| 摘要 |
An aircraft assembly having an aerodynamic surface, the assembly including a fuel tank having a refuel opening 60 within a recess 52 of the aerodynamic surface, and a hinged access door 70 having a closed position in which it encloses the recess and an open position in which the recess is accessible. The inner surface 76 of the access door 70 carries a fuel cap 80 integrated with the access door such that in the closed position, the fuel cap 80 covers the refuel opening 60 but in the open position the fuel cap is remote from the refuel opening to allow access to the refuel opening. |
