1998 Sikorsky S76C+ Specifications and Summary

Transcription

1 Specifications and Summary Sikorsky S-76C+ VVIP Helicopter Page 1 of 8

2 Aircraft Data Manufacturer: Sikorsky Aircraft Corporation, United Technologies Model Designation: S-76C+ Serial Number: Date of Manufacture: December 1998 Current Civil Registration Number: C- FHMQ Total Time, Airframe: 4734 Hours as of April 15, 2017 Number and Type of Engines: Two (2) Turbomeca Arriel 2S1, Turboshaft ENGINE ON SBH No. 1 Engine Serial No.: TTE(1): 3,431:25 Hours since new TSO(1): 125 Hours since overhaul No. 2 Engine Serial No.: TTE(2): 3,221:31 Hours since new TSO(2): 125 Hours since overhaul Maximum Gross Weight: 11,700 Pounds Equipped Weight Empty / CG: STA Basic Mission Configuration: VVIP transportation, six cabin seats Page 2 of 8

3 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 Page 3 of 8

4 Equipped with these added features: (continued) 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 HM) CAA Certification Package including AVAD Avionics Systems: 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 Page 4 of 8

5 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 Page 5 of 8

6 Photographs Page 6 of 8

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8 Major Component Status Major Component Status for S-76C+ serial number is shown below at total airframe time: 4734 Hours, as of April 15, 2017 Component Service Limit Remaining Main Gearbox ( ) 3,250 Hours (Overhaul) Hours (On PAP) Intermediate Gearbox 4,500 Hours (Overhaul) 4,383.6 Hours (On PAP) Tail Rotor Gearbox 4,000 Hours (Overhaul) 3,289.2 Hours (On PAP) Main Rotor Blade (S/N: 02413) 28,000 Hours (Retire) 23,261.2 Hours Main Rotor Blade (S/N: 02435) 28,000 Hours (Retire) 23,261.6 Hours Main Rotor Blade (S/N: 02459) 28,000 Hours (Retire) 23,285.3 Hours Main Rotor Blade (S/N: 02432) 28,000 Hours (Retire) 23,261.6 Hours Main Rotor Hub (-049) 18,000 Hours (Retire) 13,261.7 Hours Bifilar Assembly (3P) 29,400 Hours (Retire) 24,661.6 Hours Bifilar Assembly (5P) 29,400 Hours (Retire) 24,928.2 Hours Main Rotor Spindle (S/N: 03181) 5,000 Hours (Retire) Hours Main Rotor Spindle (S/N: 03203) 5,000 Hours (Retire) Hours Main Rotor Spindle (S/N: 03231) 5,000 Hours (Retire) Hours Main Rotor Spindle (S/N: 03183) 5,000 Hours (Retire) Hours Tail Rotor Blade (S/N: 0394) 20,000 Hours (Retire) 11,400.6 Hours Tail Rotor Blade (S/N: 0046) 20,000 Hours (Retire) 7,476.1 Hours Fuel Selector Valve (#1) 10 Years (Retire) Next Due: 10/31/2018 Fuel Selector Valve (#2) 10 Years (Retire) Next Due: 7/24/2018 Tail Driveshaft Bearing Support (#1) 3,000 Hours (Overhaul) Hours Tail Driveshaft Bearing Support (#2) 3,000 Hours (Overhaul) 2,101.6 Hours Tail Driveshaft Bearing Support (#3) 3,000 Hours (Overhaul) 1,091.4 Hours Tail Rotor Retaining Plate 9,100 Hours (Retire) 4,361.6 Hours No.1 Engine (S/N: 20661) 3,500 (Overhaul) 3,363.6 Hours No.2 Engine (S/N: 20719) 3,500 (Overhaul) 3,363.6 Hours LH Nose Float Bottle (S/N: 5469) 10 Years (Retire) Next Due: 6/15/2018 RH Nose Float Bottle (S/N: 5460) 10 Years (Retire) Next Due: 6/15/2018 LH Main Float Bottle (S/N: 5481) 10 Years (Retire) Next Due: 6/15/2018 RH Main Float Bottle (S/N: 5466) 10 Years (Retire) Next Due: 6/14/2018 Horizontal Stabilizer Support Fitting 14,000 Hours (Retire) 9,261.3 Hours Page 8 of 8