I can’t say for sure but it seems highly unlikely that the elevator/stab, however configured, could produce enough aerodynamic force at 60kts to put the tail on the tarmac if the CofG was inside the envelope.
That said, if there was a strong headwind, the temperature was ISA-40 or below and the the quoted 60kts was groundspeed, then the equivalent IAS could be closer to 100kts, at which point all bets are off...