Abstract: A fire suppression system for aircraft storage containers includes a fire suppression unit removably located within each cargo container and a human to machine interface (HMI) located in the aircraft cockpit. Each fire suppression unit includes an identifier so that each unit is identified and correlated with its container. The HMI monitors each fire suppression unit including monitoring internal temperature, presence of chemical fumes, presence of smoke, presence of flammable gases, and presence of fire. Each fire suppression unit is programmed with specific thresholds of temperature, chemical fumes, smoke, and/or flammable gases, whereby when a threshold is reached activation of fire suppression means within the fire suppression unit is accomplished.