根据4月21最终试验的结果，机翼和后缘的承受的极限负荷为2.5g左右，而实际最高负荷只能在实际服役的时候才能知道。
The final test occurred Apr. 21 when the wing and trailing edges were subjected to their limit load of around 2.5g, the highest loads expected to be seen in service.
根据4月21最终试验的结果，机翼和后缘的承受的极限负荷为2.5g左右，而实际最高负荷只能在实际服役的时候才能知道。
The final test occurred Apr. 21 when the wing and trailing edges were subjected to their limit load of around 2.5g, the highest loads expected to be seen in service.
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