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

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The first main display:1- Indicated air speed 2- True air speed3- Engine RPM (UPM x1000) 4- Manifold pressure5- Rotor RPM 6- CHT (2x)7- Oil temperature 8- Oil pressure9- Fuel pressure 10- Circuit voltage11- Cirsuit current 12- Turn coordinator13- Fuel consumption l/h 14- Average consumption (l/h)15- Range (km) 16- Endurance (h)17- Fuel gauge 18- G-Meter (acceleration)19- Vertical speed indicator 20- QNH21- Altitude indicator 22- GPS (moving map)23- Current position 24- Electronic compassMore information such as coordinates of current position, current time<strong>and</strong> ground speed are also displayed on this screen.<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 80
Nesis II displays warnings, whenever a value (oil pressure, CHT, max.air speed, min. rotor RPM, …..) gets out of the set limits. The illustrationbelow shows a “Fuel Low” warning.When connected to the transceiver <strong>and</strong> set for audio warnings, theNESIS II will also announce audio warnings in the head set. The usermay enable or disable any of the warnings in the setting list of warnings.Audio (beep) or voice warnings may also be enabled or disabled in thesame list. The range limits for each warning are predefined <strong>and</strong> cannotbe changed by the user in the unit.Turning the rotating knob 2 will result in zooming in or out in the movingmap. Turning the rotating knob 1 will toggle between the 5 maindisplays.<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 81
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 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 27 and 28:
Flight and
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 45 and 46: Flight and
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
Page 73 and 74: 6.11 Dynamic- and
Page 75 and 76: 7.2 DescriptionEMSISThe sta
Page 79: The warning window also displays th
Page 83 and 84: The third main display (the flight
Page 85 and 86: The fifth main display (the setting
Page 89 and 90: 9.2 TriebwerkansichtenSide viewDire
Page 91 and 92: 9.5 Cooling systemTo check the leve
Page 97 and 98: 11.1.1 Frame, propeller and
Page 99 and 100: 11.4 Maintenance and</stron
Page 103 and 104: Minimum instrumentation required by
Page 107 and 108: 13.2 Engine failureThe following is
Page 109 and 110: c) Landing with de
Page 111 and 112: The transceivers of type Funkwerk A
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Flight and Operation Manual Rev 3.0 on 09-04-2013 - Trixy Aviation

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