Flight and Operation Manual Rev 3.0 on 09-04-2013 - Trixy Aviation

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1.6 Description Gyrocopter with nose wheel steering Stainless steel frame welded in gas-shielded process Two seats in t<strong>and</strong>em configuration inside an open cabin(Liberty) or inside an enclosed cabin made of carbon fibercomposite with removable hard top (Princess). Main undercarriage strut, equipped with hydraulic brakes Rotor made of extruded aluminum profile. Rotor head steering with push rods for 2 heads: tilt head orswash-plate head. Rudder steering with steel wires. Rudder <strong>and</strong> stabilizers made from CFC.1.7 Technical dataLengthWidth:Heigh:Empty weight:Load capacity:Max. Take-off weight:Tank capacity:4.90 m1.85 m2.80 m265 - 310 kg190 - 280 kg500 - 560 kg (as motorized)34 l / 68 l (as equipped)1.8 RotorAir foil:NACA 8H12Manufacturer:Averso AviationRotor diameter:8.4 m / 8.6 m (as equipped)Rotor surface area: 55.4 m² / 58.0 m²Specific load of rotor surface area: 10.1 kg/m² / 9.65 kg/m²Recommended overhaul/exchange: 500 h / 1000 h1.9 Propeller (3 types)Type:3B-FC Windspoon leftManufacturer:DUCwww.duc-helices.comNo. of blades: 3Diameter:173 cmBlade materialFiber-reinforced plasticPitch adjustment:Ground adjustableRecommended overhaul/exchange: 800 h<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 14
Type:CL3-V-70-(IP)-R2Manufacturer:Neuformwww.neuform-composites.deNo. of blades: 3Diameter:170 cmBlade materialFiber-reinforced plasticPitch adjustment:Adjustable in flightRecommended overhaul:1000 hType:TXL3-V-70-R2Manufacturer:Neuformwww.neuform-composites.deNo. of blades: 3Diameter:170 cmBlade materialFiber-reinforced plasticPitch adjustment:Adjustable in flightRecommended overhaul:1000 h1.10 Power plant (3 types)Type:912 ULSManufacturer:Rotaxwww.rotax-aircraft-engines.comRecommended overhaul:2000 hPerformance / RPM:100 HP / 5800 RPMContinuous output:95 HP / 5500 RPMTorque / RPM:107 Nm / 5500 RPMNr. of cylinders / type:4 / opposedDisplacement:1352 cm³Cooling system:Liquid/Air coolingLubrication:Oil in separate tankFuel:Regular unleaded (min. 95 octane)Alternative fuel:Aviation fuel AVGAS 100 LLFuel supply: 1 mechanic Pump (optional: 1Electric booster pump)Fuel / air mixture:2 CD-carburetorsConsumption at performance %: 16.5 l/h at 75%Ignition:Dual solid-state magnetosPropeller drive:Via integrated transmissionExhaust system:Steel exhaust system +2 mufflers<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 15
Page 2 and 3: Flight and
Page 4 and 5: INDEX1 GENERAL 81.1 Introduction 81
Page 6 and 7: 6.8 Doors, windows and</str
Page 8 and 9: 1 GENERAL1.1 IntroductionThis manua
Page 10 and 11: Warning: This manual is not to be c
Page 12 and 13: 1.5 Side view, top view and
Page 16 and 17: Starter:Generator:Electric (12V 0.6
Page 18 and 19: 1.11 Abbreviations and</str
Page 20 and 21: 1 OPERATING LIMITATIONS2.1 Introduc
Page 22 and 23: 2.3 Engine limitationsRotax 912 ULS
Page 25 and 26: 2.10 FuelTotal tank content: 34 l (
Page 29 and 30: All hub bolts are in place No defor
Page 31 and 32: 3.3 Pre-flight check01 Both Magneto
Page 33 and 34: 3.4 Before engine start check Passe
Page 35 and 36: 3.7 Before taxi check Close <strong
Page 37 and 38: 3.10 Take-off Accelerate with full
Page 39 and 40: 3.17 After landing
Page 41 and 42: 3.21.1 Uninstalling the rotor1. The
Page 43 and 44: 5. The second person may now releas
Page 47 and 48: 4.3 Influence of rain & insects on
Page 51 and 52: 5.2 Weighing procedureThe G 4-2 is
Page 53 and 54: 5.4 Empty weight alterationAny chan
Page 55 and 56: 5.5 Determining the center of gravi
Page 59 and 60: 6.3 Steering systemsRudder steering
Page 61 and 62: Hydraulic wheel brakesThe hydraulic
Page 63 and 64: Type PRINCESSThe stand</str
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G 4-2 is equipped with two luggage
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Flight and
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Flight and
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Flight and
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6.11 Dynamic- and
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7.2 DescriptionEMSISThe sta
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Flight and
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The warning window also displays th
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Nesis II displays warnings, wheneve
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The third main display (the flight
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The fifth main display (the setting
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Flight and
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9.2 TriebwerkansichtenSide viewDire
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9.5 Cooling systemTo check the leve
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Flight and
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Flight and
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11.1.1 Frame, propeller and
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11.4 Maintenance and</stron
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Flight and
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Minimum instrumentation required by
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Flight and
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13.2 Engine failureThe following is
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c) Landing with de
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The transceivers of type Funkwerk A
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Flight and
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Flight and Operation Manual Rev 3.0 on 09-04-2013 - Trixy Aviation

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