Some of the info is here (3rd link down)
electrical load
I have not confirmed everything on flight testing, but at runup, with lights on, fuel pump on, avionics on (basically full load except flaps), I see about 16-18 amps, which matches the spreadsheet.
No load, I see 3-5 amps, which is battery charging current, field current and avionics on receive/standby. If the battery is low, this current increases.
No info on the primer pump, since it's not (normally) used in flight.
Vern Little
9A