Abstract: An example avionic data communication method includes determining one or more available communication channels within a plurality of communication channel types, selecting one of the plurality of available communication channels using a channel controller, the channel controller configured to determine the quality of service of the available communication channels and to select one of the plurality of available communication channels having a cost threshold value that is not less than the cost threshold value of another channel type within the plurality of available channel types. The method further includes communicating data between an aircraft and a ground-based system using the selected one of the plurality of available channel types.

Abstract: A system and method for managing a vehicle is provided that includes at least one sensor, a certified processor, a database, a computer network, and a user portal. The at least one sensor is operable to generate data indicative of a critical condition of the vehicle. The certified processor in communication with the computer network and is operable to receive, process and store the data generated by the at least one sensor. The database is in communication with the computer network and is operable to selectively download and store a replica of the data stored on the certified processor via the computer network. The user portal is in communication with the computer network and is operable to enable a user to download, via the computer network, selected portions of the data stored on the certified processor or selected portions of the replica data stored on the database.

Abstract: An example avionic data communication method includes determining one or more available communication channels within a plurality of communication channel types, selecting one of the plurality of available communication channels using a channel controller, the channel controller configured to determine the quality of service of the available communication channels and to select one of the plurality of available communication channels having a cost threshold value that is not less than the cost threshold value of another channel type within the plurality of available channel types. The method further includes communicating data between an aircraft and a ground-based system using the selected one of the plurality of available channel types.

Abstract: An example avionic data communication method includes establishing a plurality of available channels using a channel controller. The channel controller also establishes a quality of service for each of the plurality of available channels. The channel controller then selects one of the available channels. The quality of service of the selected channel is not less than the quality of service of another channel within the plurality of available channels. The method then communicates a type of data using the selected channel.

Abstract: A system and method for managing a vehicle is provided that includes at least one sensor, a certified processor, a database, a computer network, and a user portal. The at least one sensor is operable to generate data indicative of a critical condition of the vehicle. The certified processor in communication with the computer network and is operable to receive, process and store the data generated by the at least one sensor. The database is in communication with the computer network and is operable to selectively download and store a replica of the data stored on the certified processor via the computer network. The user portal is in communication with the computer network and is operable to enable a user to download, via the computer network, selected portions of the data stored on the certified processor or selected portions of the replica data stored on the database.

Abstract: An aircraft component assembly has an aircraft component for an aircraft. A sensor is configured to monitor the aircraft component. A local wireless transmitter is provided for communication with a remote receiver. In addition, a local wireless receiver is provided for communication with the remote transmitter. A processor is in communication with the sensor. The processor is configured to control the sensor, the local wireless transmitter and the local wireless receiver. A power source is configured to generate energy proximate the installed aircraft component.

Abstract: A method of exposing and recording embedded avionics data using dynamically assigned labels assigns a first plurality of data labels to aircraft controller parameters designated for at least one aircraft sub-controller. A second plurality of data labels are dynamically assigned to desired embedded parameters of an aircraft main controller. At least one data word storing one of the desired embedded parameters is created. The at least one data word has one of the second plurality of data labels. The at least one data word is exposed by transmitting the at least one data word to a selective recording device. The selective recording device records the at least one data word.

Abstract: The example avionic data communication management arrangement includes a common infrastructure having a first account and a second account. The first account is configured to receive and store avionic data collected from a first aircraft. The second account is configured to receive and store avionic data collected from a second aircraft that is from a different airline than the first aircraft. The avionic data within the first account and the avionic data within the second account can both be accessed or managed by an administrating entity.

Abstract: An example avionic data communication method includes establishing a plurality of available channels using a channel controller. The channel controller also establishes a quality of service for each of the plurality of available channels. The channel controller then selects one of the available channels. The quality of service of the selected channel is not less than the quality of service of another channel within the plurality of available channels. The method then communicates a type of data using the selected channel.

