• AIR6110

• 2011-12-16

• S-18, Aircraft And Sys Dev And Safety Assessment Committee

This AIR describes, in detail, a contiguous example of the aircraft and systems developmentfor a fictitious aircraft design. In order to present a clear picture, an aircraft function was brokendown into a single system. A function was chosen which had sufficient complexity to allow use ofall the methodologies, yet was simple enough to present a clear picture of the flow through theprocess. This function/system was analyzed using the methods and tools described in the body ofthis ARP document. The interaction of the braking system functions with the aircraft are identifiedwith the criticality identified based on implied aircraft interactions and system availabilities at theaircraft level. This example does not include validation and verification of the aircraft level hazardsand interactions with the braking system. However, the principles used at the braking system levelcan be applied at the higher aircraft level (departing runway). The methodologies applied here arean example of one way to utilize the principles defined in ARP4754A. The basic ARP4754A document contains information which places the information in this appendix in context. This AIR should be used in conjunction with the main body and the other appendices of the ARP4754A. In addition, this example shows the interrelationships with ARP4761.

• SAE AIR 6110

• Aerospace

• Reliability Maintainability Supportability
• Safety
• Accident prevention
• Risk assessments
• Aircraft
• Commercial aircraft