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Screenshot of a page of the A320 enhancements document - Within Safety Beyond Standard initiative, ELAC B L104 standard is developed to reduce the threat of Loss of Control In-flight, by enhancing the flight envelope protections availability. The ELAC B L104 standard introduces the following main SBS functions: - Addition of the Pitch Attitude Limitation in Alternate Law (PALAL) for all CEO/NEO, except A318: pitch positive angle limitation is available in alternate law, in clean configuration with settings function of altitude. Stall potential situation is thus delayed in case of inappropriate pitch-up inputs; - Flight envelope protections kept in case of system failures: in case of dual loss of yaw damper or dual loss of Flight Augmentation Computer (FAC), flight envelope protections are kept available, ALTN LAW is still displayed on Electronic Centralized Aircraft Monitoring (ECAM) as protections efficiency is reduced.
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📆📆 Created At
2025-11-29T14:30:18.643Z
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📜📜 Alt Text / Comment
Screenshot of a page of the A320 enhancements document - Within Safety Beyond Standard initiative, ELAC B L104 standard is developed to reduce the threat of Loss of Control In-flight, by enhancing the flight envelope protections availability. The ELAC B L104 standard introduces the following main SBS functions: - Addition of the Pitch Attitude Limitation in Alternate Law (PALAL) for all CEO/NEO, except A318: pitch positive angle limitation is available in alternate law, in clean configuration with settings function of altitude. Stall potential situation is thus delayed in case of inappropriate pitch-up inputs; - Flight envelope protections kept in case of system failures: in case of dual loss of yaw damper or dual loss of Flight Augmentation Computer (FAC), flight envelope protections are kept available, ALTN LAW is still displayed on Electronic Centralized Aircraft Monitoring (ECAM) as protections efficiency is reduced.
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