| CPC B64C 25/66 (2013.01) [B64C 25/54 (2013.01); B64C 25/58 (2013.01); B64C 2025/008 (2013.01)] | 20 Claims |

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1. A float assembly mountable to an aircraft, the float assembly comprising:
a float extending lengthwise between a bow of the float and a stern of the float;
a nose wheel being coupled to the bow of the float, the nose wheel being rotatable about a wheel axis and being able to swivel about a swivel axis; and
a bifluidic strut being coupled to the nose wheel, the bifluidic strut containing a liquid and a gas, the bifluidic strut having a strut longitudinal centerline, the bifluidic strut having selectively a compressed state and an extended state, the bifluidic strut being longer in the extended state than in the compressed state, the strut longitudinal centerline being at a first angle to the swivel axis when the bifluidic strut is in the compressed state, the strut longitudinal centerline being at a second angle to the swivel axis when the bifluidic strut is in the extended state, and the first angle being different than the second angle.
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