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EASA AD No.: 2012-0236R1 EASA AIRWORTHINESS DIRECTIVE AD No.: 2012-0236R1 Date: 17 December 2012 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC)
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Navigation angle of attack is the angle between the maximum camber line of the airfoil and the chord line of an aircraft, specifically in the context of navigation and flight control systems.
The aviation authorities and relevant regulatory bodies require aircraft manufacturers and operators to file navigation angle of attack data as part of their compliance with safety and performance regulations.
To fill out the navigation angle of attack, aircraft manufacturers and operators need to use advanced instrumentation and sensors to measure the angle accurately during flight. The data is then recorded and documented for reporting purposes.
The purpose of tracking navigation angle of attack is to monitor and analyze the aerodynamic behavior of an aircraft during flight. This information helps in ensuring the safety, stability, and efficiency of the aircraft's navigation and flight control systems.
The reported navigation angle of attack typically includes the timestamp, altitude, airspeed, and the corresponding angle values measured during specific phases of flight or as required by the regulatory guidelines.
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