IEC PAS 62396-3:2007

1 Scope and object
2 Normative References
3 Terms and definitions
4 Avionic Systems
  4.1 Lift control flap and slat
  4.2 Engine thrust
  4.3 Systems impacted by atmospheric radiation
      4.3.1 Aircraft system level
      4.3.2 Electronic equipment level
      4.3.3 Component level
  4.4 SEE at system level
      4.4.1 Hard errors and effects
      4.4.2 Soft error accommodation
      4.4.3 Component technology susceptibility
5 Optimisation of system design
  5.1 Avionic system optimisation
  5.2 Equipment level optimisation of soft error SEE
      5.2.1 SEE Detection
      5.2.2 Soft error accommodation, and error detection
            and correction
      5.2.3 Accommodation of non-destructive hard faults
  5.3 Component level optimisation of SEE
      5.3.1 Use of larger geometry atmospheric SEE tolerant
            parts
      5.3.2 Selective use of larger geometry atmospheric
            SEE tolerant parts
      5.3.3 Use of components not subject to hard faults or
            errors
      5.3.4 Use of components subject to non destructive
            hard faults or errors

Provides guidance to those involved in the design of avionic systems and equipment. Builds on the initial guidance on the system level approach to Single Event Effects in IEC/TS 62396-1, considers some avionic systems and provides basic methods to accommodate SEE so that system hardware assurance levels may be met.