TyroGyro
Junior Member
- Joined
- Sep 30, 2016
- Messages
- 651
- Location
- near Liverpool, UK
- Aircraft
- MTOsport G-IROD
- Total Flight Time
- 160
It seems to me the report is saying the rotor head design and fabrication could and should have been stronger:-Tyro
The rotor head failure was most likely fundamentally due to low hour student mishandling.
There may also be a design/material choice question but since all the other Cavalons of the same generation aren't falling out of the sky I'd say that this was an hour's/training issue.
Mike
"While not causal to the accident, a key element of the failure sequence of the gimbal block was the failure of the welds holding the roll stop bar in position. Rather than being structural welds, they effectively just located the bar in position and failed under a relatively low load.Theoretical analysis showed that had full strength welds been used, they would have remained intact under a much greater load, the roll stop bar would then not have started to deform at a low load, maintaining an even distribution in the load transferred to the gimbal block and allowing the combined structure to support a load greater than that which failed the block in the practical test."