According to CS-VLA, a landing gear has to be tested using a drop test. The Peak Normal accelerations have been recorded and plotted in the graph below: 5 Peak normal acceleration 3 N 0.1 0.2 0.3 Drop height, metres 0.4 Aircraft data: MAUM = 24 kg; Wing Area (S) = 1.5 m Question: 0.5 0.6 Calculate the (1) Level Landing condition limit maximum vertical reaction and (2) Spring Back condition load cases to be proven for the main gear assembly? (So calculate the Forces on the landing gear)!