1. A method for identifying anomalies for an aircraft, the method comprising: detecting a presence of the aircraft in a control area via monitoring, using a sensor system, the aircraft characterized by a first side, a second side, and a bottom; responsive to the sensor system detecting the presence of the aircraft in the control area, identifying, using a number of array encoders, a speed of travel for the aircraft; determining a scan rate for the aircraft using the speed of travel, wherein the scan rate is a number of electrical signal pulses sent to a number of cameras resulting in the number of cameras taking an exposure of at least a portion of the aircraft on each of the number of electrical signal pulses; identifying, using a maintenance control system comprising a computer comprising an analysis process comprising an object identifier, the aircraft; responsive to identifying the aircraft, identifying, using the analysis process and a scan priority database comprising a hierarchy of anomaly priorities, a number of scan priorities for the aircraft on the ground after a flight, wherein the number of scan priorities ranks different sections of the aircraft to be sought out during a scan based on information comprising operational maintenance information about the aircraft; determining whether the analysis process received a datalink communication, identifying an anomaly with a section of the aircraft, from the aircraft during the flight; assigning a first priority to the anomaly identified in the datalink communication, and responsive to receiving identification of multiple anomalies, identifying prioritization of the multiple anomalies received in the datalink communication based upon a hierarchy of anomaly priorities within a scan priority database communicating with the analysis process; identifying prior scan results for the aircraft; determining, using the analysis process and the prior scan results, whether an anomaly trend exists; responsive to a determination that the anomaly trend exists, assigning a second priority to the anomaly trend; determining, using a designated use for each sensor in the sensor system and a potential for degradation of each sensor influenced by dynamic conditions comprising: a cloud coverage, an artificial illumination, a full moon light, a new moon darkness, a degree of sun brightness based on sun position due to season, a shadow, fog, smoke, sand, dust, rain, and snow, a number of redundant sensors in the sensor system used in scanning the aircraft; responsive to identifying the number of scan priorities for the aircraft, scanning the aircraft, using the scan rate and a number of sensor components in an array in accordance with the number of scan priorities, the array including at least a horizontal array of sensors directed at the bottom of the aircraft and an angled array of sensors directed at the first side of the aircraft; and responsive to scanning the aircraft, using the analysis process for forming scan results and determining whether a number of maintenance anomalies is present among a set of locations for the aircraft, the set comprising: inside the aircraft, on an exterior surface of the aircraft, on an interior surface of the aircraft, and within a structure comprising the aircraft; responsive to determining that the number of maintenance anomalies is present for the aircraft, generating a maintenance action to address the number of maintenance anomalies detected, transmitting the maintenance action to a maintenance unit, and executing the maintenance action on the aircraft.