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

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Starter:Generator:Electric (12V 0.6 kW)Alternating current with externalRectifier (12V 20A DC)Type:914 ULManufacturer:Rotaxwww.rotax-aircraft-engines.comRecommended overhaul:2000 hPerformance / RPM:115 HP / 5800 RPMContinuous output:100 HP / 5500 RPMTorque / RPM:128 Nm / 5500 RPMNr. of cylinders / type:4 / opposedDisplacement:1211 cm³Cooling system:Liquid/Air coolingLubrication:Oil in separate tankFuel:Regular unleaded (min. 95 octane)Alternative fuel:Aviation fuel AVGAS 100 LLFuel supply: 1 electric Pump (optional: 2electric pump2)Fuel / air mixture:2 CD-carburetorsConsumption at performance %: 20.4 l/h at 75%Ignition:Dual solid-state magnetosPropeller drive:Via integrated transmissionExhaust system:Steel exhaust system +2 mufflersStarter:Electric (12V 0.6 kW)Generator:Alternating current with externalRectifier (12V 20A DC)Type:Manufacturer:Recommended overhaul:Performance / RPM:Continuous output:Torque / RPM:Nr. of cylinders / type:Displacement:Cooling system:Lubrication:Fuel:912 TITrixy Aviationwww.trixyaviation.com2000 h130 HP / 5800 RPM113 HP / 5500 RPM145 Nm / 5500 RPM4 / opposed1211 cm³Liquid/Air coolingOil in separate tankRegular unleaded (min. 95 octane)<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 16
Alternative fuel:Aviation fuel AVGAS 100 LLFuel supply: 1 electric Pump (optional: 2electric pump2)Fuel / air mixture:2 CD-carburetorsConsumption at performance %: 2<strong>3.0</strong> l/h at 75%Ignition:Dual solid-state magnetosPropeller drive:Via integrated transmissionExhaust system:Steel exhaust system +2 mufflersStarter:Electric (12V 0.6 kW)Generator:Alternating current with externalRectifier (12V 20A DC)<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 17
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 14 and 15: 1.6 Description Gyrocopter with nos
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
Page 65 and 66: 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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