Abstract: A method and system is provided for updating a sensor disposed within a mobile unit. The method includes the steps of: a) providing a remote server and at least one sensor, which remote server and sensor are located in the mobile unit and are in communications with one another through a first wireless network, and wherein the sensor has a first functionality; b) receiving an update signal transmitted from a base server to the remote server over a second wireless network; c) transmitting the received update signal from the remote server to the sensor over the first wireless network; and d) reconfiguring the sensor from the first functionality to a second functionality based upon the transmitted update signal.

Abstract: An example method of verifying avionic data includes establishing a first cyclical redundancy check value associated with a data file. The first cyclical redundancy value is established on an aircraft. The method transmits the data file from the aircraft to a ground system. The method receives a second cyclical redundancy check value associated with the data file. The second cyclical redundancy check value is established by the ground system. The method determines the transmitted data file integrity by comparing the first cyclical redundancy check value to the second cyclical redundancy check value. An example aircraft avionic data verification arrangement includes a collector device that assembles avionic data into a data file that is transmittable to a ground system.

Abstract: Systems and methods for communicating aircraft data are provided. In this regard, a representative system includes a data reduction system operative to: receive aircraft data; store a first set of the aircraft data; analyze a next set of the aircraft data; and store the next set of the aircraft data if the next set of aircraft data differs from the first set of the aircraft data.

Abstract: A method of exposing and recording embedded avionics data using dynamically assigned labels assigns a first plurality of data labels to aircraft controller parameters designated for at least one aircraft sub-controller. A second plurality of data labels are dynamically assigned to desired embedded parameters of an aircraft main controller. At least one data word storing one of the desired embedded parameters is created. The at least one data word has one of the second plurality of data labels. The at least one data word is exposed by transmitting the at least one data word to a selective recording device. The selective recording device records the at least one data word.

Abstract: A method of aircraft maintenance involves storing part information relating to an aircraft part on the aircraft part. The part information is wirelessly transmitting from the aircraft part to a receiver. A note of a change relating to the aircraft part is made. The part information with the note of the change relating to the aircraft part is electronically stored at a location remote from the aircraft part.

Abstract: A method and system is provided for updating a sensor disposed within a mobile unit. The method includes the steps of: a) providing a remote server and at least one sensor, which remote server and sensor are located in the mobile unit and are in communications with one another through a first wireless network, and wherein the sensor has a first functionality; b) receiving an update signal transmitted from a base server to the remote server over a second wireless network; c) transmitting the received update signal from the remote server to the sensor over the first wireless network; and d) reconfiguring the sensor from the first functionality to a second functionality based upon the transmitted update signal.

Abstract: An example method of communicating with an aircraft includes receiving a text message with an aircraft avionics box and initiating an operation with the aircraft avionics box based on the text message.

Abstract: Systems and methods for communicating aircraft data are provided. In this regard, a representative system includes a data reduction system operative to: receive aircraft data; store a first set of the aircraft data; analyze a next set of the aircraft data; and store the next set of the aircraft data if the next set of aircraft data differs from the first set of the aircraft data.

Abstract: A method for monitoring information of at least one unemployed aircraft components includes monitoring information relating to each of the unemployed aircraft components, transmitting the information from each location of each the unemployed aircraft components to a remotely located central control, and collecting the information in a computer-readable medium associated with the central control to thereby provide remote access of the information.

Abstract: A method of aircraft maintenance involves storing part information relating to an aircraft part on the aircraft part. The part information is wirelessly transmitting from the aircraft part to a receiver. A note of a change relating to the aircraft part is made. The part information with the note of the change relating to the aircraft part is electronically stored at a location remote from the aircraft part.

Abstract: An aircraft component assembly has an aircraft component for an aircraft. A sensor is configured to monitor the aircraft component. A local wireless transmitter is provided for communication with a remote receiver. In addition, a local wireless receiver is provided for communication with the remote transmitter. A processor is in communication with the sensor. The processor is configured to control the sensor, the local wireless transmitter and the local wireless receiver. A power source is configured to generate energy proximate the installed aircraft component.