Loved how the areas beyond the slats near the wing tip showed the turbulence of the transient separation, great visual representation of what happens in a stall and the aerodynamic affects of slats.
How did the aux track detent arms cause the wing to stall before auto-slat? I would think it was something more to do with the trailing edge flaps. Isn't stall warning and therefore auto-slat) a function of angle of attack? Therefore auto-slat isn't going to activate until a stall is reported to the flight warning computer. So, to me, auto-slat after stall is normal ops.
The stick shaker operated on the last testflight later in this video. Before it didn't because when the stall occured, the pilot recovered the a/c and did not lower the airspeed further more. Icing conditions do not do anything with it, the shaker only operates when autoslat already tried to save the plane, and the airspeed decreases further and higher angle of attacks are encountered.
Stick shaker is strictly tied to the AOA. In fact you can put the aircraft in the air mode and reach out with a coat hangar and move the AOA vane into the extreme position and the stick shaker will activate.
The only thing here I would call abnormal is one wing falling off before the other. The stall should be gentle, level and predictable. I've corrected rig problems before and they were always the trailing edge flaps...usually the aft flap segment eccentrics needed adjusting. The leading edge slats are a little more mechanical than the trailing edge with all their monkey-motion.
Loved how the areas beyond the slats near the wing tip showed the turbulence of the transient separation, great visual representation of what happens in a stall and the aerodynamic affects of slats.
blampa 7 months ago
that guy talking all the time is annoying...
flchange 10 months ago
Is this plane from KLM?
BermudaGreenNox 1 year ago
@BermudaGreenNox
clicked thumbs down by accident and it's not letting me undo it :(
kneejouster 7 months ago
fantastic video.
rmlchin 1 year ago
How did the aux track detent arms cause the wing to stall before auto-slat? I would think it was something more to do with the trailing edge flaps. Isn't stall warning and therefore auto-slat) a function of angle of attack? Therefore auto-slat isn't going to activate until a stall is reported to the flight warning computer. So, to me, auto-slat after stall is normal ops.
JetMechMA 1 year ago
i wana c a plane just fall, like a real stall
KartKing4ever 2 years ago 2
Fantastic. Thank you for sharing this with us.
megathumper777 2 years ago
Thank you, exellent video!
kivialune 2 years ago
Great video, thank you. Very interesting to see.
GriffieRex 3 years ago
The stick shaker operated on the last testflight later in this video. Before it didn't because when the stall occured, the pilot recovered the a/c and did not lower the airspeed further more. Icing conditions do not do anything with it, the shaker only operates when autoslat already tried to save the plane, and the airspeed decreases further and higher angle of attacks are encountered.
737maint 3 years ago
@737maint
Stick shaker is strictly tied to the AOA. In fact you can put the aircraft in the air mode and reach out with a coat hangar and move the AOA vane into the extreme position and the stick shaker will activate.
JetMechMA 1 year ago
@737maint
The only thing here I would call abnormal is one wing falling off before the other. The stall should be gentle, level and predictable. I've corrected rig problems before and they were always the trailing edge flaps...usually the aft flap segment eccentrics needed adjusting. The leading edge slats are a little more mechanical than the trailing edge with all their monkey-motion.
JetMechMA 1 year ago
Great Vid, was only studying up on stall protection on the Ng's, I did notice no stick shaker while filming on cockpit.
In icing conditions, does stick shaker/stall logic reset autoslat ?
Thankyou for a great vid, we need more of these for 737 transition taining.
quinnyfly 3 years ago