Device for releasing a panel of an aircraft, said device being configured to be secured to a support, said support having an opening and said device being applied in order to cover a periphery of said opening, said device comprising: - a panel configured to be arranged at least opposite said opening, - at least two ejector components (8, 8'), each of said at least two ejector components (8, 8') comprising: • a stud (11, 21, 41) extending in a longitudinal direction oriented perpendicularly relative to said panel, • a compression pre-stressed spring in said longitudinal direction, said spring being coaxially arranged around said stud (11, 21, 41) and, • a detachable pin (15, 25, 45) engaging with said stud (11, 21, 41), said detachable pin (15, 25, 45) being configured, on the one hand, in a working position, to hold said stud (11, 21, 41) in position and to allow said panel to be secured to said support and, on the other hand, in a release position, to release said stud (11, 21, 41), - at least one link (16, 16') connected to said detachable pins (15, 25, 45) of said at least two ejector components (8, 8'), and - at least one control component (17, 27) for exerting a tensile force on said at least one link (16, 16') and for simultaneously arranging said detachable pins (15, 25, 45) of said at least two ejector components (8, 8') in their respective release positions, characterized in that said device comprises a frame configured to be secured to said support, said frame being interposed between said support and said panel, said springs of said at least two ejector components (8, 8') being respectively arranged between said frame and said panel. - a panel configured to be arranged at least opposite said opening, - at least two ejector components (8, 8'), each of said at least two ejector components (8, 8') comprising: • a stud (11, 21, 41) extending in a longitudinal direction oriented perpendicularly relative to said panel, • a compression pre-stressed spring in said longitudinal direction, said spring being coaxially arranged around said stud (11, 21, 41) and, • a detachable pin (15, 25, 45) engaging with said stud (11, 21, 41), said detachable pin (15, 25, 45) being configured, on the one hand, in a working position, to hold said stud (11, 21, 41) in position and to allow said panel to be secured to said support and, on the other hand, in a release position, to release said stud (11, 21, 41), • a stud (11, 21, 41) extending in a longitudinal direction oriented perpendicularly relative to said panel, • a compression pre-stressed spring in said longitudinal direction, said spring being coaxially arranged around said stud (11, 21, 41) and, • a detachable pin (15, 25, 45) engaging with said stud (11, 21, 41), said detachable pin (15, 25, 45) being configured, on the one hand, in a working position, to hold said stud (11, 21, 41) in position and to allow said panel to be secured to said support and, on the other hand, in a release position, to release said stud (11, 21, 41), - at least one link (16, 16') connected to said detachable pins (15, 25, 45) of said at least two ejector components (8, 8'), and - at least one control component (17, 27) for exerting a tensile force on said at least one link (16, 16') and for simultaneously arranging said detachable pins (15, 25, 45) of said at least two ejector components (8, 8') in their respective release positions, characterized in that said device comprises a frame configured to be secured to said support, said frame being interposed between said support and said panel, said springs of said at least two ejector components (8, 8') being respectively arranged between said frame and said panel.