2008 SIKORSKY S-76C++
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Standort des Flugzeugs:Rio De Janeiro, Rio De Janeiro, Brasilien
Verkäuferinformation
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Beschreibung
Spezifikation
Jahr2008
HerstellerSIKORSKY
ModellS-76C++
ZustandGebraucht
FlugregelnIFR
Flugzeit7,036
Angaben FlugzeugzelleAirframe -->
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
Angaben RotorRotor 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 Make/ModelSAFRAN
Engine 1 Time6,103 SNEW
Motor 1 Stunden zwischen Überholung4000
Angaben Motor 1Transmission & 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
Angaben Motor 2Powerplant-->
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
Altimetrisches RadarJa
AutopilotJa
BordwetterradarJa
Avionik/FunkgeräteCockpit 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
KlimaanlageJa
HeizungJa
GepäckraumJa
Zusätzliche AusrüstungSafety & 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
Türartklappbar
Angaben ExteriorExternal 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
AusstattungOffshore
SchallisolierungJa
Angaben InteriorInternal 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