Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system
First Claim
1. A method of a calculation to determine real-time or by post processing the true aircraft braking friction coefficient based on the data collected by and available in the aircraft flight data management systems such as the Flight Data Recorder (FDR).
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Abstract
This invention relates to method and apparatus of the calculation of aircraft braking friction and other relating landing parameters including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system for example the Quick Access Recorder (QAR) to provide every involved personnel in the ground operations of an airport and airline operations including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.
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Citations
4 Claims
- 1. A method of a calculation to determine real-time or by post processing the true aircraft braking friction coefficient based on the data collected by and available in the aircraft flight data management systems such as the Flight Data Recorder (FDR).
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