Dromader 802 Crash

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Uploaded by on Dec 25, 2008

Um 802 que possivelmente sofre um disparo de hélice matando o piloto no impacto. E na sequência um Dromader executando as manobras que o 802 talvez teria feito se nenhum problema muito grave tivesse ocorrido. Que o piloto descanse em paz.

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  • The 802 has a fire gate which is completely different than an ag gate. The load left the 802 at a much faster rate and the pilot didn't understand the pitch up comming. This demo is BS.

  • Let´s please take into consideration wing design as well, Thrush, Air Tractor and PZL all have different wings, and all behave very differently, I can vouch for Thrush and Air Tractor, as I have flown them, just try and turn the Air Tractor without applying flaps on a 30+ degree ag turn, you will know what I mean. My respects to the PZL pilot in this video!

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  • One thing I notice very quickly in this video is the camel has a round motor that weighs about 3 times that of the turbine. Another is the pilot pulls hard and turns left AGAINST the torque. The 802 has a completely different wing. Air Tractors have a problem with going inverted and flat spinning if you don't treat them right. Chances are the camel in this video is in a scrap heap somewhere right now because of that giant no running engine.

  • AOA is very important....(of course)

    Airfrance flight 447 shows how a plane can stall into the ground (sea) with engines at full power (obviously not enough).

    I can't speculate exactly what this pilot did wrong, but he didn't recover, that's the hassle with low level, low speed, high angle of attack manoeuvres.

  • MIght there be a chance that buddy just went to sleep on the pitch up?

  • This is plane and simple pilot error...

  • coitado :(

  • So basically are you saying that steep incline wingovers at low speed and near zero G's are safe provided that the plane has plenty of power on..?

    Do you consider dromaders better areodynamicly than thrush and air tractors ie; shorter turn radius, more lift, slower stall speeds ect?

  • More aptly put, rather than at zero G's the stall does not occur, at zero angle of attack the stall does not occur.

    If a wing is rotated 90 degrees incedence and moves through through the air only at a few mph producing very applied little G stress on the wing the wing will stall.

    However, if the wing slows to only a few mph but remains streamlined to the wind with no AOA the wing will not stall if there are zero G's.

    AOA is more important than G's for stalling a wing.

  • Seems like a unwanted cross over spin. Often planes crash upside down. Here I explain why:

    Check out my video-channel. You find it under the name:

    Crossover spin CRASH - Umkehrtrudeln ABSTURZ - Vehicle Simulator

    Another video about stall and spins I made you find under the name:

    Stall and spins

    Fly safe!

  • ...it somehow looks like the pilot just keeps on pushing the stick....

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