A galley cooling system (10) suitable for use in an aircraft comprises a trolley compartment (18) comprising a front side access opening (20), a back wall (22) arranged opposite to the front side access opening (20) and two sidewalls (24, 26). The galley cooling system (10) further comprises a cooling unit (12) adapted to provide a cooling fluid, wherein the cooling unit (12) comprises a cooling fluid outlet (16). A cooling fluid supply manifold (32) is connected to the cooling fluid outlet (16) of the cooling unit (12) and has a cooling fluid supply manifold wall (38; 38a, 38b) extending substantially parallel to at least one sidewall (24, 26) of the trolley compartment (18). A cooling fluid supply opening (40; 40a, 40b) is provided so as to supply cooling fluid provided by the cooling unit (12) to the trolley compartment (18).
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