Airframe
Entered into service 2006Total Time: 820
General Specifications
Standard S-92 Aircraft featuring:- Two General Electric CT7-8 Turbo-shaft Engines w/Integral Particle Separator and Pneumatic Starters
- AlliedSignal 36-150[S-92] Auxiliary Power Unit 90 shp w/35 KVA 3-phase AC Generator
- Engine Instrument and Caution Advisory System (EICAS)
- Four Blade Fully Articulated Main Rotor System w/Manual Bladefold Provisions
- Dual Controls
- 115 Volt 400 Hz AC
- 3-phase Electrical System with two 75 KVA Oil Cooled Generators and two 28 Volt DC 400 amp DC Converters
- One 28 volt DC 15 Amp-hour Battery
(Note: This battery is replaced by Option 81002 24 AMP Hour Battery) - Upper Anti-Collision light (strobe)
- Retractable Landing Gear
- 760 Gallons Fuel in two External Sponsons with Self-Sealing Breakaway Valves
- Pressure Refueling System
- Pilot and copilot Heated Glass Windshields
- Dual Windshield Wipers w/Washer System
- Exterior Lighting
- Bleed Air Heating and Defogging
- Pilot and Copilot Seats with 5 Point Restraint/Harness
(Note: These seats are replaced by Option 71007 Crew Seats with Sheepskin seating)
- Active Vibration Control System
- Large 6 Ft High by 6 Ft wide by 20 Ft long Cabin Area
- Four (4) cabin emergency exits
- Two (2) cockpit emergency exits
- Hydraulic Cargo Ramp
- Six (6) Exterior Aircraft tiedown fittings
ADDITIONAL SPECIFICATIONS
- Avionics Management System
- Dual Collins VHF-422D
- Dual VOR/ILS Collins VIR-432
- Dual Mode S Transponder, TDR-94D
- Dual DME Collins DME-442
- FMS w/ GPS
- Primus 880
- Digital Moving Map EuroAvionics
- EGPWS
- TCAS-I
- Honeywell JetMap
- Life rafts
- Emergency Flotation System (EFS)
- Air Conditioning System
- Rotor Blade Ice Protection System