Module monitor unit for an electric aircraft battery pack and methods of use

An electric aircraft battery module comprising:

• a first monitor module unit (MMU), the first MMU comprising:
• a housing attached to a battery module of an electric aircraft, the battery module comprising a battery cell;
• a control circuit at least partially disposed within the housing, the control circuit configured to:
• receive a measurement datum of a battery module from a communicatively connected sensor;
• determine an operating condition of the battery module;
• and
• generate an action command to provide a control operation of the battery module as a function of the operating condition;
• transmit a current operation condition to a first pack monitoring unit (PMU), wherein the first pack monitoring unit is communicatively connected to the first MMU;
• and
• a second MMU, the second MMU configured to transmit the current operation condition to a second PMU, wherein the second PMU is communicatively connected to the second MMU. .