digits_ wrote: ↑Mon Jan 14, 2019 9:19 pm
I'm pretty sure manufacturers know exactly what the consequences are of flying weights that are exceeding MTOW. It could be damage in turbulence, damage to the gear, metal fatigue etc. Main reason to not worry too much about this, is that the number of accidents where overweight flying resulted in death or crashed airplanes, is smaller than the number of icing related deaths.
No, it's very much a similar discussion to the one we're having: an airplane won't bend as soon as the MTOW is exceeded by one pound, the maximum weight limit is set at some point that the manufacturer thinks the performance of the aircraft will be adequate, usually factoring in engine-out performance. The performance is highly unlikely to be degraded significantly one pound over, it probably won't happen a hundred pounds over, it might not even happen a thousand pounds over; the point is that you don't know because the manufacturer didn't test it. By your logic, we should have every aircraft tested to find out at
exactly what weight and atmospheric conditions the performance will no longer be acceptable,
just to show those pilots who are inclined to fly overweight how bad it would be.
digits_ wrote: ↑Mon Jan 14, 2019 9:19 pm
The calculation/simulation of "XX ice on plane YY results in a performance penalty of ZZ" can be accurately calculated. Planes already need to show that they can fly into known icing if they are to be certified like that. For modern airplanes, that guarantees there are computer models available of icing during flight. Use those models and make an accurate and educated guess on how it will affect take off performance.
For modern airplanes, you might be able to approach the manufacturer and have them provide complex computer models, but do you not realize that those models don't exist for things like Navajos and Otters that have been out of production for thirty or forty years? The Q400s and 737s aren't the ones taking off contaminated, so it doesn't even matter if you can get models for them. You're going to have to get 206s, Conquests, Beech 99s, and all the other outdated pieces of crap from up north that are the ones being flown contaminated, collect every single tiny little piece of data on every version of those aircraft with every engine, every propellor, every STC, in every configuration, for every phase of flight, and
then figure out how icing affects them.
Who the hell is going to pay for that?
digits_ wrote: ↑Mon Jan 14, 2019 9:19 pm
The regulator can define XX amount of cases, with predefined parameters as mentioned before. Frost, clear ice, mixed ice, whatever. Those limited amount of cases can be precisely and accurately calculated. Pilots then have information on their specific airplane type (excluding mods) how the plane would be affected in those circumstances. They can pick/average the most accurately described situation and be convinced that the plane can not fly safely.
I don't think you've read a single thing that's been written here. You can't boil down icing to "frost", "clear ice", "mixed ice", and "whatever". You're oversimplifying things to the point that any models you make will be utterly pointless. You have to have data for every single combination of types of icing, that accumulates both on the ground and in the air, and you have to be able to accurately measure the thickness. Otherwise it's no better than eyeballing the conditions, and that's what people are doing already.
digits_ wrote: ↑Mon Jan 14, 2019 9:19 pm
I could only read the first page of the article that was linked to. It sounded promising, but was specifically dealing with droplets encountered during flight, not with taking off with a contaminated wing on a clear day for example.
There isn't much data on the effects of ice on top of a wing on take off, because even NASA test pilots don't want to go blasting off with a sheet of ice on the wings. That should tell you something. Anyway, most of the studies I've found discuss in-flight icing, which apparently isn't relevant to you, or are behind a paywall, so here's a publication from TC that has some very detailed information, including wind-tunnel data:
http://publications.gc.ca/collections/c ... -2008E.pdf
Residual impact ice is also a concern, and arguably more complex to classify, as you need to measure not only the thickness, but how far back along the wing it spread; if the boots broke some of the ice off, you have to calculate the performance degradation for the remaining amount. How do you do that?
digits_ wrote: ↑Mon Jan 14, 2019 9:19 pm
Let me ask you this:
Why do pilots not take off in a plane with one wing missing? Why do they not take off (most of us anyway) in a twin engine plane with a failed engine? Because they know and are convinced that the plane wouldn't fly.
Convince them that an iced up plane will not fly, and they will not attempt it. If you have other suggestions on how to accomplish this, by all means, please share. I do not think the current policy/TC video is sufficient.
Your analogy is stupid, because we're talking about incremental deteriorations in performance, not a loss of a component. It's not binary. Like I said, and I'm certain you didn't read, there's no point in presenting data to someone who is convinced the data is stupid and the experts are just living in ivory towers. It doesn't matter if you show them data that is slightly more forgiving than what they're expecting, because they don't care about the numbers; they "know" the aircraft will fly, and they'll keep pushing limits until they don't get away with it anymore.
Anyway, I don't think there's much point in wasting further breath on someone who thinks an aircraft will suffer gear damage or metal fatigue if the fuel gauges are slightly off or one of the people onboard had a big lunch.