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S-76B | 760359

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Additional Specs

Airframe 7,578 Total Time 30,092 Landings Hinged cockpit and cabin doors, left & right side Improved Pilot and Copilot door lock pins Key locks for cockpit, cabin, and baggage compartment doors Hinged fuel filler caps with key locks Cockpit-controlled electric locks for cabin doors Retractable passenger boarding steps, left & right side Heated glass windshields Windshield wiper and washer system DC Electrical Power System with 2 DC Starter-generators and dual nose mounted batteries AC electrical power system with AC Generator and dual static inverters Manual rotor brake system 5P Bifilar vibration absorber Forward-facing recognition lights in nose windows Forward-facing under-fuselage recognition lights Nose-mounted controllable searchlight Fixed landing lights on left and right main gear struts Pulselite System Tel-Tail Lights on vertical stabilizer lower fairing 3-position strobe light system (Whelen) Top and bottom anti-collision lights
Avionics/Radios Honeywell SPZ-7000 Dual Digital Automatic Flight Control System Honeywell EDZ-705 Electronic Flight Instrument System (EFIS) Standby Self-Contained Attitude Indicator (JET ADI-330C) with battery backup Dual IDC encoding altimeters Pilot-selectable alternate static source switches Dual lighted approach plate holders Dual overhead master switch panels Radio master switches AC/DC Power Management Display (Insco) 5-Function Indicator (Davtron 655-2) Radio Altimeter (Collins ALT-55B) with digital display on EFIS Dual C-14A compass system (Honeywell) Standby vertical-card magnetic compass (Hamilton HI-400) Dual digital clocks (Davtron M-877) Roll checklist (MD-100) Fuel flow indicators Engine Performance Monitoring System (Howell H-598 EPAMS) Honeywell Primus II Communications and Navigation System with Dual Integrated VHF Comm. (RCZ 850) and Dual Radio Management Units (RMU- 850), Dual Integrated Nav. (RNZ-850), and Lightning Sensor (LSZ-850) Dual Mode-S transponders, Dual DME, ADF Third VHF communications radio for clearance delivery Baker Cockpit Audio system with auxiliary volume controls and cabin ICS jack Passenger Briefer and Ramp Hailer system (NAT) Cockpit Voice Recorder Cabin paging and chime system Airborne Telephone System (AirCell) with handset in Cabin Credenza Honeywell Primus 870 Weather Radar Honeywell DataNav III Multi-Function Interface Unit with checklist Universal UNS-1D Flight Management System with GPS/TAS TCAS I (Bendix CAS-66A) with dual indicators Emergency Locator Transmitter (Artex C-406-N HM)
Other Hinged cockpit and cabin doors, left & right side Improved Pilot and Copilot door lock pins Key locks for cockpit, cabin, and baggage compartment doors Hinged fuel filler caps with key locks Cockpit-controlled electric locks for cabin doors Retractable passenger boarding steps, left & right side Heated glass windshields Windshield wiper and washer system DC Electrical Power System with 2 DC Starter-generators and dual nose mounted batteries AC electrical power system with AC Generator and dual static inverters Manual rotor brake system 5P Bifilar vibration absorber Forward-facing recognition lights in nose windows Forward-facing under-fuselage recognition lights Nose-mounted controllable searchlight Fixed landing lights on left and right main gear struts Pulselite System Tel-Tail Lights on vertical stabilizer lower fairing 3-position strobe light system (Whelen) Top and bottom anti-collision lights

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