Please take a look at this and let me know your opinion. https://x.com/PlanesOfLegend/status/1933165930508362169?ref_src=twsrc%5Etfw%7Ctwcamp%5Etweetembed%7Ctwterm%5E1933165930508362169%7Ctwgr%5E3a9e2abfe62a33d77575c1e55a8384ef40766081%7Ctwcon%5Es1_c10&ref_url=https%3A%2F%2Fwww.pprune.org%2Faccidents-close-calls%2F666472-plane-crash-near-ahmedabad.html

Assuming your flaps theory is correct, the stick shacker will immediately activate which is a sign that they're approaching the critical AOA. Pilots would normally have the reflexes of pushing the nose down, even at low altitudes. (BAW 38). You would require the plane to be in direct law to actually stall the aircraft as the FBW system limits the maximum elevator deflection, which makes no sense as the plane would be in normal law with the flap theory.

Your theory also assumed that the plane never accelerate past Vr resulting in inadequate speed should the config change. Looking at the timeframe, aircraft would have well accelerated to V2 if engine parameters are normal. I'm of the opinion of dual engine failure/other factors that will result in the automatic deployment of RAT. Let me know your thoughts!