2007 Sikorsky S-76C++
2007 Sikorsky S-76C++

Price: Call For Details

Pre-Owned Sikorsky S-76C++ Aircraft, VIP Deluxe Executive Configuration.

Details - 20th January, 2015:
  • Date of Manufacture: October 2007
  • Serial Number: 760684
  • Total Airframe Hours (@ 20 Jan 2015): 1295.00 Hours
  • Total Landings: 3412
Turbomeca ‘Arriel’ 2S2 engines:
Engine Hours No 1: S/N 42147 1295.00 hours
Engine Hours No 2: S/N 42146 1295.00 hours
Engine Cycles: No 1: C1 / 5294 C2 / 5953
Engine Cycles: No 2: C1 / 5298 C2 / 4949
Main Gearbox: S/N A231-00414 1295.00 hours
Intermediate Gearbox: S/N A242-00400 1295.00 hours
Tail Gearbox: S/N A239-00403 1295.00 hours
  • Built to FAA/EASA Specification
General Equipment:
  • Crashworthy designed fuselage
  • Tinted cabin windows
  • Tail boom with fixed horizontal stabilizer
  • Upper deck with fittings for main gearbox, engines, hydraulics and cooling systems
  • Cowlings for main transmission and engines
  • Retractable undercarriage (including emergency down system)
  • Dual engine fire protection system
  • Emergency floatation system
  • Maintenance built-in steps
  • ELT system
  • External boarding steps L.H. & R.H.(retractable)
  • Exterior paint - Ivory upper surfaces, Green lower surfaces and metallic gold stripes
Cockpit:
  • Two hinged doors
  • Completed in black
  • Carpeted
  • Portable fire extinguisher
  • Flight controls (pilot and copilot side)
  • Removable copilot controls
  • Height adjustable pilot and copilot seats
  • Headset hooks
  • Air Comm flight deck heater
Instruments:
  • 2 x Dual EFIS
  • Digital engine instrumentation
  • Central warning panel
  • Airspeed indicator
  • Triple tachometer (rotor and N2)
  • Vertical speed indicator
  • Encoding altimeter
  • Weather radar
  • Clock
  • Door open warning system
  • Pitot static system (electrically heated)
Cabin:
  • Interior paneling with integrated VIP sound proofing
  • Interior ‘Silencer’ noise reduction system
  • Passenger crew call
  • Passenger soft lighting
  • Bleed air heating system automatically controlled
  • Air conditioning system
  • Fresh air vents
  • Illuminated “No Smoke & Fasten Seat belts” sign
  • Digital passenger briefing system
Interior:
  • VIP Configuration - Seating for 6 passengers:
  • 3 x Forward facing seats
  • Fold down center table
  • 3 x Aft facing seats
  • Fold down center table
  • Fully carpeted with leatherette interior & gold plated fixtures
  • Standard Configuration - Seating for 8 passengers:
  • 4 x Forward facing seats
  • 4 x Aft facing seats
  • Fully carpeted with leatherette interior
Power Plant:
  • Two Turbomeca Arriel 2S2 engines compete with:
  • Fire detectors
  • Engine control DECU (with manual reversion)
  • Chip detectors with fuzz burn capability
  • Oil cooling and lubrication system with thermostatic valve
  • Fuel filler flap, lockable
Transmission System:
  • Main gearbox with three stage reduction. Quiet technology gearing.
  • Electrical chip detectors with check capability
  • Oil cooling and lubrication system
  • Free wheel assemblies in engine input drive
  • Hydro/mechanical rotor brake system
  • Intermediate gearbox with splash lubrication, oil level sight glass and electric chip/overheat detector
  • Tail rotor drive shaft
  • Tail gearbox with splash lubrication, oil level sight glass and electric chip/overheat detector
Electrical Installation:
  • Power generation system:
  • Two starter/generators
  • Lead Acid battery (40AH)
  • AC generator
  • External power connector
  • Dual inverter
  • Power distribution system:
  • Two primary busbars
  • Two essential busbars
  • Shedding busbar
  • Battery bus
Electrical:
  • 28 Volt Electrical System with two 200 Amp Starter/Generators
  • 10 KVA AC Generator
  • Dual 375 VA Static Inverters
  • Avionics and EFIS Master Switches
Honeywell EFIS/DAFCS:
  • 4-Tube Honeywell EDZ 756 EFIS with 5" x 6" Indicators Displaying Airspeed
  • Altitude and Vertical Speed
  • Dual Litef AHRS, Dual Penny and Giles Air Data Computers
  • Dual Honeywell Digital SPZ 7600 Automatic Flight Control System, Altitude Alert
Backup/Safety Systems:
  • 2" Backup Airspeed Indicator and Altimeter,
  • ADI-335D Standby Attitude Indicator with Nav1/Nav2 Select,
  • ELT 100HM,
  • CVR/FDR /DVRS
  • Electric Door Locks - Cabin
Rotors and Flight Controls:
  • Fully articulated main rotor head
  • Four metal/composite main rotor blades
  • Four bladed composite tail rotor system
  • Bifilar anti vibration system
  • Basic provision for track and balance built in
Lighting:
  • LED Anti-collision warning light
  • Adjustable instrument lighting
  • Three position LED light (red/green/white)
  • One utility light in cockpit
  • Steerable search light
  • 2 x fixed search lights
  • Illuminated no smoking and fasten seat belt sign
  • Cabin reading lights
  • External strobe lights
Avionics Equipment:
  • Collins Proline II:
  • Dual Collins VHF 22A Comms
  • VIR 32 Navs
  • Single ADF 462 ADF
  • Dual TDR 94D Transponders,
  • DME 42 DME with IND 42A Indicator,
  • ALT 55B Radio Altimeter with Expanded Scale
  • ALI 55A Indicator
Audio:
Dual dB Systems Audio control panels with ICS and VOX plus three maintenance jacks, one in the cabin and two in the baggage compartment. This also includes dual 45° pedestal mounted ICS foot switches, three David Clark Headsets, one six-foot walk-around cord and two 30-foot walk-around cords, Cabin PA/Chime System, and a Passenger Briefing System - PBS 250

