Turbine Agusta

SINGLE/DUAL PILOT IFR -Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass and ILS data) -Second PFD (co-pilot display) -Second Master Warning Light -Second Master Caution Lights -Co-pilot clock -Dual control -Second display controller -Remote Instrument Controller -Second cursor control device -Left modular radio cabinet with following modules: - 1 VHF Comm - VOR/LOC/GS/MB -Right modular radio cabinet with the following modules: 1. 1 VHF Comm - 1 Mode-C diversity transponder 2. 1 VOR/LOC/GS/MB 3. 1 ADF 4. 1 DME -Emergency communication panel -RMU – Radio Management Units -Radio Altimeter (RT – 300) -Cockpit digital audio panel with remote ICS audio port for ground operation -PAX audio panel for 1 headset FLIGHT/ENGINE INSTRUMENTATION -PFD (Pilot Primary Flight Display 8 x 10 color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data -MFD (Pilot Multifunction Display 8 x 10 color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data -AHRS (Attitude and Heading Reference System) -ADM (Air Data Module) -Flux valve -Display Controller -Cursor Control Device -Reversion Control Panel -Display Dimming Control Panel -Stability Augmentation System (SAS) Controller -Modular Avionics Units (MAUs) - Vehicle Monitoring System – VMS (dual) - Monitor Warning System – MWS (dual) - Aural ---Warning Generator – AWG (single) - Central Maintenance Computer – CMC (single) - 4-axis Digital Automatic Flight Control System – DFACS (dual) with Autotrim function - Flight Data Acquisition Unit – FDAU (single) -Clock (digital) -Magnetic Compass -Free air temperature indicator -Master Warning Light (MWL) -Master Caution Light (MCL) -Engine 1 fire light -Engine 2 fire light -Baggage fire light COMMUNICATION SYSTEM -Microphone and headset (2) -Interphone control (cyclic grip and floor switches) (2) -Stand-alone VHF/AM radio equipment -Intercommunication control panel -Primus Epic HF 1050 long-range system

Exterior
Standard cabin and cockpit liners with soundproofing Pilot/Co-pilot crashworthy seats 12 padded crashworthy utility passenger seats Windshield wipers Steps for cabin access Pilot steps for cockpit access

ADDITIONAL STANDARD EQUIPMENT -Second radar altimeter system -Flight plan management system (FPMS) and GPS module with MCDU -Dual flight director system integrated with MAU -Steps for passenger cabin access and cockpit access -Rotor brake -ELT -Air conditioning and heating -EAPS - Engine Air Particle Separator -Slope Operation Envelope Extension to 10º -Cargo hook and cargo camera provision -Aux Fuel Tank ROTORS & CONTROLS -Fully-articulated main rotor with five composite blades, five elastomeric bearings and five hydraulic dampers -Rotating main rotor flight controls -Three main dual servo actuators -Fully-articulated tail rotor with four composite blades, four elastomeric bearings and four elastomeric dampers -Rotating tail rotor flight controls -One tail rotor dual servo actuator -Force trim system -Pilot fixed flight controls (cyclic, collective, rudder) -Co-pilot fixed flight controls (cyclic, collective, rudder – provisions for) -Engine mechanical back-up control (2) -Dual digital three-axis linear actuators (6) ELECTRICAL SYSTEMS -DC primary power generation: 28-volt DC regulated voltage provided by two independent 300-amp starter generators -DC external power receptacle -One nickel-cadmium battery 40 Ah plus one 13 Ah auxiliary battery -DC starter generator control unit (2) -Manual engine start and ignition system (2) -Navigation lights -Anti-collision lights -Landing light/search light -Utility lights -Pilot cabin dome light -PAX cabin lights (dome or reading lights according to interior configuration) -Tritium-lighted emergency exit signs -Seatbelt/no smoking signs -Baggage compartment light & fire/smoke sensor -AC static inverters system (provisions for) TRANSMISSION / DRIVE SYSTEM & HYDRAULIC SYSTEM -Main transmission with chip detectors/debris collectors with burning capability -Four strut rods for upper deck attachment and anti-torque plate -Intermediate gearbox (sight gage and magnetic drain plug/chip detector) -Tail gearbox (sight gage and magnetic drain plug/chip detector) -Two hydraulic power control modules (PCMs) -Three hydraulic mechanical pumps for controls (2 independent sys) and one electrical pump for controls check on ground (engines off) -Upper-deck cowlings -Provisions for BCS compressor POWER PLANT & FUEL SYSTEM -Two Pratt & Whitney Canada PT6C-67C engines -EEC (Electronic Engine Control) -Overriding clutches -Two magnetic chip detectors -Two integrated and independent engine oil coolers -Separate firewall protection for each engine -Fire detecting system -Cowlings -Engine exhausts and ejectors -Two independent crashworthy fuel cells -Pumps on engines (2) and submerged in fuel tanks (2) -Fuel filter assembly