Abstract: A system to filter a data transfer between an external application and a component of a vehicle, includes: a failsafe validation engine, wherein the failsafe validation engine includes: a rules engine to process a data model from the external application based on one or more rules, a context analyzer to receive context data associated with the vehicle, process the context data as the one or more rules, and send the one or more rules to the rules engine, and a schematic parser to receive the data model from the rules engine and parse the data model based on one or more object models defined for the component of the vehicle; and a controller to control the failsafe validation engine.

Abstract: Methods and systems for providing platform agnostic flight management data access for a flight management system (FMS) of an aircraft have been developed. First, a configuration file is loaded to a configuration database. The configuration file is for a data format of an external data source from the aircraft. Upon receiving a data access request from a user for external data from the external data source, downloading the configuration file is downloaded to an FMS data formatter. The configuration file is parsed with a data processor component of the FMS data formatter to update a rule set. The FMS data formatter receives an external data file from an application programing interface (API) of the external data source. The external data file is parsed with a rule engine of the FMS data formatter using the updated rule set. A flight plan file is generated with the FMS data formatter using the parsed external data file and sent to the FMS on the aircraft.

Abstract: Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.

Abstract: Disclosed are methods and systems for bi-directional communication between one or more vehicles and a cloud based computing system. For instance, a method may include processing, by a first digital twin of the cloud based computing system, a first request received from and/or sent to a gateway unit associated with a first vehicle, the request comprising data related to one or more vehicle operations; validating, by an avionics data processing service (ADPS) in communication with the gateway unit, the first request against an operational parameter corresponding to the one or more vehicle operations; upon validating the first request, matching, by the ADPS, the operational parameter with a flight operation; and upon matching the operational parameter with the flight operation, inserting, by the ADPS, a modified flight operation into the flight management system of the vehicle.

Abstract: A system and method in an aircraft for providing enhanced services is provided. In one example, the method includes: setting up triggering logic to identify a beginning point and ending point for collecting a set of avionics system data during a flight; and systematically retrieving information for use by the triggering logic to identify the beginning point and the ending point. When the beginning point is reached, the method includes systematically repeating: retrieving the set of avionics systems data; and sending, to an off-board application, data from the set of avionics system data that has changed state from prior data sent to the off- board application. When the ending point is reached, the method includes cease sending data from the set of avionics system data to the off-board application.

Abstract: A computer-implemented method for integration of data into flight data monitoring comprises receiving quick access recorder data from an aircraft; receiving flight management system data from the aircraft; combining the quick access recorder data and the flight management system data to form combined data; and displaying the combined data on a user device.

Abstract: Methods and systems are provided for flight management system (FMS) familiarization training. The system comprises a user application programming interface (API) that receives a request for a training scenario from a user. A flight management engine (FME) generates the training scenario that simulates the flight mission of an FMS onboard a designated aircraft. The training scenario is generated using the same algorithms as the FMS. A database configuration module retrieves performance and condition data that is provided to the FME for use in generating the training scenario. An external API retrieves external third-party data that is provided to the FME for use in generating the training scenario.