I agree Tyler, Inconsistencies is a good term!
On a running engine, the level of the Oil tank can be quite generous.
The lower limit would be where the Oil Pump can no longer reliably draw the Oil UP to the pump.
The Upper limit would be where the Crankcase pressure becomes excessive in forcing the Oil back into the tank.
Both of these extremes are likely in excess of a few feet and well beyond the dimensions of any typical fuselage that would be power by a 912 series engine.
The Oil tank position limits on a stopped engine are quite a bit more limited.
While a stopped Oil pump presents a nearly total blockage to any oil flow, given enough time some amount will flow and it is only prudent to assume that ALL the Oil that Can possible flow, Will eventually Flow.
As long as the Oil level in the tank is above the Oil pump inlet, the Inlet hose will not drain, causing the Oil pump to lose its prime. Making the center of the Oil Pump a practical lower limit.
The upper limit would need to be restricted to the point that if the Oil were to drain into the crankcase to the point of equilibrium, there would still be enough Oil remaining that on the initial engine start, enough of the Oil in the crankcase would begin returning to the Oil tank before the Oil pump had sucked the tank dry. Making the Center of the Prop Shaft a somewhat arbitrary but Practical Upper Limit.
It is a good practice to "Burp" the Engine, or at least turn the prop through one revolution to confirm there is not an undue amount of Oil in the crankcase or cylinders before any start where more than ~18 hours has passed since shutting down. Unless there is a puddle of Oil under the plane, it is not absolutely necessary to check the Oil Level as much as it just a good idea to rotate the prop.