1992 SIKORSKY S 76C
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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