As with all design on aircraft, weight is a key part of the specification. A nacelle that could contain all possible failure modes would be too heavy to fly.
Losing a fan blade, as demonstrated in your two youtube links, is both a more likely event to occur and low enough energy to be able to contain with a reasonable structure.
However consider the situation in [0] where a turbine disk became detached from its shaft. The disk is still taking power from the exhaust gas, but rather using the energy to power the compressor or rotate the fan it is now just increasing its own kinetic energy. This continues until the incredibly strong turbine disk rotates itself apart. From the linked article:
> For engineering purposes, disk fragments are assumed to have infinite energy at the moment of release; they will cut through any reasonable material and cannot be contained
You can see from photographs of the aftermath, the nacelle is missing where this happened
There are some nuances to it. British Airways (not the original British Airways Ltd [0], who merged to form BOAC) was established to manage several existing airlines that had already been nationalised (BOAC, BEA) and two regional carriers (Cambrian Airways and Northeast Airlines).
Of course BOAC and BEA had been made my consolidations of many smaller airlines which gets messy quickly when tracing the lineage. Even Cambrian and Northeast had formed British Air Services prior to this which was 70% owned by BEA.
So it is technically true that is was started as a state owned airline, but one made from companies that were originally created as private with a mixed history of state ownership.
You may be thinking of a different film, as all the cast members listed on wikipedia[0] are stated to have died after 1945.
The trivia section of the German wiki page of the same film says there's a disputed rumour that the film was prolonged to help the young extras avoid conscription.
Before the Ballmer/Zune use of the term I remember my father talking about data being squirted to A2A missiles (he was military) prior to launch, so perhaps that is one of the niches.
I run a similar setup with a bunch of EAP-225 APs controlled by a local instance of their Omada software (running on x64 rather that on ARM).
I've been very happy with roaming/throughput/reliability generally. The EAP-225 is 2x2, which they don't readily announce. Their newer and more expensive units are available as 4x4. That being said they're so cheap, I've been happy just to throw more onto the network.
For the software to manage them it uses some kind of multicast identification scheme to find new APs. If you're on a different subnet then it won't be able to automatically see them. They have a tool to connect to the AP and give it the management server IP, but that's Windows only.
The other option (that I went for) is just to create a management VLAN (good practice anyway) that the controller and APs live on. This is specifically supported by the APs.
Losing a fan blade, as demonstrated in your two youtube links, is both a more likely event to occur and low enough energy to be able to contain with a reasonable structure.
However consider the situation in [0] where a turbine disk became detached from its shaft. The disk is still taking power from the exhaust gas, but rather using the energy to power the compressor or rotate the fan it is now just increasing its own kinetic energy. This continues until the incredibly strong turbine disk rotates itself apart. From the linked article:
> For engineering purposes, disk fragments are assumed to have infinite energy at the moment of release; they will cut through any reasonable material and cannot be contained
You can see from photographs of the aftermath, the nacelle is missing where this happened
[0] https://admiralcloudberg.medium.com/a-matter-of-millimeters-...