Standard Avionics Package
- 1ste PFD (Pilot Primary Flight Display 8” x 10” colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 2nd PFD (Co-pilot Primary Flight Display 8” x 10” colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 1st MFD (Pilot Multifunction Display 8” x 10” colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 2nd MFD (Co-Pilot Multifunction Display 8” x 10” colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
- 1 Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
- 2 Attitude and Heading Reference Systems (AHRS)
- 2 Air Data Modules (ADM)
- 2 Flux Valves
- 2 Display Controllers (DC)
- 2 Cursor Control Devices (CCD)
- 1 Reversion Control Panel (RCP)
- 1 Display Dimming Control Panel (DCP)
- 1 Stability Augmentation System (SAS) control panel 2 Remote Instrument Controllers (RIC)
- 2 Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions:
• Vehicle Monitoring System (VMS) dual
• Monitor Warning System (MWS) dual
• Aural Warning Generator (AWG) single
• Central Maintenance Computer (CMC) single
• 4-axis dual Digital Automatic Flight Control System (DAFCS) Basic Provision for CVR/FDR data interface (single)
• Flight Director System (dual)

- Pilot and co-pilot headsets
- Pilot and co-pilot interphone control (cyclic grip and floor switches)

- Left Modular Radio Cabinet (MRC) with the following modules:
- 1 VHF Comm.
- 1 VOR/LOC/GS/MB

- Right Modular Radio Cabinet (MRC) with the following modules:
• 1 VHF Comm
• 1 Mode S diversity transponder 1 VOR/LOC/GS/MB
• 1 ADF
• 1 DME

- 2 pedestal mounted Multi Control Function Display Units (MCDU)
- 1st radar altimeter RT-300
- 2nd radar altimeter RT-300
- Emergency Locator Transmitter (ELT)
- 1 Flight guidance controller
- Honeywell GPS module with Flight Plan Management System (FPMS)
- Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
- Pilot clock (digital)
- Co-pilot clock (digital) 1 Magnetic compass
- 1 Outside air temperature indicator 2 Master Warning Lights (MWL)
- 2 Master Caution Lights (MCL) Engine 1 fire light
- Engine 2 fire light
- Baggage compartment smoke detector
- Dual electrical power connection for CVR/FDR (FAA requirement compliant)
- Cockpit voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)

EQUIPMENT HIGHLIGHTS
- BLEED AIR HEATER AND DEFROSTER WITH AIR NOISE SUPPRESSIONS
- FIRE EXTINGUISHER
- TWO PLUG-IN SLIDING DOORS FOR PASSENGER CABIN ACCESS WITH 4
- LOCKING LATCHES
- PASSENGER DOORS STOP IN FULLY OPEN POSITION
- WHEELED RETRACTABLE TRICYCLE LANDING GEAR (2 WHEELS ON NOSE GEAR AND BRAKES ON MAIN LANDING GEAR)
- HOISTING AND JACKING FITTINGS
- 2 ANTI-VIBRATION MASSES UNDER CABIN FLOOR

POWER PLANT AND FUEL SYSTEM HIGHLIGHTS
- 2 PRATT & WHITNEY CANADA PT6C-67C TURBOSHAFT ENGINES
- 2 INDEPENDENT FADEC SYSTEMS WITH AUTOSTART AND ENGINE CONTROL
- FUNCTIONS FOR NORMAL, EMERGENCY AND TRAINING OPERATIONS
- 2 INTEGRATED AND INDEPENDENT ENGINE OIL COOLERS
- 2 MAGNETIC CHIP DETECTORS
- SEPARATION FIREWALL PROTECTION FOR EACH ENGINE
- FIRE DETECTION SYSTEM
- FIRE EXTINGUISHER SYSTEM (2 BOTTLES)

ROTORS AND CONTROLS HIGHLIGHTS
- Fully articulated Main Rotor (M/R) with 5 composite blades, 5 elastomeric bearings and 5 hydraulic dampers
- Rotating M/R flight controls
- Main rotor hub beanie
- 3 Main dual servo actuators
- Fully articulated Tail Rotor (T/R) with 4 composite blades, 4 elastomeric bearings and 4 elastomeric dampers
- Rotating T/R flight controls
- 1 T/R dual servo actuator
- Force trim system
- Pilot fixed flight controls (cyclic, collective, anti-torque pedals)
- Co-pilot fixed flight controls (cyclic, collective, anti-torque pedals) Dual digital 3-axis linear actuators
- Rotor brake
- Provision for main rotor tracking (magnetic pick-up)

Miscellaneous/Ground Equipment
- Covers and flags: 2 engine exhaust pipes, 2 engine air inlets and 2 pitot tubes, 1 battery connector warning flag
- 5 Tie-down assemblies for main rotor blades
- 1 Tail rotor blades flapping block
- 1 Main rotor blades sock pole
- 2 Main landing gear wheel chocks
- 1 Nose landing gear centre pin and 1 landing gear handle locking pin
- 1 Jacking dome assy

Offshore configuration

Offshore common package:
- ADELT (Automatic Deployable ELT w/ NAV interface w/ GPS) in lieu of std ELT Emergency floats (AFDS)
- Helicopter Emergency Exit Lighting System (HEELS)
- 2 Life Rafts up to 17 passengers
- Weather Radar – Primus 660 – Honeywell
- Additional anti-collision lights under fuselage
- Two strobe lights on tail plane

