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#1
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Mark James Boyd wrote: [snip] " . . . during a PCC a bellcrank broke and
this was caused by the pressure exerted by the "helper." Nice to have this happen on the ground, and I can't think of how this could have been detected without a PCC. So now I think a PCC is useful too..." Having a helper exert this much force is good??? I retain my renegade attitude to PCC's - they may be suitable for some things if done right (and breaking gliders is not doing it right in my book - the above is not an isolated example) but other checks are far more useful, and less damaging, for some gliders, e.g. my Ka6E. Chris N. |
#2
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I'm going to guess that the 10,000 repetitions of
opening and closing the dive brakes were what really caused the bellcrank problem in this case. On the other hand, I'm not a dig fan of manhandling and potentially deforming the spoilers on the glass ships either. If I was smarter and I owned my own ship, I'd likely investigate the best places to apply pressure which would't damage anything even when repeated 10000 times... In article , Chris Nicholas wrote: Mark James Boyd wrote: [snip] " . . . during a PCC a bellcrank broke and this was caused by the pressure exerted by the "helper." Nice to have this happen on the ground, and I can't think of how this could have been detected without a PCC. So now I think a PCC is useful too..." Having a helper exert this much force is good??? How much is too much? There's really no manual for this, and the POH doesn't even mention PCC... This area could use a bit of advice from sailplane manufacturers/materials engineers... I retain my renegade attitude to PCC's - they may be suitable for some things if done right (and breaking gliders is not doing it right in my book - the above is not an isolated example) but other checks are far more useful, and less damaging, for some gliders, e.g. my Ka6E. -- ------------+ Mark Boyd Avenal, California, USA |
#3
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A Positive Control Check is a means to an end, not an end in itself.
What is required is a Critical Assembly Check, of which the PCC may form a part. It is not possible to do a CAC unless the way the particular glider is rigged is understood, and there may be variations between different versions of the same type of glider, e.g. the elevator control connection on the ASK21. I know of several cases where gliders have flown mis-rigged and got away with it, e.g.: K13 with the drag spar pins not in safety. K21 with the drag spar pins missing. K13 with the aileron and brake safety pins missing (discovered when one aileron disconnected itself while flying). ASW20 with the elevator bolt missing. ASW24 with the elevator bolt missing. All these things happened to people I know, none of them would have been found by a PCC, indeed in many cases a PCC was done. Of course, there have been many cases where the pilot did not get away with it. I also know one club with several K23s, where the elevator control is automatic when the tailplane is rigged. After PCCs were made compulsory at that club, at the subsequent annual inspection damage was found to several elevators almost certainly caused by too much force during the PCC. I am sure the method of PCC recommended by Jim Vincent is correct, (posting 5th April 04.53 above), and his presentation http://www.mymedtrans.com/personal.htm looks ideal to me. However this is only part of a Critical Assembly Check, and if that is done properly the PCC is not the most important part. I am sure that a PCC should be done with the pilot at the control surfaces, and the helper at the cockpit controls. When Hotelier connections were first used it was not considered necessary to use safety pins, indeed some were provided with check holes so small that the use of pins was not possible. It was subsequently found that it was possible for Hoteliers to come undone UNDER NORMAL FLIGHT LOADS, and EVEN WHEN CORRECTLY RIGGED. This was why the use of locking wire, pins or some other safety device was made compulsory, and those connectors manufactured with small holes had to have them drilled larger. W.J. (Bill) Dean (U.K.). Remove "ic" to reply. "Chris Nicholas" wrote in message ... Mark James Boyd wrote: [snip] " . . . during a PCC a bellcrank broke and this was caused by the pressure exerted by the "helper." Nice to have this happen on the ground, and I can't think of how this could have been detected without a PCC. So now I think a PCC is useful too..." Having a helper exert this much force is good??? I retain my renegade attitude to PCC's - they may be suitable for some things if done right (and breaking gliders is not doing it right in my book - the above is not an isolated example) but other checks are far more useful, and less damaging, for some gliders, e.g. my Ka6E. Chris N. |
#4
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Bill,
I'm under the impression that you haven't looked at the presentation and are just evaluating it based on the title itself..if you have, my apologies. Some points I would like to make: What is required is a Critical Assembly Check, of which the PCC may form a part I fully agree with you. Not only is a PCC and CAC needed, but also takeoff checklists and landing checklists. The presentation does cover the requirements to do a PCC, CAC, as well as L'Hotelier connectors, the requirement for pins or LH connectors, preflight checks, landing checks....you get the picture. After PCCs were made compulsory at that club, at the subsequent annual inspection damage was found to several elevators almost certainly caused by too much force during the PCC. In addition, regarding avoiding damage to gliders, it does have a detail slide adressing this, points mentioned he * Don’t bang stick or control surfaces against the stops * Use light pressure on control surface… perhaps equal to weight of forearm * Control surfaces and trailing edges are damaged easily…apply pressure with open hand to avoid point loads * Apply pressure at control surface strong point…typically near pushrod attach point * For elevator, one hand on left elevator, one hand on right elevator * For spoilers, hold by spoiler plate, not spoiler cap…be careful of your fingers Regards! Jim Vincent CFIG N483SZ illspam |
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