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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

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

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5.5 Determining the center of gravityExplanati<strong>on</strong>:Hereafter is an example (see weighing report in secti<strong>on</strong> 5.3).Weight in kg X in mm X-MomentEmpty weight 272 2320 631<strong>04</strong>0Pilot 80 1190 95200Co-Pilot 73 1950 142350Luggage 5 1950 9750Fuel 20 2215 44300Summ 450 922640CG= 922640 / 450 = 2050 cm from datumThe empty mass of the gyrocopter is 272 kg (last valid).The center of gravity is located 2320 mm from the Pitot-tube’s leadingedge in X-directi<strong>on</strong>.The X-Moment = 272 * 2320 = 631<strong>04</strong>0Sum of all weights = 450 kgSum of all X-moments = 922290The CG of the loaded gyrocopter in X-directi<strong>on</strong> is calculated:922290 / 450 = 2050 mmWarning: The center of gravity must be within the following limits:In X-directi<strong>on</strong> between 1900 mm <str<strong>on</strong>g>and</str<strong>on</strong>g> 2200 mmThe pilot’s mass must be between 65 <str<strong>on</strong>g>and</str<strong>on</strong>g> 125 kg.The valid MTOF must be observed.The CG is calculated by the pilot in comm<str<strong>on</strong>g>and</str<strong>on</strong>g> in the following table (forhelp see example above):<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> 55

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