It doesn't take much to induce a stress fracture in a prop, a tiny inclusion or micro bubble when molded an be enough. Once a stress riser is present, a cyclical loadin/ unloading can cause it to propagate quickly, resulting in failure.
For a while we had to pull the blades off the PW 120 powered Dash -8s every 100 hrs and have NDT inspections done on the blade root. Tiny points of corrosion in the taper bore where they packed lead wool to balance the blade weight would start a stress riser that could lead to a blade Fracture / Liberation in flight- Not Good! Took them months to get all the blades back to overhaul, but once certified by OEM, the 100 hr inspection went away. We got really tired of pulling props and blades every night.
The defect came to light when an EMB-120 spit a blade, the resultant severe vibration tore the engine gearbox/ prop from the rest of the engine before the crew could shut it down. The prop/ gearbox got lodged between the nacelle and fuselage causing severe drag and yaw. They tried toput it down in a field, but hit some trees about 1/2 mile short. No survivors, and one passenger was a congressman or something. EMB fleet grounded within a couple days, AD came out in record time, and subsequently spread to other aircraft with same basic blade design.
Don't miss that aspect of my former career one bit, your sphincter gets tight every time you do a post install vibration / Power Assurance run......