Weather Related Systems:
  • Wx Avoidance Radar - Primus 440
  • Windshield Washer System
  • Heated Glass Windshields
  • Engine Inlet Barrier Filter Kit
Radio Equipment Installed:
Single pilot IFR - Cat A certified
Traffic Advisory System Skywatch HP
UNS 1F FMS CDU Universal
UNS GPS-1000 Universal
UNS 1FFMS NCU Universal
Compass gyro Honeywell
JET vert. gyro C14 JET
2 x VHF comm. Controller CTL-22C Rockwell Collins
2 x NAV controller CTL-32 Rockwell Collins
ADF controller CTL-62 Rockwell Collins
ADF Receiver RX462 Rockwell Collins
ATC controller CTL-92 Rockwell Collins
DME indicator IND-42A Rockwell Collins
2 x DME T/R DME 442 Rockwell Collins
2 x VHF Nav. Receiver VIR 432 Rockwell Collins
2 x VHF T/R VHF 422B Rockwell Collins
2 x Transpondeur T/R TDR 90/94D
2 x Autopilot FZ-700 DAFCS Honeywell
2 x Autopilot controller Honeywell
2 x Flight director controller MS-700 Honeywell
Radar altimeter Indicator Honeywell
2 x Air data sensor AZ-649 Honeywell
Altitude selector Honeywell
2 x Pilot EHSI AL-300 Honeywell
Radar indicator E9-600 Honeywell
2 x Symbol generator Honeywell
2 x SG display controller SG-705 Honeywell
B+D TAS computer B&D
CVR/FDR with :- MPFR Curtiss Wright
D2 x Audio control box Keystone STC
Data Nav computer Baker
Data Nav controller Honeywell
AVAD voice generator Honeywell
Moving Map GMX 200 Racal
Satphone VRS EASA Approved system Garmin AirCell
Additional Information:
  • Keystone Anti-rattle door locks
  • Removable cover for collective bearing inspection
  • Dual cabin floor inspection holes LH/RH
  • T/R pedal lub kit
  • Engines on Turbomeca ‘SBH (Privilege)’
  • Airframe “Sikorsky Power by Hour” on all transmissions
Contact:

For more details contact Stephen A. Ayling on: +44 (0) 1276 855-340

The offer for sale of this aircraft is subject to contract and the aircraft may at any time be withdrawn from the market without prior notice.

Specification is subject to verification by the purchaser.

2007 Sikorsky S-76C++2007 Sikorsky S-76C++

Tel: +44 (0) 1276 855-340
Mob: +44 (0) 7785 901-943
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All Aircraft Specifications are Subject to Verification Upon Inspection. Availability Subject to Prior Sale, Lease, or Withdrawal From Market Without Notice.

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