2008 Sikorsky S-76C++Turbine Helicopter • Rio de Janeiro, Brazil

This 2008 Sikorsky S-76C++ is presented in a proven offshore configuration, located in Rio De Janeiro, Brazil, with registration not specified. The aircraft shows 7,036 total hours on the airframe. It is powered by twin Safran Arriel 2S2 turboshaft engines, with the left engine reported at 6,103 hours and a 4,000-hour TBO. The helicopter is equipped for demanding IFR operations with a comprehensive avionics suite including a four-axis Automatic Flight Control System (AFCS) with Honeywell SPZ-7600 computers, a Garmin GNS 530W GPS, Honeywell Primus 660 weather radar, and a Mode S transponder with ADS-B Out. Safety and utility features are...

Year: 2008

Make: Sikorsky

Series: S-76

Model: S-76C++

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Specifications

Category: Turbine Helicopter

Intended Use: Passenger, Utility

Flight Rules: IFR

Seats: 12

Hours, Logs & Inspections

Total Time: 7,036 hrs

Engine 1 Time: 6,103 hrs (SNEW)

Avionics

GPS

Garmin GNS 530W

Comms

VHF 22A - VHF-AM radios: VHF VHF FM radio:

Honeywell SPZ-7600 - Four-axis AFCS, Two Flight Control Computers

Audio

Dual Audio Control Panels (pilot & co-pilot)

Weather

Honeywell Primus 660 - Weather radar: with panel display

Traffic

Ryan 9900BX - Traffic Advisory System: TAS TCAD

ADSB

Trigg TT21 - Mode S with ADS-B Out

PFD

Honeywell Electronic HSI - Two HSI (5” x 6”), Two ADI (5” x 6”), Integrated Instrument Display System (IIDS): Three panel-mounted displays

Additional Equipment

Air Conditioning

Air conditioning system

Heater

Cabin heater

Baggage Compartment

Baggage compartment liner, Cargo tie-down fittings

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

EVXP - 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

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

Internal Lighting

Instrument panel lighting, Inter-seat console lighting, Overhead cockpit console lighting, Cockpit dome light, Utility and glare shield lighting, Baggage compartment light