N711DS - 1997 SIKORSKY S 76C+


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    Aircraft Summary


    General

    Year
    1997
    Manufacturer
    SIKORSKY
    Model
    S-76C+
    Serial Number
    760473
    Registration #
    N711DS
    Condition
    Used
    Description
    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 Dual Audio Systems (AV-850)

    Airframe

    Total Time
    4191.8
    Airframe Notes
    10,627 Landings Executive Transport, Six/Eight Cabin Passengers

    Engine 1

    Engine 1 Notes
    No. 1 Engine Serial No.: 20505TEC TTE(1): 10,848 Hours since new TSO: 1,598.3 On SAFRAN SBH

    Engine 2

    Engine 2 Notes
    No. 2 Engine Serial No.: 20092 TTE(2): 5,848.4 Hours since new TSO: 2,357.6 On SAFRAN SBH

    Avionics

    Avionics/Radios
    • Honeywell SPZ-7600 Dual Digital Automatic Flight Control System • Honeywell EDZ-756 Electronic Flight Instrument System (EFIS) • Single-Pilot IFR capability with ADI-335D standby attitude indicator • Dual lighted approach plate holders • Dual overhead master switch panels • Radio master switches • AC/DC Power Management Display (Insco) • 5-Function Indicator (Davtron) • Ice Detector system • Radio Altimeter (Honeywell AA-300) with digital display on EFIS • Dual C-14A compass system (Honeywell) • Standby vertical-card magnetic compass (Hamilton HI-400) • Dual Attitude Heading Reference System (Litef LCR-92 AHRS) • Dual digital clocks (Davtron M-877) • Fuel flow indicators and totalizer (Foxboro) • Dual Mode-S transponders • Dual DME • Dual ADF • WAAS Certified • Third VHF comm. radio for clearance delivery • Cockpit Voice Recorder (Universal CVR-30A) • Passenger Briefing System (PBS-250) and loudhailer • Cabin paging and chime system • Honeywell Primus 700 Weather Radar • Honeywell DataNav V Multi-Function Interface Unit with Checklist • Honeywell LSZ-850 Lightning Sensor • Universal UNS-1FW Flight Management System with GPS/TAS/WAAS • TCAS I (Bendix CAS-66A) with dual indicators • Emergency Locator Transmitter (Artex C-406-N HM)

    Additional Equipment

    Additional Equipment
    Airframe & Systems: • Hinged cabin doors, left & right side • Key locks for cockpit, cabin, and baggage compartment doors • Hinged fuel filler caps with key locks • Cockpit-controlled electric door locks for cabin doors • Retractable passenger boarding steps, left & right side • Heated glass windshields • Windshield wiper and washer system • Manual rotor brake system • Engine Inlet Snow Protection Kit • 5P Bifilar vibration absorber • Baggage floor liner • Forward-facing recognition lights in nose windows • Nose-mounted controllable searchlight • Fixed landing lights on left and right main gear struts • Pulselite System • Tel-Tail Lights on vertical stabilizer • 3-position light system (LED) • Top and bottom anti-collision lights LED Mission Equipment: • Emergency Flotation System Loose Equipment: • Main rotor blade tie-downs (set) • Exterior covers and plugs (set) • Pitot-tube covers (2) • Landing gear pins (3) • Door lock keys

    Interior

    Interior Notes
    • Executive Cocoon cabin interior and soundproofing system • Cockpit-cabin divider bulkhead with sliding windows • 3-4 Place forward-facing executive divan with fold-down table and armrests • 2 Aft-facing single executive seats or rear facing four place divan • Cabin refreshment credenza with hot liquid containers, ice drawer, and storage w/six place interior • Cabin and Cockpit Climate Control System (C4) • Magazine racks on cabin doors • Storage compartments beneath divan for fire extinguisher, first aid kit, life vests • Cabin control panels on side rails for lighting, stereo speakers, and headsets

    Inspection Status

    Inspection Status
    12-Month inspection: June 2025
    Airworthy
    Yes


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