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Why aren't there a lot of passenger airliners (short flights) using this configuration, since using Coanda effect by blowing wing's extrados is much safer in harsh weather, and would provide extra safety during gusty landings and takeoffs?

I guess extra weight, induced drag, and engine maintenance height may be good reasons, but is it enough to eliminate this solution in the economy/safety equation?

An 72

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    $\begingroup$ I think the problem is that it does not actually count towards any of the safety regulations. Most of those revolve around engine failure and that's exactly where the layout does not help. $\endgroup$ – Jan Hudec Apr 24 '17 at 18:16
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    $\begingroup$ The other issue is that positioning the engines there is really good for STOL operations, and operations out of unimproved strips. Not really a big problem for commercial airliners. $\endgroup$ – Ron Beyer Apr 24 '17 at 18:19
  • $\begingroup$ @RonBeyer -- besides, most commercial operations out of STOLports and unimproved strips are small enough that Dorniers and Twotters get the job done, anyhow... $\endgroup$ – UnrecognizedFallingObject Apr 25 '17 at 0:04
  • $\begingroup$ Exhaust gases get quite warm. What material is the blown part of the wing made off? $\endgroup$ – Koyovis May 1 '17 at 21:33
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The extra lift provided by the blown flaps and the better protection against FOD is simply not needed in regular airline service, and the higher engine location will make maintenance harder and more expensive. Airport runways are long enough for most purposes already, and only tactical transports could possibly benefit from the enhanced lift and better FOD protection.

At least the An-72 and -74 is operated by a number of civilian and military entities. Note that all of them serve small, local airfields. Note also that passenger service with the An-72 has been discontinued in Finland since this type was not cleared there for passenger services.

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