We are looking to take one of your RevPi Compacts to flight test (it will be a none critical component so don't panic!!). To support his work we need to provide some evidence that the system is sufficiently robust to meet the requirements which fall in to the categories given below. Whilst we acknowledge that the system will never be fully certified for flight we would like some confidence that there is a good chance it will work for the duration of the flight test campaign. I have seen previous posts about certification that gives general information about testing to the general requirements EN61131-2 but any more specific information would be gratefully received.
General areas covered are given below and includes comments based on information I could find:
Temperature - I have used your information to say the operational range is -20C to +55C (storage -40C to +85C)
Humidity - max 93% assuming none condensing
Altitude - ?
Vibration - ?
Power interruption - ? Our specification is 200ms but this might be beyond the system capabilities given previous comments
Shock/Impact/Crash - ?
Voltage spike susceptibility - ?
Radio Susceptibility and Emissions - ? I have seen 2014/30/EU mentioned but is there specific information?
Lightning - ?