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

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

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13.8.3 Loss of maneuverability of yaw axis:C<strong>on</strong>trol course <str<strong>on</strong>g>and</str<strong>on</strong>g> speed by pitching <str<strong>on</strong>g>and</str<strong>on</strong>g> rolling.C<strong>on</strong>trol altitude with engine power.13.8.4 Loss of maneuverability of banking:Hold course with side rudders, l<str<strong>on</strong>g>and</str<strong>on</strong>g> straight ahead.C<strong>on</strong>trol altitude with engine power.13.8.5 GEN-light:The normal electric circuit voltage is around 13.2 V. The glass cockpitNESIS II displays a warning <strong>on</strong>ce the circuit voltage drops below 12 V.The display of the glass cockpit darkens at a voltage around 10 V.However, the unit c<strong>on</strong>tinues to operate with a voltage as low as 6.5 V.The generator light lamp is used to check the generator. If the LEDstays <strong>on</strong> c<strong>on</strong>stantly during flight, the battery is no l<strong>on</strong>ger charged. If thisoccurs, all electrical loads beside the glass cockpit, the transceiver <str<strong>on</strong>g>and</str<strong>on</strong>g>the transp<strong>on</strong>der are to be turned off:1. All external units c<strong>on</strong>nected to the board net OFF2. L<str<strong>on</strong>g>and</str<strong>on</strong>g>ing light OFF3. Navigati<strong>on</strong> light OFF4. Windshield fan OFF5. Cabin heat fan OFFIf the voltage c<strong>on</strong>tinues to drop down, the pilot must plan a normall<str<strong>on</strong>g>and</str<strong>on</strong>g>ing in the closest airfield <str<strong>on</strong>g>and</str<strong>on</strong>g> must be ready for a safety l<str<strong>on</strong>g>and</str<strong>on</strong>g>ing, ifhe cannot reach an air field. At a voltage of 12 V or lower, the pilot mustc<strong>on</strong>sider a safety l<str<strong>on</strong>g>and</str<strong>on</strong>g>ing.A sudden drop of the electrical circuit will cause all electr<strong>on</strong>ic units inthe panel to drop off. In such a case, the pilot must initiate a safetyl<str<strong>on</strong>g>and</str<strong>on</strong>g>ing or an emergency l<str<strong>on</strong>g>and</str<strong>on</strong>g>ing. The pilot should reset all circuitbreakers in the panel. If this solves the problem, the pilot must plan anormal l<str<strong>on</strong>g>and</str<strong>on</strong>g>ing in the closest air field. The pilot must keep an eye <strong>on</strong> thevoltage <str<strong>on</strong>g>and</str<strong>on</strong>g> remain alert for a safety or emergency l<str<strong>on</strong>g>and</str<strong>on</strong>g>ing.A drop of the electrical circuit should not cause the engine type Rotax912 ULS to quit. However the engines of type Rotax 914 UL <str<strong>on</strong>g>and</str<strong>on</strong>g> <strong>Trixy</strong>912 TI are equipped with electrical fuel pumps. A breakage of the boardnet will cause these those engines to quit.<str<strong>on</strong>g>Flight</str<strong>on</strong>g> <str<strong>on</strong>g>and</str<strong>on</strong>g> operati<strong>on</strong> manual G 4-2 <str<strong>on</strong>g>Rev</str<strong>on</strong>g>isi<strong>on</strong> <str<strong>on</strong>g>3.0</str<strong>on</strong>g> – <strong>09</strong>.<strong>04</strong>.<strong>2013</strong> 110

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