A basic magneto drop-off check
based on engine speed is typically done during the pre-flight inspection to determine the loss of engine speed that occurs when magnetos are switched from BOTH magnetos to one (LEFT or RIGHT) magneto. The maximum drop-off limit is specified in most Lycoming publications as Revolutions Per Minute (RPM) from a stated engine speed.
Although this basic drop-off check, based on just engine speed, is satisfactory under most normal conditions, it does not take into account unusual circumstances of temperature, humidity, and engine wear. In those cases, use the following procedure to measure the magneto drop-off as a ground check based on manifold pressure on Lycoming opposed series aircraft engines equipped with a manifold pressure gage or a constant speed propeller. This procedure will be incorporated in all new editions of Lycoming Operator’s Manuals.
A proper magneto check is important. Additional factors, other than the ignition system, affect magneto drop-off.
They are load-power output, propeller pitch, and mixture strength. The important point is that the engine runs smoothly because magneto drop-off is affected by the variables listed above. Make the magneto check in accordance with the following procedures
b) (Fixed pitch propeller). Aircraft that are equipped with fixed pitch propellers, or not equipped with a manifold pressure gage,
may check magneto drop-off with the engine operating at approximately 1800 RPM (2000 RPM maximum).
https://www.lycoming.com/sites/default/files/Magneto Drop-Off.pdf
For your just barely ground run up, clean and gap the plugs every 50 hours and lean during taxi.