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

More documents

Recommendations

Info

The fourth main display (the modern instrument screen):This screen is the glass cockpit (modern instrumentation) display. Theindicated air speed is displayed on a vertical scale with a dial containingthe IAS in numbers. The true air speed is indicated at the bottom of thevertical scale. The altitude is indicated on a vertical scale on the rightside of the moving map with a dial containing the altitude in numbers.The vertical speed is indicated on a vertical scale on the right side of thealtitude scale. The G-meter is indicating the acceleration in a whitewindow below the Vertical speed indicator.Engine RPM, Rotor RPM <strong>and</strong> manifold pressure are indicated left of theengine data at the left bottom corner of the display.Traffic awareness, ADS-B <strong>and</strong> Flarm (if installed) will be displayed onthe moving map in this display.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 84
The fifth main display (the setting screen):The user can set in this screen the desired personal settings.Downloads <strong>and</strong> uploads of data are also activated in this screen.More information about the operation <strong>and</strong> the proper use of the unit isfound in the separated manual of NESIS.<strong>Flight</strong> <strong>and</strong> operation manual G 4-2 <strong>Rev</strong>ision <strong>3.0</strong> – 09.04.2013 85
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 and 80: The warning window also displays th
Page 81 and 82: Nesis II displays warnings, wheneve
Page 83: The third main display (the flight
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
show all

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

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?