This could take different forms, but it is essentially a test of engine start up parameters of the fuel (methane) and/or oxidizer (lox) pumps. These pumps are powered by turbines which burn methane and lox, but this creates a chicken or the egg situation when starting an engine. If the pumps are off and the shaft is not spinning you have zero fuel or lox pressure, and you can't run the turbine without it. Did it spin first to get pressure to the turbine pump combustion chamber, or did they do some combustion first to get it to spin? Well, you spin it first by running a high pressure inert gas through the turbine, this spins the pump and create a little bit of fuel and lox pressure that is injected into the turbine pump combustor where it is ignited to power the pump's turbine. Once this happens, the turbine is off to the races and the pump outlet pressure and also combustion chamber inlet pressure rise rapidly bringing everything up to design operating point.
So spin start test implies they were testing this start up process and running their fuel or ox pumps, or both simultaneously. If the intent was to actually ignite the combustors that feed the turbines in the turbo pumps, it's a lot higher risk test, but something they've done before so probably had some confidence in whatever they were doing. This would be something they've done a lot on individual engines test stands and for static fire tests of the raptors they've already done a few times, but this was the first with the vehicle integrated with 33 engines I think.
Any number of things could be a cause. Too little information to speculate.