| 摘要 |
The invention relates to an overhead panel capable of being arranged in an aircraft cockpit, which includes a set of independent sub-modules (67) each associated with a specific system or a specific function of the aircraft, built into a rigid self-supporting module (60), comprising a front surface (65) on which the sub-modules (67) are mounted, and two side surfaces provided with peripheral connectors (63) intended for being connected to various aircraft systems. The invention also relates to a method for manufacturing such a panel. |
