I've never checked this on an automotive motor, but on an airplane motor, specifically a Lycoming IO-360, there IS a difference in readings between the front tap and the rear tap. Here is my experience... I had a new (in 2003) electronic engine monitor installed on my airplane. I noticed afterward there was a difference in oil pressure readings between the electronic monitor and the the original oil pressure gauge, which was a mechanical gauge using a copper capillary tube. I asked the mechanic who installed the monitor about it, and he said he had to use the front tap for the oil pressure sender for the monitor, because the rear tap was already taken up by the original mechanical gauge tube and there wasn't room to use a tee (translation: "I was too lazy to re-work the rear tap set-up."). I asked why the difference in pressures, and he said as the oil moves through the galleys from the rear of the engine to the front, it loses pressure. He said it was "perfectly normal." Intuitively, that made sense to me, but I called Lycoming just to make sure. They said, "yep, that's normal." At take-off power (2,700 rpm), the rear tap was reading 70 psi, and the front tap was reading 55 psi.
I'm just sayin'...