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Comment by trenchpilgrim | Hacker News Reader

No, because the plane is designed to safely fly without an engine. They test the engines by shooting turkeys from the grocery store into them while they run.

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Afterwards, they ship the entire engine, with turkey giblets and all, to a lab where the resulting damage is analyzed. Smells awful, according to the engineer I sat next to at a Thanksgiving dinner once...

Hopefully the giblets at your Thanksgiving dinner didn't come from the engine-sliced turkeys...

There's even a whole Wikipedia article on the "chicken gun" https://en.wikipedia.org/wiki/Chicken_gun

Exactly. The plane can land with one engine or even no engines, but it can't land without a pilot in a functioning cockpit.

As god as my witness, I thought turkeys could fly. Through jet engines.

Pretty sure even Les wouldn't have thought that ;-)

See, now I'm thinking of mayonnaise injectors to make instance turkey salad

without working one working engine - sure. with serious structural damage - perhaps not so much

Yes, with serious structural damage. It's part of certification process for the engine: https://youtu.be/iBqWS1hil18

I think GP meant structural damage to the airframe. That said, I think there are some modes of structural damage a modern plane can sustain and still fly, but to gp's point, probably not many.

yes I did :)

The FAA limits the mass of a weather balloon for this reason. I also would not be surprised to see new regulation on the distribution of that mass as a result of this incident.

There are some limitations on such balloons already. For example, if the payload is 4-6lbs, stricter rules apply if the weight/size ratio is greater than three ounces per square inch (measured by the smallest surface on the payload).[1]

Also for larger balloons, any trailing antenna must break if subjected to an impact force of 50lbs, or the antenna must have colored streamers every 50ft.

The ideal measurement would be some sort of crash testing. eg: The payload is accelerated at some standard velocity towards some standard target that represents the weakest part of an airplane (either cockpit glass or leading edge of a wing) and must not damage the target beyond some threshold. But that seems like it would be expensive, since every change in payload would require re-testing. Limits on sectional density seem like a good compromise.

1. https://www.ecfr.gov/current/title-14/chapter-I/subchapter-F...

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