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) 8,600 ft 2,621 mRange (long range cruise* speed @ 4,000 feet) (no reserve)

2 - 32 5 gallon 191 nm 354 km- 64 0 gallon 375 nm 694 kmWeights Maximum takeoff gross weight 2,050 lb 930 kgEmpty weight, standard configuration 1100 lb 499 kgUseful load 950 lb 431 kgDimensionsFuselage length 22 19 ft 6 76 mFuselage width

3 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) 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)

4 6 54 ft 1 99 mAccommodationNormal cabin seating (training) 2 Maximum certified cabin seating (utility) 3 Cabin length 4 75 ft 1 45 mCabin width 4 92 ft 1 50 mPowerplantsType

5 Textron Lycoming HIO-360-D1 APowerplant ratings (per engine, standard day, sea level)- Takeoff (5-minute) 190 shp 141 kw- Maximum continuous 190 shp 141 kwFuel CapacityStandard fuel capacity 32 5 US gal 123 03 lExtended range capacity

6 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)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)

7 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, 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.

8 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 fairings Fuel flow oil filter, remotely mounted Low fuel warning light Lycoming HIO-360-D1A engine M/R transmission oil temp/pressure warning light Magnetic compass Manifold pressure gauge Oil cooling system with integral spin-off oil filter Oil filler/dipstick Outside air temperature gauge Running time (Hobbs) meter, panel mounted T/R transmission chip detector warning light*Requires purchase of communication transceiver**Not available w/cargo hook - optional grip availableNote: Manufacturer reserves the right to modify this configuration by substituting comparable or better in the aircraft basic certified empty weight.

9 Based on 2007 300c Technical InformationSZR-004 February 2008 1473 Optional EquipmentUtility and Convenience Options Alternator, electrosystems 130 amp Cabin cover Cargo hook installation Cargo rack Cyclic grip, special Door openers, pneumatic Doors, triple latch Elastomeric teeter bearings Fire extinguisher, dry chemical Fire extinguisher, halon First aid kit Float kit, fixed Fuel system, auxiliary (64 gallon) Grease fitting, short shaftAvionics Options ADF receiver, KR87 with KI227-00 indicator Attitude gyro Audio panel, KMA24H-71 Blind encoder, ACK A-30 Clock, electrical Clock, quartz (LC-2) Clock, quartz (LC-2E) Comm/GPS, Garmin GNC 420 Comm/GPS, Garmin GNC 420A Comm/GPS, moving map, Garmin 250XL Comm transceiver, KY196A Comm transceiver, KY96A Compass-vertical card, overhead Compass system, KCS55A with HSI and heading transmitter Dimmer assembly, supplemental Directional gyro Emergency locater transmitter, EBC502 Fan, avionics cooling Intercom foot switch Headset, David Clark H10-56 Intercom, NATAA80 Intercom, NATAA83 stereo Intercom, NATAA85 Marker beacon, KR21 Master avionics switch NAV/COMM, KX155-39 with 203 CDI NAV/COMM/GS, KX155-43 with KI209 CDI NAV/COMM/GS Garmin GPS, GNC 430 with Gi106A indicator Transponder, Garmin GTX320A, 327 Turn coordinator Turn and slip indicator, Electric Gyro Corp.

10 Vertical speed indicator, United 7000 Ground handling wheels, flyable Heater, muff Heater, Paravion High stance landing gear with extra heavy duty gear Hobbs meter - landing gear contact switch Landing lights - two or three position Map case Muffler Skid shoes, extra heavy duty STAR system (start-up overspeed limiter, automatic rotor engagement, low RPM warning device) Up-stack exhaust installation Up-stack exhaust with supertrap Windows, with sliding glass 7 Schweizer 300c Technical InformationSZR-004 February 2008 1473 Paint OptionsBASF Glasurit exterior paint is used on all Schweizer 300 CTM helicopters. It is one of the most technically advanced paints available and is used by numerous premium automobile companies such as BMW and Mercedes. The Schweizer nine-step paint process assures superior corrosion protection and a durable, yet highly attractive appearance.