Sikorsky S-76C+

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

Aircraft Information

Condition: 
Pre-Owned
Year: 
1998
Hours: 
4734
Serial Number: 
760492
Registration Number: 
C-FHMQ
Price: 
Call For Price
Aircraft Description: 

• VVIP Helicopter
• Collins ProLine II Avionics
• Engines & Gearboxes on PBH Programs

Airframe Information
Airframe: 

TTAF: 4734

Maximum Gross Weight: 11,700 pounds
Equipped Weight Empty/CG: 8201.0 Lbs @ STA 206.1
Basic Mission Configuration: VVIP Transportation, Six Cabin Seats

Engine(s) Information
Engine(s): 

Two (2) Turbomeca Arriel 2S1, Turboshaft
Engines & Gearboxes on PBH Programs

Engine 1: S/N 20661
3431.25 HSN, 125 SOH

Engine 2: S/N 20719
3221.31 HSN, 125 SOH

Avionics / Radios Information
Avionics / Radios: 

Collins ProLine II Avionics with dual Collins VHF-22A Communications radios
Dual VIR-32 FM Immunity Navigation radios
Single ADF-462
DME-42 with 2 IND-42A indicators
Dual Mode-S TDR-94D Transponders (with diversity)
ALT-55B Radio Altimeter with ALI-55 indicator
Altitude Alerter
Dual Honeywell AA 300 Radio Altimeter systems with expanded scale indicators
Universal UNS-1D Flight Management System (FMS)
Dual Penny and Giles Air Data Computers
3" Backup Airspeed Indicator and Altimeter
3" Standby Attitude Indicator
Weather Avoidance Radar (Bendix RDR 2100) with Checklist Controller
BF Goodrich Lightning Detector interfaced with the radar display
TCAS I System (CAS 66A) with TA Display, Dual TID 66A
Health and Usage Monitoring System I (HUMS I) with CVR and FDR
Skyforce Observer digital map display

Interior / Exterior Information
Interior: 

Cabin Amenities
Cocoon interior panel system with added bay-blankets for enhanced sound suppression
Ultra-suede covering on cabin sidewalls and ceiling. Carpeting throughout the interior
Cabin/Cockpit Divider Bulkhead with a full width window above the seat backs
Silk-screened information placards, membrane switches, decorative satin plating
Illuminated No Smoking/Fasten Seat Belt signs
Four cabin dome lights with cockpit control and eight cabin reading lights
Ceiling-mounted hidden lighted mirror above left rear cabin seat
Cabin door threshold lighting, left and right
Colorless cabin window tint
Magazine racks on left and right cabin doors
Cabin coat hooks, cup holders, and ash trays

Cabin Seating
Aft-facing 3-place divan with a refreshment credenza between positions 2 and 3
Two hot-liquid containers in the aft-facing credenza
Storage for two food serving trays in the center compartment behind the aft-facing divan
Forward-facing 3-place divan a with refreshment credenza between positions 1 and 2
Custom swing-out writing table with leather-insert built into the forward-facing credenza
Top-access storage for life vests in the forward-facing seat bottom extension
Leather upholstery with fabric seat inserts for cabin seat bottoms and seat backs

Aircraft Maintenance
Aircraft Maintenance: 

Please See PDF Information Sheet Above To View Major Component Status

Additional Information
Additional Information: 

Configuration Features

Equipped with these standard features:
Two Turbomeca Arriel 2S1 turboshaft engines
Four blade fully articulated Main Rotor system with a high-visibility paint scheme
Bifilar vibration absorber (3P) at the Main Rotor Head
Four blade Tail Rotor system
Hinged cockpit doors for Pilot (right) and Copilot (left)
Hinged cabin doors, left and right, with key locks
Fully retractable tricycle landing gear with independent main wheel brakes
Pneumatic emergency landing gear extension system
Glass windshields with dual washers and wipers
Two integral fuel tanks with 281 U.S. Gallon total capacity; gravity filled
38 cubic foot baggage compartment with left and right doors aft of the main cabin
Dual pilot flight controls with redundant dual hydraulic servo systems
Dual Honeywell SPZ-7600 Digital Automatic Flight Control System
Dual 4-tube Electronic Flight Instrument System (Honeywell EDZ-756 EFIS)
Integrated Instrument Display System (Parker-Gull IIDS)
Attitude Heading Reference System (Litef AHRS)
Dual pilot instruments, dual Internal Communication System (ICS), and standby compass
Dual 28 Volt DC Electrical System with two 200 Amp Starter/Generators
AC Electrical system with Main Gearbox-driven 10-KVA generator and inverter
Exterior lighting including position lights, landing, and controllable search lights
Cabin and cockpit Bleed-air Heating system with fresh air ventilation

Equipped with these added features:
VIP Exterior paint preparation and finish with silk-screened exterior markings
Retractable cabin boarding steps, left and right
Cockpit-selectable cabin electric door locks
Locking fuel filler caps
Provisions for 50-Gallon Auxiliary Fuel Tank in the baggage compartment
Foot duct-heater in cockpit (Air Comm)
Cabin and cockpit Air Conditioning system using R-134A refrigerant
Digital Cabin Air Temperature Indicator in the cockpit
Gooseneck Map Lights for pilot and copilot
Lighted Approach Plate Holders for pilot and copilot
Custom map and cockpit storage compartments
Map table on pilot’s door
Cockpit sun visors
Windshield Heat system
Engine Inlet Snow Protection Kit
Main Rotor Bifilar (5P) vibration absorber (Not presently installed)
Nose-mounted vertical vibration absorber
High Intensity Strobe/Anti-Collision Lights (HISL), top and bottom
Second (fixed) Landing Light on the left main landing gear
Logo Lights for tail illumination
Dual 375 VA Static Inverters
Cabin ICS with handset in forward-facing credenza and additional cabin ICS jacks
Cabin Call system with bell-ringer, paging, and chime
Emergency Flotation System
Emergency Locator Transmitter (Artex ELT-110-406HM)
CAA Certification Package including AVAD

Contact Information

10 Fox Run
Allendale, New Jersey, United States - 07401
Ph: (201) 906-1411

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