Looks like this one was covered quite some time ago, but now that nbasson has revived it, I read it and it has piqued my interest.
Quote:Hmm, exiting spins and exiting stalls are 2 v.different things methinks!
A stall is a lack of speed to keep airflow over the wings sufficient to fly (barring the torque turn, but you need an SU29 for that!)
A spin is where you intestines take it in turns to squash each other whilst your eyeballs suffer compression one moment, and suction the next.
I think aub doesn't know to much about aerodynamics and flying.....
Ozzy
To enter a spin, an aircraft must FIRST be STALLED!
-A spin is created when one wing still produces lift and in turn, that lift pulls the aircraft about it's vertical axis.
-During a spin the airspeed will be at or near stall, and the aicraft will experience relatively LOW G-force.
-Most airframe damage occurs during Improper spin RECOVERY(not during the spin)due to overzealous recovery technique, OR lack of(allowing the speed to build too much and THEN recovering).
-Power, absolutely, should be reduced to idle BUT, this is due to induced torque affect, NOT increased speed DURING a spin.
-Spin training IS required for ALL CFI's in the U.S.
-Spin training(verbal instruction)saved me from certain death, as a student pilot, and in my opinion is VERY valuable.
-Spin training is not a bad idea, but I would highly recommend doing it with an aerobatic(as opposed to primary PPL) instructor, in an aerobatic aircraft, such as a Pitts, Decathalon, Sukhoi etc.
-Without repeating the same thing - Redwing is correct RE:description of the accelerated stall. The example we used to use was the turn to final. It is drummed into our heads from day one, that when you are " low and slow" while turning final, to limit your angle of bank(stall speed increases with bank angle(very bad)). So, it would make sense that if you're carrying an extra 20-30knots while turning final, you should be safe right? The accelerated stall(in this case) occurs at a HIGH AIRSPEED and HIGH ANGLE OF BANK, due to the wing exceeding the critical AOA(as Redwing stated).
Finally, I agree with Hagar 100%. For those that have done spins in real airplanes, the F$ version is hardly a substitute. The aircraft (in MS) falls in and out of the stall(a stall is maintained through an actual spin's entirety), and the airspeed varies from zero to VsX2. Actual aircraft dynamics are more than a matter of three axis' and power, lift and drag. And the current computers are still not up to speed in this department.