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Anecdotes make poor proof of thesis.
However - you are correct that the ultimate cause of the accident was poor maintenance of the hook. But - the failure mode is one the Tost/Ottfur does not have. They cannot rotate in a horizontal plane around the mounting bolt. If yours is welded on - good, if it is inverted - better. If not, as on the Cessnas - your daily checks should include whether there is enough friction to prevent rotation around the mount bolt. If it does rotate it will back release. It is unlikely to do this at a peaceful, stable moment in the tow. One near miss - does someone have to die before we accept there is a risk? This means there are at least two situations where the Schweizer hook is unsafe. The other is failure to release under high lateral angle - which can be overcome by inverted mounting. ref - http://www.jdburch.com/Towstudy.htm The Tost is safer - if you have the option I can't see why you would fit an obsolete design that is no longer in production and is known to be unsafe under circumstances that have killed a number of pilots - time to move on. Bruce BT wrote: " We had a world class pilot write off an ASW20 in December. The schweizer hook turned 180 degrees and sold him the rope at 50 feet... An anthill saw to the rest. How can a tow hook on the tow plane rotate (turn) 180 degrees, do you mean it was mounted "inverted"? And if mounted upright or inverted, the SGS hook, if properly installed and maintained would not just, "sell him the rope". Just because it was "inverted" means nothing.. they are all "inverted" when installed on the glider. Something was not maintained. I noticed once between flights and I was out of the cockpit that the tow plane end of the rope (hook) seemed to be almost "1/2" way to the release point. I reset it, did a tow and got out and looked again. It had moved again on it's own. So now I start looking to see what would have happened to cause that. The release cable rides in a plastic casing inside the Pawnee, zip tied to fuselage formers. Some ties had aged and broke, the cable was free to sag. So bouncing in turbulence on the way down, the cable bounced in the aft fuselage, no "pressure" on the hook and it was pulling the release lever. There is more to towing than inspecting the rope and the release system... Check ALL of the airplane and it's parts. The SGS hook failure is no different than if TOST springs were broken and not caught on preflight inspection or checked during the day. No different than a weak link failure.. No different than the engine coughing and the tow purposefully releasing the rope. Had a Stearman blow a jug, the glider pilot saw the puff of smoke and then saw the rope release within a second of the puff. Those are the chances you take... don't blame the hook, blame the preflight. BT (Pawnee Tow Pilot on an SGS Upright Hook) --- news://freenews.netfront.net/ - complaints: --- |
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