Schweizer 300C Helicopter - WFH Florida

1 Schweizer 300 CTM HelicopterPiston-Powered Multi-Mission Schweizer 300 CTM HELICOPTERTECHNICAL INFORMATION1 Schweizer 300c technical InformationSZR-004 February 2008 1473 Performance Standard day, sea level, maximum gross weight unless otherwise notedMaximum speed (VNE) 95 kts 176 km/hrMaximum cruise speed (VH) 86 kts 159 km/hrHover ceiling, In-Ground-Effect (1700 lb) 10,800 ft 3,292 mHover ceiling, Out-of-Ground-Effect (1700 lb)

2 8,600 ft 2,621 mRange (long range cruise* speed @ 4,000 feet) (no reserve)- 32 5 gallon 191 nm 354 km- 64 0 gallon 375 nm 694 kmWeights Maximum takeoff gross weight

3 2,050 lb 930 kgEmpty weight, standard configuration 1100 lb 499 kgUseful load 950 lb 431 kgDimensionsFuselage length

4 22 19 ft 6 76 mFuselage width 4 25 ft 1 30 mFuselage height 7 17 ft 2 18 mOverall length (rotors turning) 30 83 ft 9 40 mOverall height (to top of tail rotor) 8 72 ft 2 65 mWidth (canopy)

5 4 25 ft 1 30 mMain rotor diameter 26 83 ft 8 18 mTail rotor diameter 4 25 ft 1 30 mMain landing gear tread (fully compressed) 6 54 ft 1 99 mAccommodationNormal cabin seating (training) 2 Maximum certified cabin seating (utility)

6 3 Cabin length 4 75 ft 1 45 mCabin width 4 92 ft 1 50 mPowerplantsType Textron Lycoming HIO-360-D1 APowerplant ratings (per engine, standard day, sea level)- Takeoff (5-minute)

7 190 shp 141 kw- Maximum continuous 190 shp 141 kwFuel CapacityStandard fuel capacity 32 5 US gal 123 03 lExtended range capacity 64 0 US gal 242 27 ISpecificationsAnti-Submarine Warfare (ASW)Anti-Surface Warfare (ASuW)Search and Rescue (SAR)Vertical Replenishment (VERTREPS)2 Schweizer 300c technical InformationSZR-004 February 2008 1473 ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m)

8 Aircraft Dimensions3 Schweizer 300c technical InformationSZR-004 February 2008 1473 The 300 CTM Helicopter s cockpit offers two different configurations. The standard right-hand Pilot-In-Command (PIC) flight control configuration allows for comfortable seating of an instructor and student. With the optional left-hand PIC configuration, the right-hand controls can be removed making it possible to seat a pilot and two Layout4 Schweizer 300c technical InformationSZR-004 February 2008 1473 Full Panel (Police/Military)Small Profile PanelStandard PanelIntermediate PanelCockpit Instrument Display Panel5 Schweizer 300c technical InformationSZR-004 February 2008 1473 Standard EquipmentAirframe and Control Systems Three bladed fully articulated main rotor Elasometric main rotor dampers Dual flight controls, left hand pilot-in-command Collective friction control Cyclic friction control, two axis Electric cyclic trim, two axis Tubular skid-type landing gear Conical tail rotor teetering bearingsPowerplant.

9 Systems and Instruments gallon fuel tank Airspeed indicator Altimeter Ammeter Cylinder head temperature indicator Dual engine/rotor tachometer Dual large oil coolers Engine oil pressure indicator Engine oil temperature indicator Exhaust collector Fuel pressure indicator Fuel quantity indicator Fuel shut-off valveElectrical System 70 amp alternator Cabin accessory plug Circuit breaker protection Cyclic mounted radio frequency scrolling switch*, ** External APU plug Lead acid battery Light weight, high torque starter Modular electric harness Night lights with strobe beacons Switchable hot mic intercom systemElectrical System Adjustable ventilation system Three-seat cushioned interior Clear cabin door windows Floor/cabin carpet Circular air scoop vents on doors Lap belts and shoulder harnesses Tinted canopy windows Single latch doors Glove box Offset anti-torque pedals Booted Oleo landing gear dampers Heavy duty skid shoes Ground handling wheel brackets Fuselage jack/lift fittings Tie down kit White Glasurit Urethane paint Three piece chin skin with integral side

10 Fairings Fuel flow oil filter, remotely mounted Low fuel warning light Lycoming HIO-360-D1A engine M/R transmiss