I'm surprised when I find counter discussions on topics that are so blatantly obvious...
The aeroplane may not be Rolling around it's axis, but it is YAWING around it's centre of gravity.
This is applying a centrifugal force at all four extremities, that gains intensity as you move away from the centre in the four directions.
The aircraft probably has wet wing tanks along most of their span, add that to a reasonable amount of dihedral, and it is possible to have fuel sitting in the root area (keeping the engine running), as well as fuel travelling towards the tips and exiting via the vents.
The three points they are testing/making here are;
1. largish fuel load in a spin not having a serious affect on yawing momentum, which would delay recovery,
2. With four passengers on board, the aircraft is possibly closer to it's rearward CofG, which would delay recovery,
3. The four occupants are reasonably spread fore and aft which can also add to the yawing moment, as well as giving a tendency for the spin to go flat, which could put the aircraft into a deep stall situation, often very hard to recover from.
Looks like the high aspect wings and long tail moment have added to the overall stability of the plane.
ps, Yes, it's fuel......