The calculation of hangpoints to the airframe GRS 6/1420-1640 SDS FF

GRS 6/1420-1640 SDS FF


x= Speed aircraft VNE - km/h
y= Dynamic opening shock - power kN

curve 1 150 200 260 300 speed km/h
47,0 48,3 50,2 59,0 power kN
curve 2 150 200 230 250 speed km/h
57,7 58,6 60,0 62,2 power kN

Max. MTOW 1.645 Kg /250 Km/h
curve 1 - 1420 kg
curve 2 - 1645 kg

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