I need to answer a question about a practical thing in aircraft design management...maybe you could help?
Here goes......during the design phase, for PDR, all the systems have to be integrated into the wing, engines, fuel lines, landing gear, wiring, flight controls, the whole lot that bolts onto the wing. The question is what interface project systems are used in reality to make sure for example all the integration checks are carried out. By system I mean an ISO or EASA AMC or perhaps SAE ARP4754 protocol to list out what should be done to check the matching of parts for all the reasons from galvanic action to vibration to interface gaskets, safety analysis, etc. I refer to the US or EU environment here to try to establish what compliance requirements might be cited in a compliance review for a Design organisation in the civil aircraft sector.
What to you do in reality to manage this? I used to use Do178 for avionics, mainly specifies the connector socket.
Any tips come to mind?
Much appreciated.
Here goes......during the design phase, for PDR, all the systems have to be integrated into the wing, engines, fuel lines, landing gear, wiring, flight controls, the whole lot that bolts onto the wing. The question is what interface project systems are used in reality to make sure for example all the integration checks are carried out. By system I mean an ISO or EASA AMC or perhaps SAE ARP4754 protocol to list out what should be done to check the matching of parts for all the reasons from galvanic action to vibration to interface gaskets, safety analysis, etc. I refer to the US or EU environment here to try to establish what compliance requirements might be cited in a compliance review for a Design organisation in the civil aircraft sector.
What to you do in reality to manage this? I used to use Do178 for avionics, mainly specifies the connector socket.
Any tips come to mind?
Much appreciated.