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Old 14th Sep 2014, 07:05
  #377 (permalink)  
Owain Glyndwr
 
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Machinbird


The roll oscillation finally stabilizing was likely related to the decrease in roll acceleration available as a result of the substantial deceleration that the aircraft had experienced as was approaching stall speed.


Not sure about that. I take your point that system gain (roll acceleration/stick movement) was reduced as the airspeed fell, but against that you have to set worsening dutch roll damping and increased roll/sideslip ratio as AOA increases. And I don't think one can exclude Bonin learning how to fly it!
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