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Adams flexbody distributed forces

Hello,
 
I have an flexible MBD model of an airctaft and a loadcase for air pressure in the form of distributed loads normal to the aircraft elements. I understand that using modal forces I can insert the load to the flexbody but only direction-wise i.e., if the load acts in all three coordinates, I 'd have to specify the load for each one.
 
However I only have the distributed load in the form of it beeing normal to each element. Is there a way to instert this load to Adams directly or must I find a way to break the load down to three components and insert them individually?
 
Thanks,
 
Josef K.