SE024 DIP – Aircraft Design

SE024 DIP – Aircraft Design

Detailed Implementation Plan for

SE-24 Approach and Landing Accident Reduction (ALAR) Aircraft Design – Continuing Airworthiness

Statement of Work

The purpose of this project is to promote incorporation of fault tolerant design principles for flight critical system components and to facilitate critical-point, flight-realistic-condition, certification testing/analysis. Changes to flight critical system components will be considered a major change unless the applicant can show the change is in fact a minor change and monitors the continued airworthiness (in-service failures) of these systems using a risk assessment focused methodology.

Detailed Implementation Plan

Related Safety Enhancements

Related Outputs

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