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facthunter

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Everything posted by facthunter

  1. Different Cause in the Jabiru. Some similarity. I'm not that stupid as to be confusing the two... Jabiru fretted the cases .Nev
  2. Well spotted. The passengers (if any) would not be locked inside, either. Nev
  3. I'm pretty hard on them all But a lot are compromised by Poor management Particularly starting techniques and Avoiding Prohibited rpms, MP/ Rpm combinations over propping and using motor for short periods where they never get Properly warmed up. Motor cowled with adjustable Cowl flaps and properly Baffled with Air blast tubes on the parts that need them to be specially cooled and Lagged fuel Lines etc. ie Properly Installed . Nev
  4. Just as soon Have a Good Comanche, thanks. Nev
  5. They Had them in the C-150. They had them in each door. Nev
  6. ALL Planes have a comfortable taxi speed and its nowhere near V1. Nev'
  7. I wouldn't try that line at any enquiry. Nev
  8. The Plane was close to it's service ceiling and relied on the downslope to help it get back in the air It's a rehearsed procedure for that location. Sort of OK IF there's no climbers there at the same time. Nev
  9. I critically examine many aircraft engine in dept and they ALL have some design Faults No engine is bullet proof particularly piston engined ones. Rotax later motors are becoming more highly stressed and complex. People say Merlins were a great Engine and the highest TBO ever was 650 Hours . My comment wasn't generalised. It was related to the LONG studs holding alloy bits together that get Hot and expand at different rates.. Nev
  10. It would fit RAAus rules. . Nev
  11. The Walrus would have been one of the More rough water capable. Nev
  12. Pistons are the Most efficient of the ICE ones .Hydrogen to electric direct? Hydrogen is difficult to store. Makes things brittle Nev
  13. Not made up at all,. But carry on IF it makes you feel better. Do your own proper research if you really care. Nev
  14. For rescue etc? Wouldn't a helicopter be able to do the same? Nev
  15. Why stick with Piston engines IF you don't have to? Nev
  16. Its been happening. They are too long and the steel doesn't expand as much as the Alloy. It's not an uncommon problem in such designs. . Be interest to have my question answered. Nev
  17. What about your SAFETY in the Meantime? The days of people getting electrocuted should be over. Nev
  18. Get those earth return circuit Breakers installed or you are NOT legal. They will POP instantly when some thing is wrong and a proper electricians screwdriver will indicate which wire is active. Nev
  19. There seems to be a Major change there. Is that shortening the studs that have been Breaking in the Genuine Motors? Nev.
  20. Thanks. Often cranks have sections that are much weaker than the general section and that concentrates stress in those areas. Poor design. Usually where a throw goes to a crank pin section. Billet is not really like a bit of grained timber as some imagine if it's rolled properly. The ends of each rolled length should be discarded if there's any chance of a Scarf being there.. Nev
  21. I've seen Legless people coming out of a PUB, who were Blind drunk.. Nev
  22. Why would a billet Crank weigh More than a forged one? I can't see why it would have to. (refering back a little way). Nev
  23. That worked when I voted today. Nev
  24. it's Extremely Difficult to forge something like a six throw crank shaft with seven Main Bearings. The grain flow you refer to is not ideal either in that application as it is in a poppet valve where you an extrude the shape and jump it up to thickness it. Plenty of racing car shafts are from billet and the get a more balanced result as well. Aero shafts are often nitrided where stress reliving is achieved at the same time as surface hardening.. Crack testing is done new and at every rebuild. There is NO non destructive test for Metal fatigue. At some stage the Part should be discarded, "Lifed" or it was built far too heavy to be on a plane. .Nev
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