There are Pitts's / Pittses (?) with stall warning switches??
Well, the certified ones surely do. They only work for +ve AOA, but ....
But quit throwing the rest of us ,that do like you ,under the bus!!
My bad. I will try to sit on that.
Back to the L39 ... a lesson from history:
https://en.wikipedia.org/wiki/Richard_Bong#Death
40 kills in WWII, top fighter pilot ace - in piston/prop aircraft. A really good stick.
Died in a P-80 (think single seat T-33) shortly after WWII:
It was his 12th flight in the P-80; he had a total of four hours and fifteen minutes of flight time in the jet.
The plane's primary fuel pump malfunctioned during takeoff. Bong either forgot to switch to the auxiliary fuel pump, or for some reason was unable to do so
The I-16 fuel pump had been added to P-80s after an earlier fatal crash. Captain Ray Crawford, a fellow P-80 test/acceptance flight pilot who flew on August 6, later said Bong had told him that he had forgotten to turn on the I-16 pump on an earlier flight
A lesson from history there, for ya.
Engines like fuel, to run. You have probably noticed this with gasoline engines -
you can treat them pretty badly, but if the gas stops flowing, it's all over.
Jet engines have these horribly complicated FCU (Fuel Control Units) that scare
the shit out of me. See, it's really complicated, and when it fails, you have a bad
day. If that doesn't make the hair on the back of your neck stand up ....
So. Systems knowledge time. Why do FCU's fail? Well, one reason is ice plugging
them up, and that's why you always get Prist.
Also, the L39 has a secondary FCU. When you take off in an L39, you watch the RPM
and if it sags, you want your thumb next to the secondary FCU switch.
Those of you that fly fuel-injected Continentals will not find this unusual.
I know that I'm a horrible pessimist, and that can be a downer at parties. But I
expect everything to fail, and am somewhat pleasantly surprised when it does not.