There is a torque setting for every single fastener with a thread in an aircraft. Either a general one for that thread pitch and diameter of fitting, or a more specific one for a lot of the higher stress and critical parts. Even screw terminals have a torque setting, it is not a Gutentight spec, but a specific setting for each one. That is why every aircraft maintenance bay has a row of calibrated torque testers on the floor, so that every fastener that is put in has the correct value applied. Looks like here though that there is a culture of do it fast, and self inspection, or in reality no inspection. As it is rather well known that there is lax QC, I would say that there is a bigger issue, in that nothing that has come out of this assembly line for the last decade is going to be good, just that the redundancies are keeping them together.
Seems the cost cutting of dumping those expensive people, the ones with knowledge, degrees and 20 years of work experience, and replacing them with people earning minimum wage, because the suits think that assembling an aircraft is no different than flipping a burger at the golden arches, and anybody with a pulse can do it. That the product from the arches does not resemble the pictures in the ad, is not thought by the suits to be important, but when you have no option to return and tell them to make it again, because you have now made a large hole in the ground, this is not really good.