Hacker Read top | best | new | newcomments | leaders | about | bookmarklet login

That is actually kind of scary.

How many cycles does the airframe have to go through in order for this to become a problem? I tend to think that if the FAA gave a shit about general aviation maybe we wouldn't be flying planes from the 1960s



sort by: page size:

I don't see why that's a problem. Airplanes have a lifespan of 30 years.

There’s a lot of inertia in commercial aviation. Airframes last for decades. At some point though, the current path will lead to ruin.

This isn’t a very very bad. This stuff is highly controlled for a reason.

Engines have a variety of LLPs (Life Limited Parts), and airlines are required to count cycles, hours, etc and replace with OEM certified replacements— all part of the reasons jets don’t fall out of the sky


Planes have pretty disastrous failure modes, and useful lifespans in the decades. An accelerated test cycle seems... unwise.

The airframe isn't getting old. In fact there's nothing left of the old airframe but the general shape of the windshields.

It's the type rating approval process that got old and caused all this.


For anyone immediately going to UAF 232 as an example please realize that this is titanium used in the air frame not the engine. The engine is under dramatically higher loads and is far more material fault intolerant. I'm not saying this isn't serious issue but this is not as severe a concern, otherwise the planes would be grounded already.

This looks like a serious issue that the faa should investigate. Since they look at so many problems and frequently issue repair orders, recalls, etc by certain dates, why would they treat this particular issue so differently?

I don't understand how modern airliners, with all their advanced high-tech complicated design, operating in such a tightly controlled regulatory environment, can still be having trouble with this. Crazy.

Hoo boy, that could be dangerous if there's something physically wrong with the plane (a non-functional aileron or stabilator, for example).

I have been wondering how dangerous flying is going to be when when / if it comes back and all these planes come out of storage. Mechanical things just sitting around is some times far worse than them being in constant use.

Except this is not about cracks in the airframe but in a component that is certified for significantly more cycles than when the cracks are being found. If these were benign FAA wouldn’t have released an AD to inspect and repair them.

If the Aircraft is 20 years old, you should worry a lot more about the airline's safety culture than the manufacturer's. Just saying.

I am not aware that the aiframe is the main reason why planes are taken out of service. Fuel inefficiency is typically the primary reason, plus increased maintenance cost. I can't remember an accident of a major airliner as a result of the airframe failing post the 1970s.

Will be interesting to look at fatigue of the control surfaces though, if they get used many times more per flight to adjust for minor turbulences.


What's wrong with that? Seems like good practice if you expect these planes to be flying for decades.

Yeah, this is getting ridiculous. Aircraft break all the time, and the FAA investigates all the time. I'm begining to think some people here have short positions in Boeing stock or something.

That isn't completely true. We don't know exactly, but the documented time between overhaul and the life of the airframe place upper bounds on those.

Some cheap airlines might ignore those rules, but none in the US. (Only the poorest, most corrup, countires in the world will ignore those limits)


They were designed in the 60s and the FAA certification process makes designing a replacement cost prohibitive with current and future sales volumes.

So, it's at least a 30 year old plane.

I'm not connected at all with the private aviation industry... What is the useful (safe?) lifespan of an aircraft like this?


"These are not considered an immediate safety concern but could cause premature aging of the airframe." So this would seem to be about quality control issues as opposed to design engineering or flightworthiness.
next

Legal | privacy