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