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Abstract
Electronic Flight Display System certification can present wide challenges in showing compliance with many existing regulatory requirements. This paper provides a guidance for manufacturers, system integrators and airworthiness authorities for the design, integration, and approval of electronic flight displays for fixed wing transport aircraft. Discussion on various existing standards available for aircraft electronic displays with their means of compliance at various stages of system certification has been presented in this paper. Detailed failure hazards associated with the failure of display functions are also provided in the paper.
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References
- Genesys Aerosystem Inc. USA, Pilot Operating Guide and Reference IDU 680, 2016.
- Moir I., Seabridge A. and Jukes., Civil Avionics Systems, Second Edition, John Wiley and Sons Ltd, 2013.
- ARINC Specification 429, Mark 33, Digital Information Transfer System.
- Moir, I. and Seabridge, A., Design and Development of Aircraft System, Second Edition, John Wiley and Sons Ltd, 2016.
- Framework and Procedure for Design, Development and Production of Military Air System and Airborne Stores DDPMAS Ver 1.0, 2021.
- Cary Spitzer., Ferrell and Ferrell., Digital Avionics Handbook, Third Edition, 2015, CRC Press.
- SAE ARP 4102-7, Aerospace Recommended Practices: Electronic Displays, 2007.
- SAE AS 6296, Aerospace Standard: Electronic Flight Instrument System (EFIS) Displays, 2016.
- SAE AS 9034C, Minimum Performance Standard for Airborne Multipurpose Electronic Displays, 2018.
- RTCA DO-178B, Software Considerations in Airborne Systems and Equipment Certification, RTCA Inc.,Washington.
- RTCA DO-254, Design Assurance Guidance for Airborne Electronic Hardware, RTCA Inc., Washington.
- SAE ARP4754A, Guidelines for Development of Civil Aircraft and Systems, SAE, 2010.
- Ananda, C.M., Venkatanarayan, K.G., Preme, M. and Raghu, M., "Avionics Systems, Integration, and Technologies of Light Transport Aircraft", Defense Science Journal, Vol.61, No.4, July 2011, pp.289-298.
References
Genesys Aerosystem Inc. USA, Pilot Operating Guide and Reference IDU 680, 2016.
Moir I., Seabridge A. and Jukes., Civil Avionics Systems, Second Edition, John Wiley and Sons Ltd, 2013.
ARINC Specification 429, Mark 33, Digital Information Transfer System.
Moir, I. and Seabridge, A., Design and Development of Aircraft System, Second Edition, John Wiley and Sons Ltd, 2016.
Framework and Procedure for Design, Development and Production of Military Air System and Airborne Stores DDPMAS Ver 1.0, 2021.
Cary Spitzer., Ferrell and Ferrell., Digital Avionics Handbook, Third Edition, 2015, CRC Press.
SAE ARP 4102-7, Aerospace Recommended Practices: Electronic Displays, 2007.
SAE AS 6296, Aerospace Standard: Electronic Flight Instrument System (EFIS) Displays, 2016.
SAE AS 9034C, Minimum Performance Standard for Airborne Multipurpose Electronic Displays, 2018.
RTCA DO-178B, Software Considerations in Airborne Systems and Equipment Certification, RTCA Inc.,Washington.
RTCA DO-254, Design Assurance Guidance for Airborne Electronic Hardware, RTCA Inc., Washington.
SAE ARP4754A, Guidelines for Development of Civil Aircraft and Systems, SAE, 2010.
Ananda, C.M., Venkatanarayan, K.G., Preme, M. and Raghu, M., "Avionics Systems, Integration, and Technologies of Light Transport Aircraft", Defense Science Journal, Vol.61, No.4, July 2011, pp.289-298.