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2008 Sikorsky S-76C++

General Year: 2008 Manufacturer: SIKORSKY Model: S-76C++ Condition: Used FlightRules: IFR Description: Sikorsky S-76C++ in proven offshore configuration, featuring 4-axis AFCS, Arriel 2S2 engines, full HUMS, EGPWS, ADS-B Out, emergency flotation and 12-passenger utility cabin. Available for sale or lease. Airframe Total Time: 7,036 Airframe Notes: Airframe --> Primary airframe structure including: Nose radome Cockpit Main cabin (flat floor) Baggage compartment Tail boom, vertical fin, horizontal stabilizer Fuel tank housing Main gearbox and engine attachment structure Upper deck cowlings Landing gear attachments Wheeled, retractable tricycle landing gear: Single nose wheel Dual main wheels with brakes Mooring rings Doors and windows: Pilot doors with locks and storm windows Lower cockpit windows Hinged passenger door (LH) Sliding passenger door (RH) Push-out windows in passenger doors Baggage compartment: Access doors (LH & RH) Lockable doors Cargo tie-down fittings Cockpit structure and fittings: Instrument panel, overhead panels, inter-seat console Adjustable cockpit air outlets Cockpit windshields Pilot and co-pilot windshield wipers Environmental features: Heated pitot tubes (2) Heated static intakes (2) Forced fan ventilation Bleed air heater and defroster Rotor Rotor Notes: Rotor Systems & Flight Controls--> Main Rotor System with composite blades Tail Rotor System with composite blades Rotating main and tail rotor flight controls Pilot and co-pilot fixed flight controls: Cyclic Collective Anti-torque pedals Force trim system Dual AFCS electrical actuators in pitch, roll, and yaw channels Engine 1 Engine 1 Make/Model: SAFRAN Engine 1 Time: 6,103 SNEW Engine 1 TBO: 4000 Engine 1 Notes: Transmission & Drive System--> Main transmission gearbox: Dual direct-drive engine inputs Integrated lubrication and oil cooling system Two chip detectors with burn capability Intermediate gearbox: Sight gauge Magnetic drain plug / chip detector Tail gearbox: Sight gauge Magnetic drain plug / chip detector Hydraulic-driven systems: Two main transmission-driven hydraulic pumps Controls and wheel brake actuation Servo actuators: Three main rotor dual servo actuators One tail rotor dual servo actuator Tail rotor actuator shut-off valve Hydraulic System--> Dual independent, fully redundant hydraulic systems Two hydraulic modules Two transmission-driven hydraulic mechanical pumps Three main rotor dual servo actuators One tail rotor dual servo actuator Tail rotor actuator shut-off valve Engine 2 Engine 2 Notes: Powerplant--> Two Safran Arriel 2S2 turboshaft engines Engine inlet barrier filters with cockpit condition monitoring Engine chip detectors Engine wash remote connectors Dual independent FADEC systems (one per engine) Engine control quadrant Engine bay group: Mounts Firewalls Cowlings Drains Exhausts Fire protection: Fire detection system Fire extinguishing system Fire detection and extinguisher control panel Fuel System--> Two fuel cells Two gravity refuelling ports (LH & RH) with locking caps Fuel quantity gauging system Electrical System--> 28 V DC primary electrical system Two independent 200 A starter-generators One 44 Ah lead-acid battery (Concorde) 28 V DC external power receptacle DC power distribution system: Bus bars Circuit breaker panels Two 375 VA DC/AC static inverters Emergency power supply (2.5 Ah) for standby ADI Avionics Radar Altimeter: Yes Auto Pilot: Yes Airborne Weather Radar: Yes Avionics/Radios: Cockpit Display System (CDS)--> Two Honeywell Electronic HSI (5” x 6”) Two Honeywell Electronic ADI (5” x 6”) Integrated Instrument Display System (IIDS): Three panel-mounted displays Reversion and scroll controls Remote Data Acquisition Unit (RDAU) Central Warning Panel: Two Master Caution Lights Two Master Warning Lights Cockpit lighting dimming panel Automatic Flight Control System (AFCS) Four-axis AFCS Two Honeywell SPZ-7600 Flight Control Computers Two Mode Selector Control Panels Communication & Navigation--> VHF-AM radios: VHF 22A Garmin GNS 530 / 530W Navigation receivers: VOR/ILS/Marker Beacon (VIR-32) ADF-462 DME-42 Transponder: Mode S with ADS-B Out (Trigg TT21) Radio Altimeter: ALT-1000 with dual displays GPS: Garmin GNS 530W VHF FM radio: Technisonic TFM-500 Satellite tracking & communications: Skytrac ISAT-100 Weather radar: Honeywell Primus 660 with panel display Traffic Advisory System: Ryan 9900BX TAS / TCAD Intercommunication: Dual Audio Control Panels (pilot & co-pilot) Third station intercom Primary & Standby Instruments: Two Air Data Computers Two AHRS Two flux valves Standby instruments: 3” airspeed indicator 3” altimeter Magnetic compass Pilot and co-pilot clocks Additional Equipment A/C: Yes Heater: Yes Baggage Compartment: Yes Additional Equipment: Safety & Emergency Equipment--> Rotor brake system Cockpit Voice & Flight Data Recorder (CVFDR) with ULB Automatically Deployable Emergency Locator Transmitter (ADELT) Emergency flotation system: Automatic and manual deployment External liferafts (2) under cabin doors Emergency exit lighting Fire extinguishers: One cockpit One cabin First aid kit Health Monitoring & Data Systems--> HUMS (EVXP) Flight Data Monitoring (FDM) system Utility & Ground Equipment Engine, pitot, and static covers and flags Main rotor blade tie-down assemblies Wheel chocks (2) Nose and main landing gear locking pins Modifications & STCs (Summary)--> Baggage compartment liner Cabin heater External life rafts Aero Seats passenger seating Water-activated float system Emergency exit lighting EVXP HUMS Garmin GNS 530 GPS & antenna Ryan 9900BX TAS ADS-B Out ISAT Skytrac-100 Technisonic TFM-500 Air conditioning system Ambulance module provision Crash position indicator Additional cockpit and systems enhancements Exterior Door Type: Hinged Exterior Notes: External Lighting--> Anti-collision beacon Navigation lights (red, green, white) Strobe lights on horizontal stabilizer Retractable swiveling landing/taxi light Fixed landing light on RH undercarriage Interior Configuration: Offshore Soundproofing: Yes Interior Notes: Internal Lighting--> Instrument panel lighting Inter-seat console lighting Overhead cockpit console lighting Cockpit dome light Utility and glare shield lighting Baggage compartment light Cockpit--> Crashworthy, adjustable pilot and co-pilot seats Five-point harnesses with inertia reels Chart holders with lighting 28 V DC power outlet Headsets (pilot & co-pilot) Passenger Cabin--> Offshore configuration seating for 12 passengers Four-point passenger harnesses Utility rigid liners Soundproofing Cabin lighting system: PSU reading lights Ventilation outlets Emergency lighting and exit signs Passenger advisory lights and PA speakers (6) Air conditioning system Cabin floor tie-down points Push-out cabin windows Baggage Compartment Utility interior finishing Cargo tie-down fittings Smoke sensor Call for price 
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Name Gustavo Semeraro

City Rio De Janeiro

State Rio De Janeiro

Country Brazil

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