Solving for time directly requires solving a quadratic equation in time if the launch is asymmetrical for launch and landing (The solution for symmetrical launch is just 2vy0/g = tair)
Here you must solve y = y0 + vy0t - (1/2)gt2
8.08 m = 2.08m + (17.8 m/s * cos(64.5°))t - (1/2)(9.8 m/s2)t2 (t that solves this is tair)
The other way to solve this is to solve for vy using
vy2 = vyo2 - 2g(y-y0) then solve for t: t = (vy - vy0)/(-g)
This second way leads you through the quadratic equation without having to use it (at the cost of not solving for t directly)