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Description

Western Aviation is proud to present this 2005 Sikorsky S76C+ one of 4 Sikorsky's available!
Call Now for complete details of these Sikorsky's!
Airframe
Nose and tail avionics compartments, Glass windshields, Cabin bleed air heating and ram air ventilation system, Bleed air windshield defogging system with combines flight deck heater (Air Comm), Cabin & cockpit air conditioning system. Dual windshield wiper system, Pilot and Copilot high back seats with 5-point restraint harness and height adjustable, Two ejectable, hinged cockpit doors, Two cabin doors, LH & RH hinged equipped with electric and manual door locks. Fully retractable tricycle landing gear with pivoting nose gear and main wheel brakes, Pneumatic emergency landing gear extension system, 204 cubic foot cabin fitted with a hard utility interior, Cabin fitted with 12 seats with upper body harness restraint system, Separate 38 cubic foot baggage compartment with dual locks, Emergency floatation system with manual & automatic activation, Two internal liferafts with 10 man normal and 15 man overload capacity, Cabin first aid kit, Portable fire extinguisher, Cabin pop-out emergency egress windows, Cargo hook provisions.
Engine(s)
Propulsion: Dual Turbomeca Arriel 2S1
Dual fuel tanks with gravity fuel fillers plus auxiliary fuel tank provision. Low level fuel warning system. Engine fire detection and extinguishing systems
Avionics/Radios
Dual independent 3,000 PSI hydraulic systems with quick disconnects for ground servicing
Dual independent flight control servo systems
Dual Digital Automatic Flight Control System (DDAFCS) (Honeywell SPZ-7600 four axis fully coupled).
Electronic Flight Instrumentation System (EFIS) with four displays which display aircraft heading, attitude, airspeed, altitude, vertical speed and flight director information.
Integrated Instrument Display System (IIDS) which consists of three identical and fully independent displays which provide triple redundancy for engine instrumentation and crew advisory system (EICAS). The IIDS displays N1, T%, engine oil temperature/pressure, transmission temperature/pressure, dual fuel quantity, dual hydraulic oil pressure, fuel flow rate, dual torque, triple tachometer and caution/advisory panel.
Dual low glare-shield mounted master warning panels
Landing gear warning indication system
Dual digital electric clocks
Integrated GPS, NAV & Com with moving map display (GNS-530) which can display EGPWS/TAWS & ACAS/TCAS information.
VOR/ILS system supplies bearing, approach and landing navigation guidance data:
VOR/ILS #1 – VIR-32
VOR/ILS #2 – GNS-530
Automatic Direction Finder (ADF): ADF #1 – ADF 462
Distance Measuring Equiment (DME): DME #1 – DM-42
Radio Alt. System (RAD ALT) w/ single expanded scale analog indicator: RAD ALT #1 – ALT-55B
Enhanced Ground Proximity Warning System (EGPWS) (MK XXII)
Weather Radar (Primus 660)
Dual Attitude Heading Reference System (AHRS) (LCR-92S)
Single Mode C transponder (TDR-90)
Airborne Collision Avoidance System (TCAD) (TAS-620)
Dual Air Data Computer system (ADC) with instantaneous vertical speed trend vector
Standby attitude indicator with emergency power supply
Backup airspeed indicator
Backup barometric altimeter
Standby magnetic compass
Dual pitot static systems with heated ports
Multi-purpose digital voice & flight recorder (MPFR)
Health/Vibration monitoring system (VXP)
Underwater Locator Beacon (ULB)
Helicopter Flight Data Monitoring System (FDM)
Pilot & co-pilot audio select panels (DB 380) with additional maintenance jacks in the cabin and baggage compartment.
Very High Frequency (VHF) system supplies air to air and air to ground communication:
VHF #1 – VHF 22A, VHF #2 – GNS 530
Flight Following System (ISAT 100)
VHF/FM Maritime Transceiver (TFM 550)
Cabin audio select panel (DB 380)
Passenger address system (PBS-250)
Cabin paging and chime system with six overhead speakers
Passenger briefing system (PBS-250)
Emergency Locator Transmitter (ELT) (Artex 406)
Additional Equipment
Lighting
Two cabin emergency lights with battery backup, Three strobe/position light system, Fixed landing light on RH hand landing gear, Controllable landing light, Dual baggage compartment lights, Helicopter Emergency Egress Lighting (EXIS), Non-smoking/fasten seatbelt sign in cabin

Rotor System
Four-blade articulated main rotor with one-piece aluminum hub and elastomeric bearings
Main rotor blades with titanium spars, fiberglass skins, honeycomb cores and high visibility paint
Manual rotor brake system
Four-blade flex beam tail rotor drive system with tail intermediate gearboxes

Electrical
Dual 200 amp DC starter-generators
Generator hot warning system
Dual 375 VA static inverter
DC external power receptacle with overvoltage protection
Pilot & Co-pilot overhead master switch panels
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