PPRUNE FAN#1
28th Aug 2004, 04:25
One thing I don't like to do in a helicopter is the botched-auto-go-around. That's the one where you see it's not going to work out so you go, "Err, let's get out of here and try this again, shall we?" But now that I think of it, doing auto-rpm checks require the same maneuvre, and I don't like doing them either. While helicopters transition easily enough from powered to autorotative flight, the reverse does not seem to be true. They seem awkward and uncomfortable.
On the JustHelicopters free-for-all/discussion board, an operator of R-22's rather courageously reported that he now had two of the little birdies lying on their side. Seems that in both cases, the instructors (one of which was him) were letting the students practice "autorotative glides" with a termination at (low) altitude. In both cases, the engines failed to respond and the resulting real autos were not successful for a number of reasons.
Let's say that you were in an autorotative descent at...oh, 60 knots. Let's say that you had just decided to resume powered flight. Let's say that you've increased the power (to max or top-of-the-green or whatever value you choose). Further, let's say that the aircraft has not yet arrested it's rate-of-descent. Now let's say that the engine picked exactly that moment to quit. How fast would the main rotor rpm bleed off? Any of you wannabe (or actual) test pilots want to go out and try it? (Perhaps Nick will give it a go when he starts test-flying the "new" Sikorsky/Schweizer/Hughes VHS-300.)
Not me. I've never been brave enough to - especially in a recip, but I believe that the results would probably be startling. It would probably look like somebody pulled the rotor brake handle.
After his first R-22 accident, the confessor on the JustHelicopters melee/discussion board decided that the altitude he'd previously selected as his "floor" for the maneuvre was too low to get the auto re-established and get everything back within the proper parameters. Ergo, he increased it as a matter of school policy to 150 feet agl. (We can only surmise what the floor was prior to that.) This still proved too low, of which the second accident is unfortunate proof.
Regulatory agencies require applicants for a certificate to demonstrate "autorotational descents with a power-recovery and power-recovery to a hover." Two different things. In both cases, there are a lot of human variables possible in the performing of the procedures. In the first, if the student were to let the nose rise a little, thus bleeding off airspeed, it could get quite uncomfortable as both P1 and P2 realize that the engine isn't responding to the lash and the rotor rpm is going down faster than the governor of New Jersey on a good-looking Israeli guy.
We've had many discussions on this board about the Height/Velocity curve and how it is derived. We believe that the worst-case scenario involves an engine failure in a climb at a high power-setting and low airspeed. But I wonder if there isn't another even-worse-worst-case scenario?
On the JustHelicopters free-for-all/discussion board, an operator of R-22's rather courageously reported that he now had two of the little birdies lying on their side. Seems that in both cases, the instructors (one of which was him) were letting the students practice "autorotative glides" with a termination at (low) altitude. In both cases, the engines failed to respond and the resulting real autos were not successful for a number of reasons.
Let's say that you were in an autorotative descent at...oh, 60 knots. Let's say that you had just decided to resume powered flight. Let's say that you've increased the power (to max or top-of-the-green or whatever value you choose). Further, let's say that the aircraft has not yet arrested it's rate-of-descent. Now let's say that the engine picked exactly that moment to quit. How fast would the main rotor rpm bleed off? Any of you wannabe (or actual) test pilots want to go out and try it? (Perhaps Nick will give it a go when he starts test-flying the "new" Sikorsky/Schweizer/Hughes VHS-300.)
Not me. I've never been brave enough to - especially in a recip, but I believe that the results would probably be startling. It would probably look like somebody pulled the rotor brake handle.
After his first R-22 accident, the confessor on the JustHelicopters melee/discussion board decided that the altitude he'd previously selected as his "floor" for the maneuvre was too low to get the auto re-established and get everything back within the proper parameters. Ergo, he increased it as a matter of school policy to 150 feet agl. (We can only surmise what the floor was prior to that.) This still proved too low, of which the second accident is unfortunate proof.
Regulatory agencies require applicants for a certificate to demonstrate "autorotational descents with a power-recovery and power-recovery to a hover." Two different things. In both cases, there are a lot of human variables possible in the performing of the procedures. In the first, if the student were to let the nose rise a little, thus bleeding off airspeed, it could get quite uncomfortable as both P1 and P2 realize that the engine isn't responding to the lash and the rotor rpm is going down faster than the governor of New Jersey on a good-looking Israeli guy.
We've had many discussions on this board about the Height/Velocity curve and how it is derived. We believe that the worst-case scenario involves an engine failure in a climb at a high power-setting and low airspeed. But I wonder if there isn't another even-worse-worst-case scenario?