1992 SIKORSKY S 76C


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    Aircraft Summary


    General

    Year
    1992
    Manufacturer
    SIKORSKY
    Model
    S-76C
    Serial Number
    760407
    Condition
    Used
    Description
    Max Gross Weight: 11700 lbs Empty Weight: 8142 lbs Basic Operating Weight: 8658 lbs Dual Honeywell RCZ-850 Communication, Dual Honeywell RNZ-850 Navigation System, Dual Encoding Altimeters (IDC).

    Airframe

    Total Time
    4630.0
    Airframe Notes
    4630 TT 14235 Total Landings

    Engine 1

    Engine 1 Notes
    Turbomeca Arriel 1S1 Engine #1 SN# 15-15 TT since new: 4136 Total Cycles Since new: 4426 Time Since Overhaul: 1022 Engine #2 SN# 15010 TT Since New: 4161 Total cycles since new: 5478 Time Since Overhaul: 1178 Main Gearbox: TBO-3250 Next Due-7124 Intermediate Gearbox: TBO-4500 Next Due-8374 Tail Gearbox: TBO-4000 Next Due-7496

    Avionics

    Avionics/Radios
    Dual Honeywell RCZ-850 Communication Systems with Honeywell RM-850 Radio Management Units and a clearance delivery unit. Dual Honeywell RNZ-850 Navigation System Dual Honeywell SPZ-7600 Automatic Flight Control Systems Honeywell EDZ-705 Electronic Flight Instrument System (EFIS) Universal UNS-1 (FMS) with GPS Univeral CVR with Rotor Speed Modulation Honeywell P700 Radar Stormscope WX-1000 Weather Mapping System Dual Encoding Altimeters (IDC) Allied Signal Traffic Alert & Collision Avoidance System (TCAS) Dual Honeywell AV-850 Audio Control Systems Honeywell AA-300 Radio Altimeter w/Digital Readouts on ADI's Standby CDI (Aeronetics) and ICS Modifications for Single Pilot IFR Certification Dual Davtron 877 Digital Electronic Clocks Allied Signal Flitefone VI Heads-up Technologies Checklist and Passenger Briefing System (CMS-400) ARTEC ELT-100 HM Emergency Locator Transmitter

    Additional Equipment

    Additional Equipment
    Emergency Flotation System Cocoon Cabin Noise Reduction System Heated Windshields Heated Engine Inlet Kits Parket Hannifin FreonAir Conditioning System Electric Passenger Door Locks Retractable Passenger Boarding Streps (Synergetics Quick-Step) Aircraft Wired for Chadwick-Helmuth Model 8500 Balancer Single Side Refueling Option (from Rigth side) Pulselite Recognition Light System Dual Inverter System Hydraulic Quick Disconnects located in Baggage compartment

    Exterior

    Exterior Notes
    Matterhorn White with Kelly Green and Aristo Blue Stripes. Pin Striped with Metallic Gold.

    Interior

    Interior Notes
    This Aircraft's Six Place Interior was completed by Sikorsky. It features three forward facing and three aft facing seats, with opposing credenzas. The seats are upholstered in green leather with the rest of the interior keeping the green and tan theme. The credenzas are finished in an oak veneer with hardwood edging. All exposed metal in plated coffee-copper bronze. The side walls and ceiling are upholstered in ultrasuede, that were installed new in August 1998. In-Fab-Pro Treatment was applied to all interior materials. A new cabin main carpet was installed in 1997.

    Inspection Status

    Inspection Status
    Maintenance Program: Approved Inspection Program in Accordance with FAR 91.409 (f) (4). (Manufacturer's) Records Maintained on CAMP Andromeda Program and transferable to the standard CAMP format. Fire Blocked in completion to FAR 29.853 standards Single Pilot IFR capable 1500 Hour inspection c/w 9/22/98 @ 3874 hrs.


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