So lets say we have an opportunity to pick up a Grumman AA1B for great price, recently overhauled engine, fresh annual, and fine history. Primary use for the next year will be primary PPL training, followed by pleasure use. This would be replacing the current C150. Gaining useful load, a few knots, and the pluses listed above.
Note that due to changes in the landing gear, the AA-1B has 60 lb more max gross weight than the earlier AA-1/1A, without being significantly heavier. This could be a big deal for flight training, so choosing a B-model is a good thing. But check the actual W&B on the plane and do
not exceed MGW or your takeoff/climb performance will disappear completely.
Also, I wouldn't recommend a stock AA-1-series plane for flight training at higher DA's -- for that, you'd want one of the AA-1x's STC'd with an O-320 engine. You don't get a significant increase in payload, but takeoff/climb performance improves spectacularly. I see you're in Maryland, so that shouldn't be an issue unless you're flying out of Garrett County in the summertime.
What can ya'll tell me about flight characteristics and handling?
Light, responsive, quick, and crisp. No tolerance for being sloppy or off the correct speeds on approach/landing. IOW, it makes you be a better pilot, and rewards you for being such. Getting a checkout from an AYA PFP Instructor would be a very good idea, especially one of the more experienced ones who've seen enough type-specific student mistakes to give you an instructor-oriented checkout.
I've read that spins can quickly become unrecoverable, so don't.
Not exactly true, but intentional spins are indeed prohibited, so don't. However, if you do mishandle it at the stall, it will recover promptly from an inadvertent
incipient spin (that is, up to 3 seconds or one turn) by application of proper anti-spin controls as described in the aircraft manual, and was so tested during certification.
However, if you accidentally spin it and don't initiate recovery within 3 turns, it can go flat on you, blanking the rudder, and then recovery becomes a lot trickier and takes a lot more altitude, so don't. But if you do get into that situation, try using ailerons full
with the spin to generate some adverse yaw to counter the rotation of the spin. No guarantees on this working, but it was done once to my knowledge. I warn you, however, that the idiot who intentionally tried this entered the spin at 12,500 and recovered at 1,500.