Total number does nothing to back up your statement- "Still much safer than many other forms of transport. "
Look up some comparison, like fatalities/passenger mile. I bet you'll find that putting you foot aboard a helicopter is like stepping into a grave with the other foot on a banana peel.
Fixed wing pilots call helicopters "10,000 parts all flying in close formation" for a reason. They are just waiting to break formation.
I used to have a PPL, and I wouldn't go in a helicopter if I could reasonably avoid it (I've had four helicopter flights - two military and two commercial - and I don't plan to have many more).
My father was a military fighter pilot and he wouldn't go anywhere near a helicopter.
There's a very good set of reasons why fixed-wing pilots are reticent about helicopters in comparison to fixed-wing:
1) Helicopters are inherently aerodynamically unstable: there is virtually no aerodynamic lift generated in forward (or stationary) flight other than that developed by the powered rotation of the main blade. If the main blade fails, you're in big trouble.
2) There's zero redundancy. If anything in the main rotor mechanism - whether powerplant, gearbox, drive or rotor set - fails, then the whole machine fails. By contrast, almost all aircraft are capable of safe flight with single engine failure.
3) There's an added potentially-catastrophic failure point for nearly all helicopters, and that's failure of the tail rotor. Even if the main rotor is fine, a tail rotor failure will almost-inevitably cause uncontrollable counter-rotation, and an uncontrolled descent. Therefore, it can be said that a failure of
either of the rotor sets of a helicopter could well cause a catastrophic loss of stable flight. Those aren't great odds......
4) The angle of attack of helicopters in failure tends to be very steep and high-velocity, whereas fixed-wing aircraft - even in total mechanical failure - are usually controllable to the extent of being able to make a shallow descent (unless of course there's either total electrical/hydraulic failure and/or significant structural damage, but those are rare compared with power-delivery-related failure.
5) The key power element of a helicopter - the main rotor drive - is a set of components operating under severe torsion loads. Metal fatigue under long-term load profiles is a real possibility - if servicing practices aren't scrupulously observed, you can end up with fatigue failures in critical components, particularly in the gearbox, final drive and rotor assembly.
Having said all that, I know a couple of helicopter pilots, and they both have utmost faith in their mode of flight (and the machines they use). And of course the Glasgow crash is a double tragedy because of the apparent loss of not only the crew but also the people on the ground. I hope that the AAIB and other authorities can get to the bottom of it, so that at least we can try to minimise the chances of something similar happening again.