CDS)
• Three Rockwell Collins Display Units 10” X 8” colour AMLCD with LED backlight and NVIS compatibility: 2 Primary Flight Displays (PFD) and 1 Multi-Function Display (MFD)
• One Integrated Standby Instrument System (ISIS)
• Two Display Control Panels (DCP)
• Two Cursor Control devices (CCD)
• One Reversionary Control Panel (RCP)
• One Display Dimming Panel
• Two Master Caution Lights (MCL)
• Two Master Warning Lights (MWL)
• Two Avionics Full Duplex Ethernet (AFDX) switches
• Aircraft Monitoring and Management System (AMMS)
• Two Aircraft Monitoring & Management Computers (AMMC)
• One Data Transfer Device (DTD)
• Two touch screen control panels
• 4-Axis Automatic Flight Control System (AFCS)
• Flight Control Computer (FCC)
• One Flight Control System (FCS) Control Panel
• Radio Comm and Navigation System
• Two VHF -AM radios
• Two NAV (VOR/ILS/MB) receivers
• One DME
• One Transponder with Enhanced Surveillance Mode (Mode S)
• First SBAS GNSS (GPS)
• Second SBAS GNSS (GPS)
• TCAS II TSS 4100 Rockwell Collins
• Interphone Communication System
• Two Audio Control Panels (Pilot and Co-pilot stations)
• One Audio Management Unit interfacing external transceivers
• One Passenger Intercom Amplifier
• Primary Flight Instruments
• Two Flux Valves
• Two Air Data and Altitude Heading Reference Systems
• One Radar Altimeter
• Pilot Clock integrated in the display
• Co-Pilot Clock integrated in the display
• One Standby Magnetic Compass

• Cockpit compartment utility finishing interior
• Cockpit panel sun-glare shields
• Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
• 28V DC / 10A cockpit/cabin utility power socket
• Baggage compartment utility finishing interior rear tail separation
• Baggage smoke sensor
• Pilot / copilot headsets
• Cockpit Door Pockets
• Pilot / Co-pilot headset holders
• Cockpit Access Handles

• Standard painting and finishing
• Up to 4 colors from LHD selection
• Painting scheme and finishing from LHD selection
• Registration Marks and Logos
• Tail rotor high visibility painting

• Extension Headset
• Covers and flags for engines, pitot and connectors
• Manuals and parts catalogue
• Tie-down assemblies for main rotor blades
• Tail rotor blades flapping block (1)
• Main rotor blades sock pole (1)
• Main landing gear wheel chocks (2)
• Landing gear handle locking pin (1)
• Tow bar (1)
• Loose equipment bag (1)
• Baggage compartment cargo net

Additional Baseline Equipment

• Steps for cockpit / cabin access
• Rotor brake system
• Second radar altimeter
• One solid state Cockpit and Voice Flight Data Recorder with provision for image recording and 90 days ULB battery (as per AIR OPS)
• One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed)
• Overhead cockpit windows sunshades
• First aid kit (as per AIR OPS)
• One cockpit and one cabin fire extinguisher (as per AIR OPS)
• USB Interseat Console Socket
• Maritime and Corrosion Protection
• AW 169 Enhanced Performance Pack

Additional navigation and fleet management systems

• ADS-B Out (Automatic Dependent Surveillance – Broadcast)
• Health and Usage Monitoring System (HUMS)
• Flight Data Monitoring system (FDM)
• Helicopter Terrain Avoidance and Warning System (HTAWS)
• Synthetic Vision System (SVS)
• RNP Approach with LPV/LP minima
• RNP 0.3 navigation in all phase of flight” FMS capability

Additional equipment

• Cabin Offshore/passenger transport interior
  • Utility Rigid Liners
  • Passenger cabin ambient LED lights, PSU with reading lights and ventilation/AC outlets, emergency lights, emergency exit signs, passenger advisory lights (safety belt chimes) and Passenger Addressing Loudspeakers. I CS Configuration ”008″
  • Comprises 8 passenger headset plugs.
  • Utility soundproofing
  • Kit utility sockets (12 VDC and 28 VDC)
  • Provision for single stretcher layout
  • Lightweight Crashworthy Comfortable Passenger Seat (Qty. 8)
  • Crashworthy seat in the rear cabin bay (Qty.2)
• Cockpit
  • Co-pilot hinged window (storm window)
  • Approach plates chart holders with lights for pilot and co-pilot (USB power outlet included)
  • Tablet cradle for chart holders (loose equipment)
  • Requires approach plate chart holder
  • Camera in the cockpit (Appareo)
• Avionics Equipment
  • Moving map
  • Weather Radar Rockwell Collins RTA-4112 MultiScan – Provision and Removable
• Utility equipment
  • Ice detector, stowage pocket for portable ELT, first-aid kit
  • Increased Gross Weight (4800 kg MTOW)
  • Engine Compressor Washer
  • Cargo hook 1500 kg – Provision and Removable
  • Underbelly Cameras (Qty 2)
  • Engine Air Particle Separators – Provision and Removable
  • Bear Paws – Provision and Removable (not installed provided as loose item)
  • Medevac Layout on Utility Floor (Single Stretcher) (not installed provided as loose item) including:
    • Panel AFT Assy, Rework installed
    • Stretcher Life Jacket installed
    • Extinguisher installed
    • Customized Track installed
    • Loose Safety Equip (provided as loose item)
  • Light Stretcher Cirrus 1000 (not installed provided as loose item)
  • Retainers for Transversal Light Stretcher on utility floor (not installed provided as loose item)
  • Safety and loose equipment for Medevac Layout (not installed provided as loose item) including:
    • Headpad, safety harness, rescue triangle
• External painting
  • Customized painting scheme 2-3 metallic colors from Company paint selection