Question for Cessna airframe techies...
I understand that the Cessna 152 Aerobat (A152) differs to the C152 (non-Aerobat) by being stronger, i.e. reinforced, in some areas, hence has a higher Vne etc.
Can anyway tell me exactly where the Aerobat is structurally different from the non-Aerobat? And if there are any other differences?
I've poured through the POHs of the two and can't find the answer.
Many thanks.