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barrylunch t1_ja6pqgg wrote

What does ETOPS have to do with engine placement on the stab vs. under-wing? I don’t think you answered the question (which is about placement, not quantity).

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tsme-EatIt t1_ja6rmp8 wrote

I answered how quantity is related to placement. You can't have 3 engines and have all of them under the wings, they wouldn't be balanced.

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therealdilbert t1_ja6wrf1 wrote

But there have been several planes with all the engines in back, like the Boeing 727 witt three engines, or the MD80 with two engines

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Target880 t1_ja72nlk wrote

Underwing versus on the back is not the same as why one on the vertical stabilizer or just the air intake there

If you have an odd number of engines you need to place one in the center line of the airplane and with a jet engine, you can put it in the front line with propellers.

You can but even the number of engines under the wing or on the body. 4 engines on the back have them placed side by side like a Vickers VC10

3 engines existed primarily because of ETOPS rating, you could fly longer over open water with 3 compared to 2 engines and the cost will be less than if you have 4 engines. A minor part is that it adds high-altitude takeoff performance in locations like Colorado which is at 1-mile altitude.

They have disappeared because engine performance and ETOPS regulations have changed so you are allowed to do the same flight with just 2 engines and it is a cheaper way to build and operate aircraft

Boeing 727 have all 3 engine in the rear, and McDonnell Douglas MD-11 had 2 under the wings and 1 in the back. So 2 engines under the wings or on the back are unrelated to the vertical stabilizer position of a third engine.

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tsme-EatIt t1_ja6x2e2 wrote

That's outside the scope of the question asked by the OP. They asked about wing mounted and vertical stabilizer mounted engines.

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