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

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INDEX1 GENERAL 81.1 Introduction 81.2 Registration <strong>and</strong> certification basis 81.3 Performance data <strong>and</strong> operating procedure 81.4 Warnings <strong>and</strong> precautions 81.5 Three side views 121.6 Description 141.7 Technical data 141.8 Rotor 141.9 Propeller 141.10 Power plant 151.11 Abbreviations <strong>and</strong> terminology 182 OPERATING LIMITS 202.1 Introduction 202.2 <strong>Flight</strong> speeds 212.3 Engine limits 222.4 Weights 232.5 Center of gravity 242.6 Admissible maneuvers 242.7 G-forces 242.8 Minimum crew 242.9 Operating modes 242.10 Fuel 242.11 <strong>Operation</strong> fluids 252.12 Limitation labels 263 NORMAL OPERATION 283.1 Introduction 283.2 Periodic inspection 283.3 Pre-flight check 313.4 Pre-startup check 353.5 Operating procedures with external power source 353.6 Engine startup 353.7 Pre-taxi check 353.8 Check during taxying 353.9 Preparation for take-off <strong>and</strong> pre rotation 363.10 Take-off 37<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 4
3.11 Climb 373.12 Cruise 373.13 Descent 373.14 Pre-l<strong>and</strong>ing check 383.15 Go-around procedure 383.16 Touchdown 383.17 Post l<strong>and</strong>ing check 393.18 Engine shut down 393.19 Securing the gyrocopter 393.20 Mounting <strong>and</strong> removing the rotor 403.21 H<strong>and</strong>ling the rotor system 403.22 Propeller 444 FLIGHT PERFORMANCE 464.1 Introduction 464.2 Performance data 464.3 Influence through rain <strong>and</strong> insects 474.4 Max. ascertained cross-wind 474.5 Noise data 474.6 Tire pressure 474.7 Service ceiling 474.8 Torque specifications 484.9 Battery <strong>and</strong> generator 494.10 Altitude <strong>and</strong> pace diagram 495 WEIGHTS AND CENTER OF GRAVITY 505.1 Introduction 505.2 Weighing procedure 515.3 Weighing report 525.4 Empty mass alteration 535.5 Determining the center of gravitiy 556 SYSTEM DESCRIPTION 586.1 Introduction 586.2 Gyrocopter explanation 586.3 Control system 596.4 Instrument panel 626.5 Drive train 646.6 Seats <strong>and</strong> seat belts 646.7 Luggage compartments 65<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 5
Page 2 and 3: Flight and
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 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 57 and 58:
Flight and
Page 59 and 60:
6.3 Steering systemsRudder steering
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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
Page 69 and 70:
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
Page 95 and 96:
Flight and
Page 97 and 98:
11.1.1 Frame, propeller and
Page 99 and 100:
11.4 Maintenance and</stron
Page 101 and 102:
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
Page 109 and 110:
c) Landing with de
Page 111 and 112:
The transceivers of type Funkwerk A
Page 113 and 114:
Flight and
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