Abstract: A method in an aircraft of using prognostic indicators for aircraft maintenance includes retrieving aircraft health data for a plurality of aircraft components wherein the aircraft health data includes at least one of mechanical systems condition indicator (CI) data, vibration spectrum data, resampled time-domain (RTD) data, and RTD spectrum data. The method includes estimating component health status information for the plurality of aircraft components using a plurality of prognostic modules wherein each prognostic module is configured to generate health status information for at least one of the aircraft components, the health status information includes at least one of a current health indicator and a prognostic indicator. The method also includes storing the component health status information for the aircraft components in a database onboard the aircraft, and causing the display of the health status information for the specific component on an aircraft display.

Abstract: A method in an aircraft of using prognostic indicators for aircraft maintenance includes retrieving aircraft health data for a plurality of aircraft components wherein the aircraft health data includes at least one of mechanical systems condition indicator (CI) data, vibration spectrum data, resampled time-domain (RTD) data, and RTD spectrum data. The method includes estimating component health status information for the plurality of aircraft components using a plurality of prognostic modules wherein each prognostic module is configured to generate health status information for at least one of the aircraft components, the health status information includes at least one of a current health indicator and a prognostic indicator. The method also includes storing the component health status information for the aircraft components in a database onboard the aircraft, and causing the display of the health status information for the specific component on an aircraft display.

Abstract: A method in an aircraft of using prognostic indicators for aircraft maintenance includes retrieving aircraft health data for a plurality of aircraft components wherein the aircraft health data includes at least one of mechanical systems condition indicator (CI) data, vibration spectrum data, resampled time-domain (RTD) data, and RTD spectrum data. The method includes estimating component health status information for the plurality of aircraft components using a plurality of prognostic modules wherein each prognostic module is configured to generate health status information for at least one of the aircraft components, the health status information includes at least one of a current health indicator and a prognostic indicator. The method also includes storing the component health status information for the aircraft components in a database onboard the aircraft, and causing the display of the health status information for the specific component on an aircraft display.

Abstract: Systems and methods for improving the reception and delivery of an In-Trail Procedures (ITP) altitude change request. An example system located on board a host aircraft includes a communication component, a display device and a processor unit that is in signal communication with the communication component and the display device. The processor unit presents a user interface on the display device. The user interface includes a plurality of fields for receiving In-Trail Procedures (ITP) altitude change request information. The processor sends the ITP altitude change request information received within the plurality of fields to an Air Traffic Control (ATC) facility via the communication component. An ITP unit having a display receives an altitude selection and presents ITP altitude change request information if the received altitude selection is determined to be valid.

Abstract: Systems and methods for improving the reception and delivery of an In-Trail Procedures (ITP) altitude change request. An example system located on board a host aircraft includes a communication component, a display device and a processor unit that is in signal communication with the communication component and the display device. The processor unit presents a user interface on the display device. The user interface includes a plurality of fields for receiving In-Trail Procedures (ITP) altitude change request information. The processor sends the ITP altitude change request information received within the plurality of fields to an Air Traffic Control (ATC) facility via the communication component. An ITP unit having a display receives an altitude selection and presents ITP altitude change request information if the received altitude selection is determined to be valid.

Abstract: The generation of contour plot images from elevation data in real time for use in a digital moving map. The contour line interval is dynamically selectable. The elevation data is scanned in 2 dimensions simultaneously, but in a single pass. As the elevation data is scanned for the given contour line interval, a history is maintained of the contour line elevation state in both dimensions. At any point, only comparisons against the two historical values are required to determine if a point on a contour line exists.