| CPC B64D 37/04 (2013.01) [B64D 37/30 (2013.01)] | 14 Claims |

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1. An aircraft comprising a fuselage and a wing, and at least one fuel tank; wherein
the at least one fuel tank includes a hydrogen fuel tank mounted to the wing, wherein the hydrogen fuel tank is mounted above the wing and spaced from an upper surface of the wing by a tank mounting arrangement,
the tank mounting arrangement mounts the hydrogen fuel tank to the wing via an engine pylon mounted to a lower surface of the wing, and
the tank mounting arrangement comprises a forward fuel tank support strut extending between the hydrogen fuel tank and a first aircraft mounting point provided forward of the wing, and a rear fuel tank support strut extending between the hydrogen fuel tank and a second aircraft mounting point provided aft of the wing.
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