The present invention relates to an aircraft firewall (12) separating first and second compartments (1 and 2) of the aircraft, the first compartment (1) containing a plurality of elements. The firewall (12) is provided with a first wall (3) inserted in the structure (5) of the aircraft and having a first surface (3') facing the first compartment (1), and the firewall (12) is provided with regulator elements (4, 13) for maintaining the maximum temperature of the first surface (3') of the first wall (3) at a predetermined temperature value lower than the self-combustion temperature of the elements.
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