Sheared Propeller Bolts
After rollout, I pushed the glider off the runway and inspected the prop. All four bolts had sheared off behind the gearbox flange. The prop was retained only by the feathering rod and lever! I was surprised to see that there is no mechanical "key" to lock the prop to the gearbox flange and that all of the engine torque is reacted through shear loads on the four bolts.
I had installed new nuts and bolts and torqued them to the value specified in the Heavy Maintenance Manual and I'm mystified as to why they sheared. Is it possible to install the propeller in the wrong "clock" position? I did not find guidance on the angle of the propeller with respect to the prop flange.
A final question: would it be OK to use higher strength bolts to reinstall the propeller (after inspection/repair)?