Turbine Agusta

Type: Helicopter

Available

SKU: E990052
• YOM 2018 • 910 Hours Hours / 1910 Landings • Flights above 6400 kg: 87.4 Hours • EASA Compliant • Engines are enrolled on ESP Golden Light • Honeywell Avionics Protection Plan (HAPP) • VVIP Ultra silent soundproofing • Mast Vibration Absorber (MVA) • Air conditioning
Maximum Range
Passengers
Max Speed
AIRFRAME • (EASA IFR SINGLE PILOT / FAA IFR) • Aluminum alloy fuselage • Acrylic windshields • Overhead cockpit transparent windows • Lower cockpit transparent windows • Cockpit ram air adjustable outlets • Forced fan ventilation • Bleed air heater & defroster with air noise suppressions • 2 x Heated Pitot tubes with 2 x Pitot heat failure warning • 2 x Heated static intakes • One cockpit & one passenger cabin fire extinguisher • 2 x Pilot doors with push-out emergency exit window (with “storm window” on pilot side) (High Visibility Cockpit Doors) • 2 x Plug-in sliding doors for passenger cabin access with four locking latches • Passenger doors stop in fully open position • 6 x cabin push-out emergency exit windows (2 on each passenger cabin door) • Baggage compartment with two lockable baggage compartment doors (Left & Right) • Baggage compartment cargo tie-down fittings • Wheeled retractable tricycle landing gear (two wheels on nose gear & brakes on main landing gear) • Structural provisions for nose landing gear doors • Landing gear mooring • Upper deck mooring provisions • Hoisting & jacking fittings • Tail boom & vertical fin • Horizontal stabilizers with composite “winglets” • Pilot & co-pilot windshield wipers • Maintenance steps for access to upper deck on both sides • Upper deck cowlings (one front forward sliding, 2 x side opening for engine access) • Steps for cockpit access • 2 x Anti-vibration masses under cabin floor
• 2 x (Pilot & Co-pilot Primary Flight Display) 8' x 10' (external) color Active-Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data (Phase 7, hardware 3 or latest v) • 2 x MFD (Pilot & Co-pilot Multifunction Display) 8' x 10' (external) color Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic Sys for visualization of flight and navigation data (Phase 7, hardware 3 or latest v) • 1 x Electronic Standby Instrument System (ESIS) (attitude, airspeed • 2 x Attitude & Heading Reference Systems (AHRS) • 2 x Air Data Modules (ADM) • 2 x Flux valves • 2 x Display Controllers (DC) • 2 x Cursor Control Devices (CCD) • 1 x Reversion Control Panel (RCP) • 1 x Display Dimming Control Panel (DCP) • 1 x Stability Augmentation System (SAS) control panel • 2 x Remote Instrument Controllers (RIC) • 2 x Modular Avionic Units (MAU) incorp the following majör 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 & Co-pilot headsets • Pilot & Co-pilot interphone control (cyclic grip and floor switches) • Emergency Locator Transmitter (ELT 406 MHz & 121.5 MHz) • 1 x Flight guidance controller • Left Modular Radio Cabinet (MRC) with the following modules: 1 x VHF Comm. & 1 x VOR / LOC / GS / MB • Right Modular Radio Cabinet (MRC) with the following modules: 1 x VHF Comm. / 1 x DME / 1 x ADF 1 x VOR / LOC / GS / MB 1 x Mode S diversity transponder with Extended Squitter (ADS-B out 1090 MHz) • 2 x Pedestal mounted Multifunction Control Display Units (MCDU) • 1st Radar Altimeter RT-300 & 2nd Radar Altimeter RT -300 • 2 x Honeywell GPS modules (WAAS / SBAS - Wide Area Augmentation System / Satellite Based Augmentation System) with Flight Plan Management System (FPMS) • Pilot & co-pilot digital audio panels with remote ICS audio port for ground operation • Pilot & Co-pilot digital clocks • 1 x Magnetic compass & 1 x Outside air temperature indicator • 2 x Master Warning Lights (MWL) & 2 x Master Caution Lights (MCL) • Engine 1 & Engine 2 fire lights • Baggage compartment smoke detector light • 2 x Electrical power connection for CVR / FDR • Cockpit Voice Recorder (CVR) & Flight Data Recorder (FDR) with Underwater Locator Beacon (ULB) • Health & Usage Monitoring System (HUMS COCKPIT • Honeywell Radio Altimeter & 2nd radar altimeter RT-300 • Primus 660 Weather Radar (provisions & removable) • Traffic Collision Avoidance System (TCAS ) • Enhanced Ground Proximity Warning Sys(EGPWS) (provisions & removable) • Artex Emergency Locator Transmitter (ELT) • Penny & Giles Flight Recorder & Cockpit Control Unit • Digital Clock & Magnetic Compass • 2 x Pedestal mounted Multifunction Control Display Units (MCDU) • Emergency Locator Transmitter (ELT 406 MHz & 121.5 MHz) • 1 x Flight guidance controller • 2 x Honeywell GPS modules (WAAS / SBAS - Wide Area Augmentation Sys/Satellite Based Augmentation Sys) with Flight Plan Mngmnt Sys (FPMS) • Pilot & co-pilot digital audio panels with remote Intercom System (ICS) audio port for ground operation • Pilot & Co-pilot digital clocks • 1 x Magnetic compass & 1 x Outside air temperature indicator • 2 x Master Warning Lights (MWL) & 2 x Master Caution Lights (MCL) • Engine 1 & Engine 2 fire lights • Baggage compartment smoke detector light • CVR & FDR with Underwater Locator Beacon (ULB) • 2 x Electrical power connection for CVR / FDR ROTORS • Fully articulated Main Rotor with 5 x composite blades, 5 x elastomeric bearings & 5 x hydraulic dampers • Rotating Main Rotor flight controls • Main rotor hub beanie • 3 x Main dual servo actuators - Improved version • Fully articulated Tail Rotor with 4 x composite blades, 4 x elastomeric bearings & 4 x elastomeric dampers • Rotating Tail Rotor flight controls / 1 x dual servo actuator • Force trim system • Pilot & 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)


