S-300C™ Helicopter Piston-Powered Helicopter

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S-300C™ Helicopter General Overview TH-S-300C PAYLOAD-WEIGHTS FULL FUEL 30 MINUTE FUEL EXTERNAL LOAD INTERNAL LOAD GROSS WEIGHT 2050 2150 EMPTY WEIGHT 1100 PILOT 170 PAYLOAD 600 850 750

Technical Specifications S-300C™ Helicopter Technical Specifications Dimensions Height (overall) 8.72 ft (2.65m) Length (overall) 30.83 ft (9.4m) Fuselage Length 22.19 ft (6.76m) Landing gear thread width 6.54 ft (1.99m) Weight Empty weight 1,100 lbs (499kg) Gross weight 2,050 lbs (930kg) Useful load 950 lbs (431kg) Rotor System Main rotor diameter 26.83 ft (8.18m) Main rotor disk areas 565 sq. ft. (52.49 sq. m.) Main rotor RPM 471 Tail rotor diameter 4.25 ft (1.30m) 3 blade articulated Fuel Standard capacity 32 gal (192 lbs, 87kg) With Auxiliary Fuel 64 gal (384 lbs, 174kg) 4 4

S-300C™ Helicopter Cabin Spacious cabin provides sufficient room for training or patrol missions that require the use of flight helmets Cabin useful weight limit of 950 lbs. Optional right hand PIC position available. Ideal for external load training Only production helicopter to offer 360° visibility from pilot’s seat - far exceeds FAA requirements of AC-27-1

S-300C™ Helicopter Instrument Panel New aircraft instrument panels available in both IFR and VFR training configurations Instrument panel can accommodate up to ten three-inch instruments plus a complement of avionics required for comprehensive procedural IFR training Avionics and instruments are well within reach of both pilot positions

S-300C™ Helicopter Control System Solid, conventional style cyclic similar to those used in larger helicopters Allows ab-initio students to learn through direct feedback of instructor control movements No obstacles in center of cabin to impede pilots’ reach of instrument panel Ergonomically designed anti-torque pedals with large pedal surface area. Pedals adjustable 7 5/8" to accommodate pilots of various heights

S-300C™ Helicopter Engine Lycoming HIO-360-D1A Maximum take-off 190 shp (141kw) Maximum continuous Vne at sea level 95 kts (176km/h) Cruise Speed 86 kts (159km/h) Maximum Endurance w/std. fuel 3.7 hrs. Maximum Endurance w/aux fuel 7.4 hrs. Maximum Range w/aux fuel 412 nm Hover Ceiling IGE @ GW 10,800 ft (3,292m) Hover Ceiling OGE @ GW 8,600 ft (2,621m) 8 8

S-300C™ Helicopter Main Rotor System Three-bladed, fully articulated M/R system with elastomeric dampers Never subject to mast bumping and therefore more forgiving of improper control inputs by students More capable of landing on slopes than teetering rotor systems Fully field maintainable

S-300C™ Helicopter Optional Equipment Basic Accessories Upstack with noise diffuser Muffler Paravion heater system Auxiliary 64 gallon fuel system Ground handling wheels Map case Safety kit Triple latch locking doors Avionics King-complete line Emergency locator transmitter IFR avionics suite Garmin GPS David Clark headset and boom mike Blind encoder Intercom floor switch Instrument Panel Options Small profile panel Intermediate panel Full panel Law Enforcement Options Search lights P.A./Siren system EO/IR/TV sensor and controls Radio/intercom/P.A. Mixer 130 amp alternator Utility and Convenience Options Utility float kit ENG configuration High stance landing gear Cargo rack Protective cabin cover, waterproof Heavy duty skid shoes Cargo hook Agricultural spray equipment STAR System: - Start-up overspeed limit - Automatic rotor engagement - Low rotor warning

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