dipakpunde...
What is the ultimate purpose for this investigation?
Was this due to possible conductivity issues affecting some sort of precision in-system measurement?
I have asked several aerospace hydraulics systems experts around here what the purpose for this analysis could be... and they have all given me the "Whaaaaat???” followed by “Whhyyyy???" return questions. Fire-explosion, stray current arcing, arc-induced corrosion/pitting, electrical/electronic component failures [valves, pressure sensors, etc] due to arcing, etc… were all discussed. NO KNOWN problem’s in acft or missiles.
NOTE. Commercial aircraft usually have Phos-ester hydraulic fluids; while Military acft [my world] have synthetic hydrocarbon. General aviation still tends to pure hydrocarbon fluids.
Except for wire-braided flex hoses [Teflon lined], the vast majority of an aero-hydraulic system in an aircraft is metallic tubing, fittings, valves, etc that MUST be grounded to the aircraft. Any static charge will rapidly bleed away.
The primary problem with hydraulic system fire/explosion is high-compression of entrapped air [N2/O2/Ar2, etc] with flammable fluid [IE: dieseling effect]... which is the reason systems must be purged/filled with dry nitrogen.
Regards, Wil Taylor
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