I used to fly 20-series Lears. Mmo was .83. This airplane could climb directly to 39,000' in about 15minutes and the power must be
reduced to avoid exceeding Mmo! I've also experienced two flameouts in these aircraft. What happens when you lose one engine at this altitude? First.....Mach will decay rapidly Second........the Angle of Attack (AOA) indicator will rapidly approach the yellow(indicating an inevitable stall), if you attempt to stay at that altitude...... As Hagar stated,
power on most aircraft is reduced after takeoff and again when cruise altitude is reached
but on most jets the output of each engine still remains in the 90%+ range. This Lear can achieve a 10,000fpm initial climb rate but as you approach the flight levels it falls off to less than two thousand. Usually the last two thousand feet are gained at 500-750fpm or less! That's about the same as a Skyhawk/Cherokee isn't it? Imagine losing %50 of your power in one of
these airplanes(try it on the sim!).
On the occasion that I did have a flameout a "re-light profile" is in the AOM. What this means is that the "dead engine" won't even re-light until you reach a much lower altitude. So, let's say that you wanted to try your theory at one of these lower altitudes where it's a little safer...... now you have
this problem.........
*PS. Unless the aircraft was specifically designed for it, flying on assymetric power would be even worse & potentially dangerous.
.......due to the above mentioned adverse yaw, the rudder has to counter the single running engine's desire to turn the aircraft. To accomplish this it must create lift on a horizontal plane but in the process, more drag is created because this large "paddle" is hanging out in the slipstream much more so than the subtle inputs required in more normal flight conditions. ......hope that helps.....