Exterior
• DELUXE Cabin Interior (FIVE STAR Cabin Interior - VIP 37 Plus) (FAA STC), substantially light and different design than the ones delivered so far, including: • 3 VVIP / crashworthy armchairs leather covered-forward looking, (with inertial reels & safety belt, sliding inflight direction, reclining backrest) • Four crashworthy seats leather covered (with inertial reels & 4 safety belts and under-storage compartment). • 2 lateral covered armrests cabinets with metal cup holder, ICS ctrl & multipurpose holder • Coats hooks (Qty 4) • 2 additional standard crashworthy seats leather covered, including dedicated carpeting • Headsets Bose ANR type with Bluetooth capable (Qty 2) • Multipurpose Cubby with sliding doors • Night curtain cabin separator, 50 cm length from the top, bottom side to cover the gaps on the seats • Passenger cabin sliding doors • Nose landing gear doors • Customized VIP cabin finishing • Decoration trim • Customized leather covering for pilot/co-pilot seats • Cockpit upper windows • Co-pilot hinged window • Standard passenger carpet in lieu of High thickness passenger carpet • Environmental Control System with control panel • Air conditioning • VVIP Ultra silent soundproofing (in lieu of VIP soundproofing) • Passenger Address (PA) sys (including loudspeakers & safety belts lights) • Intercom System (ICS) in the cabin for all passengers (ICS phone to speak with pilots, no push button to talk) • Passenger cabin thermo-acoustic double layer tinted windows • Ripple dampers • Main Gear Box - Premium grade • Cyclic and Collective leather gators (same color as cabin interior) • 2 metal finished cabin vertical handles on doorposts • Alternate current power outlet (Qty 3, two 115V power outlets in cabin & one 28V power outlet in cockpit) • Lighter 28V DC outlet in the cockpit • Customized painting scheme, metallic colors • Mast Vibration Absorber (MVA) • Pilot headset hooks (Qty 2) • Approach plates chart holders with lights for pilot & co-pilot • 4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover mode (HOV) • Main battery 44 Ah in lieu of 40 Ah • Auxiliary heavy-duty battery 28 Ah in lieu of 13 Ah • GPS 2nd unit (installation) • Life vest (Qty 11) • Maritime Protection • FAA STC Number : SR03212NY • EASA STC Number : EASA.R.S.01486

• Inlet Barrier Filter provision • Strobe Lights • Electrically operated step (Left & Right) with boarding lights • Pilot & Copilot Glass windshields • Honeywell Epic Primus Software (Phase 7) • TCAS II, ADS-B Out, 1090 MHz • Main Rotor Tracking Signal Connector in Cockpit • Active Vibration Control System (AVCS) - complete installation • Pilot / Co-pilot adjustable seats with sheep skin covers • Enhanced Ground Proximity Warning System (provisions & removable) • Weather Radar Primus 660 Honeywell • Auxiliary transversal fuel tanks 132 US gallon (provisions & removable) • Emergency floats provision, including switches & control panel (Aerozure Production) • Emergency floats Kevlar covers (Aerozure Production) • Increased gross weight 7,000 Kg • Tail Fin Camera • • Kevlar (panel) covers available (removable floats not available)
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Type Helicopter
Year 2018
Location Europe, Turkey
TT 910
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