Offshore additional package:
- Co-pilot storm hinged window
- Central approach chart holder with lights
- Separate 4 points seat belts
- Auxiliary heavy-duty battery 27 Ah
- Enhanced Ground Proximity Warning System (EGPWS)
- Flight Operation Quality Assurance Equipment (FOQA/HOMP)
- Health & Usage Monitoring System (HUMS)
- TCAS I – KTA 970 – Honeywell Bendix / King
- Baggage load capacity increase to 300 kg
- Cargo net in baggage compartment
- Auxiliary transversal fuel tanks USGall 132 provision
- Air conditioning
- Main rotor blades high visibility painting
- Closed circuit refuelling plus ISO 45 pressure adaptor
- Rescue hoist single (Goodrich) provision
- Cargo hook (2.200 kg / 4.850 lbs) provision
- VHF/FM
- SATCOM IRIDIUM
- NPX 138 NAT
- ISAT 100 Skytrack
- Lighting detector system
- LSZ 860 Honeywell
- Direction Finder DF 935-2 Chelton with multi-beacon tracking and OPTI or On Top Position Indicator)
- Rescue hoist single (Goodrich) – removable
- Cargo hook (2.200 kg/4.850 lbs) – removable
- Medical evacuation (MEDEVAC) – 4 longitudinal Stretcher:
• One piece open frame to support the stretcher
• 4 stretchers

- Pilot and co-pilot crashworthy seats (with inertial reels and safety belts) Cockpit dome/storm light
- 2 Cockpit utility lights
- 28 V DC cockpit/cabin power outlet
- Cockpit panel sun-glare shields
- Overhead cockpit windows sunshades
- Floor provisions for 15-seat configuration
- Fluorescent lighted emergency exit signs
- Cockpit map and data case in central console
- 2 Flashlights for pilot and co-pilot
- Map and data cases in pilot and co-pilot doors
- ICS panel with plug for one headset
- Air ventilation system
- First Aid kit


Offshore configuration

Offshore cabin basic settlement
- Silent soundproofing
- Standard roof liners with dome lights
- Composite liners painted
- ICS panel, one position in passenger cabin (LH side)
- Passenger Address System including loudspeakers on std ICS
- Fixed steps for passenger cabin access
- Rubber floor carpet

12 padded crashworthy comfortable seats fabric or leatherette covered with inertial reels and safety belts disposed on 3 rows

Basic aircraft
- Aluminium alloy fuselage
- Acrylic windshields
- Overhead cockpit windows Cockpit ram air adjustable outlets Forced fan ventilation
- Bleed air heater and defroster with air noise suppressions
- 2 Heated Pitot tubes with 2 pitot heat failure warning
- 2 Heated static intakes
- 1 Cockpit and 1 Passenger cabin fire extinguisher
- 2 Pilot doors with push-out emergency exit window (with ‘storm window on pilot side)
- 2 Plug-in sliding doors for passenger cabin access with 4 locking latches
- Passenger doors stop in fully open position
- 6 Cabin push-out emergency exit windows (2 on each passenger cabin door)
- Baggage compartment with 2 lockable baggage compartment doors (LH and RH)
- Baggage compartment cargo tie-down fittings
- Wheeled retractable tricycle landing gear (2 wheels on nose gear and brakes on main landing gear)
- Structural provisions for nose landing gear doors
- Landing gear mooring
- Upper deck mooring provisions
- Hoisting and jacking fittings
- Tail boom and vertical fin
- Stabilizers with composite ‘winglets’
- Pilot and co-pilot windshield wipers
- Maintenance steps for access to upper deck on both sides
- Upper deck cowlings (1 front forward sliding, 2 side opening for engine access)
- Steps for cockpit access
- 2 Anti-vibration masses under cabin floor

Power Plant and fuel system
- 2 Independent FADEC systems with autostart and engine control functions for normal, emergency and training operations
- 2 Magnetic chip detectors
- 2 Integrated and independent engine oil coolers Separation firewall protection for each engine Fire detection system
- Fire extinguisher system (2 bottles)
- Steel engine exhausts and ejectors
- 2 independent crashworthy fuel cells
- 2 Supply pumps on engines
- 2 Submerged booster pumps in fuel tank
- 2 Fuel filter assemblies
- 2 Engine back-up controls, mechanical and electrical 2 Manual engine start and ignition systems

Transmission drive system and hydraulic system
- Main transmission with 2 direct drive engine inputs
- 3 Main transmission chip detectors/debris collectors with burning capability
- 2 Freewheel units
- 4 Strut rods for upper deck attachment and one anti-torque plate
- Intermediate gearbox with sight gauge and magnetic drain - plug/chip detector
- Tail gearbox with sight gauge and magnetic drain plug/chip detector
- Dual independent, redundant hydraulic systems
- 2 Hydraulic Power Control Modules (PCM)
- 3 Main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
- 1 Electrical pump for control checks on ground (engines off)
- Air conditioning compressor quill

Electrical Systems
- DC primary power generation: 28 V DC regulated voltage provided by 2 independent 300 A starter generators
- DC external power receptacle
- 2 Nickel-cadmium batteries: 1 44 Ah main battery plus 1 13 Ah auxiliary battery
- 2 DC starter generator control units
- 3 Navigation lights
- Anticollision light
- 2 External emergency landing lights on the sponsons
- 2 Fixed landing/taxing lights on the sponsons
- Retractable/rotating landing light
- 3 Baggage compartment lights and smoke sensor

- P&W PT6C-67C
- 2919 HOURS REMAINING
- *SUBJECT TO VERIFICATION BY THE BUYER*

- P&W PT6C-67C
- 2956 HOURS REMAINING
- *SUBJECT TO VERIFICATION BY THE BUYER*

- LANDINGS SINCE NEW 16180
- MGB 2311
- 2 CREW/12 PAX

*SUBJECT TO VERIFICATION BY THE BUYER*