![]() |
| If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|||||||
|
|
Thread Tools | Display Modes |
|
#10
|
|||
|
|||
|
"nrp" wrote in message oups.com... It could be undertorqued too. In that case there would be a lot of fretting under the base flange of the cylinder, and probably on the main bearing webs too. Yes, but that wouldn't have sheared the bolt at the jug stud ring as the OP said it did. You would get fretting at that location, but I don't see a failure mode in shear. If it hasn't been disassembled yet, you might check the other throughstuds to see what torque is required to very slightly further tighten them - giving you an indication of how close to the spec the previous assembler was. And how much torque it takes to loosen a couple of them. Jim |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Engine Balancing and Resonance Vibration Problem | AllanFuller | Owning | 13 | September 12th 05 01:51 AM |
| Proposals for air breathing hypersonic craft. I | Robert Clark | Military Aviation | 2 | May 26th 04 07:42 PM |
| Car engine FAA certified for airplane use | Cy Galley | Home Built | 10 | February 6th 04 04:03 PM |
| What if the germans... | Charles Gray | Military Aviation | 119 | January 27th 04 12:20 AM |
| Real stats on engine failures? | Captain Wubba | Piloting | 127 | December 8th 03 05:09 PM |