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

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3.9 Preparation for take-off <strong>and</strong> pre-rotationWarning: Take-off direction should be against the wind if possible!The maximum crosswind during take-off is 35 km/h!Insure the rotor control stick position while pre-rotation otherwisesevere damage may be caused!Attention: During pre-rotation the control stick must be held in theforward center position until a minimum of 180 RPM has ben reachedotherwise a collision between the rotor <strong>and</strong> empennage may occur. Hold stick in front, center position Hold break engaged Check engine instruments Check ignition circuits at 3000 RPM. The speed drop should beno more than 150 RPM when turning off one of the circuits. Throttle back to idle position. Request take-off permission (if required) Line up against the wind on the runway <strong>and</strong> engage the brakes Rotor area free? Adjust trim nose heavy to keep the stick in a forward position Hold the stick in the forward, middle position Quickly but gently push pre-rotator pedal forward with foot Maintain engine RPM at 2500-3000 RPM with the throttle lever Build up rotor speed of 200-220 RPM with the throttle <strong>and</strong> pedal Release the pre-rotator pedal <strong>and</strong> put feet on both rudder pedals Pull the rotor control stick back towards body all the way In case of crosswind turn rotor sideways as required Release brake Push throttle forward until engine reaches maximum power Adjust trim as requiredWarning: Before accelerating, make sure the stick is pulled back allthe way towards your body. It is life threatening to start accelerationwith the stick forward.<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 36
3.10 Take-off Accelerate with full throttle Hold direction using rudder pedals Briefly check engine instruments Climb speed is 90-110 km/h IAS As soon as nose wheel leaves the ground push stick forwardgently <strong>and</strong> take-off flat on the main gear.3.11 Climb Adjust trim pressure for comfortable control stick Check engine instruments L<strong>and</strong>ing lights? Minimum safe altitude reached? Engine power as required (also see engine manual)3.12 Cruise Adjust trim pressure as desired for confortable cruise Check engine instruments Auxiliary fuel pump (optional) off unless needed Adjust engine to cruising speed 80-160 km/h at 4000-5500 RPM Periodically check engine instruments <strong>and</strong> fuelThe permissible maximum speed (VNE) is 167 km/h may never beexceeded. During strong turbulences the maneuver speed VA (100km/h) must be adhered to.Attention: The fuel required during cruise depends on the weatherconditions, speed <strong>and</strong> load. The indicated fuel consumption in theglass cockpit is a calculated value based on engine RPM <strong>and</strong> itshould not to be used as a true value for remaining fuel calculations.Consider possible fuel leaks which the instrument is not detecting.3.13 Descent Use engine throttle to maintain 100 km/h (110 km/h in case ofrain or turbulence) Adjust trim pressure for descent Request l<strong>and</strong>ing permission (if required) Enter traffic pattern (if required) <strong>and</strong> check engine instruments<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 37
Page 2 and 3: Flight and
Page 4 and 5: INDEX1 GENERAL 81.1 Introduction 81
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Page 14 and 15: 1.6 Description Gyrocopter with nos
Page 16 and 17: Starter:Generator:Electric (12V 0.6
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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 (
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Page 31 and 32: 3.3 Pre-flight check01 Both Magneto
Page 33 and 34: 3.4 Before engine start check Passe
Page 35: 3.7 Before taxi check Close <strong
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
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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 and 80: The warning window also displays th
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Page 83 and 84: The third main display (the flight
Page 85 and 86: 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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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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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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