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Total 5 documents matching your query.

1. IRS input flange/nut torque spec (score: 1): Author: Darrell Walker <darrellw@inetarena.com>; Date: Fri, 7 Mar 2003 19:17:32 -0800; I can't find a spec for the slotted nut on the input (pinion) shaft of the 4A IRS diff in the factory shop manual. Haynes says 85-100 lbs, which seems reasonable given the size of the nut and torques; /html/triumphs/2003-03/msg00199.html (7,946 bytes)
2. RE: IRS input flange/nut torque spec (score: 1): Author: "Randall Young" <Ryoung@navcomtech.com>; Date: Sat, 8 Mar 2003 07:28:34 -0800; I believe it's the same for the IRS and non-IRS diffs, which my factory manual gives as 85-100 ftlbs. There is supposed to be a very small amount of drag; there's a procedure in the manual for measu; /html/triumphs/2003-03/msg00206.html (8,178 bytes)
3. Re: IRS input flange/nut torque spec (score: 1): Author: Darrell Walker <darrellw@inetarena.com>; Date: Sat, 8 Mar 2003 13:09:29 -0800; Thanks to Randall for sending me some information (most of which was in the manual, had I bothered to read it, rather than just the reference tables). I've decided that the extra drag is probably jus; /html/triumphs/2003-03/msg00223.html (8,339 bytes)
4. RE: IRS input flange/nut torque spec (score: 1): Author: "Randall Young" <Ryoung@navcomtech.com>; Date: Sat, 8 Mar 2003 13:48:15 -0800; A little Permatex Aviation may help. But first, inspect the bore in the housing for any nicks or gouges. The outside of the seal usually doesn't need any help. That's probably as good a method as an; /html/triumphs/2003-03/msg00225.html (8,306 bytes)
5. Re: IRS input flange/nut torque spec (score: 1): Author: Darrell Walker <darrellw@inetarena.com>; Date: Sat, 8 Mar 2003 19:33:56 -0800; So far it is still holding. I probably won't be able to install it until next weekend anyway, so I'll keep an eye on it. I might make sure it holds by ordering another seal :-). -- Darrell Walker 66; /html/triumphs/2003-03/msg00237.html (8,060 bytes)

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