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References: [ +subject:/^(?:^\s*(re|sv|fwd|fw)[\[\]\d]*[:>-]+\s*)*bolts\s*$/: 6 ]

Total 6 documents matching your query.

1. BOLTS (score: 1): Author: Unknown; Date: Mon, 15 Nov 2004 16:00:45 -0700; I was referring to aircraft bolts; I think that was the question. Gene; /html/triumphs/2004-11/msg00300.html (5,928 bytes)
2. bolts (score: 1): Author: Unknown; Date: Sat, 14 Aug 2004 22:51:06 -0400 FILETIME=[B66791E0:01C48272]; TR6 drive shaft bolts need to be grade 8 and no harder. If you use stainless steel for instance they are likely to break. I have used grade 5 in a TR3 and they were there for many miles. The key is; /html/triumphs/2004-08/msg00370.html (6,739 bytes)
3. bolts (score: 1): Author: Unknown; Date: Tue, 10 Jun 2003 22:31:45 -0400 FILETIME=[9A31E2A0:01C32FC1]; My understanding of the question at hand goes like this: the grade 8 bolt while "stronger" than the grade 5 is at the same time more brittle, and in a shear application would tend to break under load; /html/triumphs/2003-06/msg00333.html (6,960 bytes)
4. bolts (score: 1): Author: Unknown; Date: Mon, 10 Feb 1997 18:14:13 -0800; Hi, In the last weeks I have seen many comments on the list concerning TR-6 connecting rod bolts.My suggestion:if there is any question, any at all, replace them. As a total cost of an engine rebuild; /html/triumphs/1997-02/msg00534.html (6,479 bytes)
5. BOLTS (score: 1): Author: "Gene" <geneglenn@qwest.net>; Date: Mon, 15 Nov 2004 16:00:45 -0700; I was referring to aircraft bolts; I think that was the question. Gene; /html/triumphs/2004-11/msg00856.html (6,095 bytes)
6. bolts (score: 1): Author: "john taylor" <jat1127@hotmail.com>; Date: Sat, 14 Aug 2004 22:51:06 -0400 FILETIME=[B66791E0:01C48272]; TR6 drive shaft bolts need to be grade 8 and no harder. If you use stainless steel for instance they are likely to break. I have used grade 5 in a TR3 and they were there for many miles. The key is; /html/triumphs/2004-08/msg01156.html (7,061 bytes)

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