How to Torque Lock nuts
How to Torque Lock nuts
We are getting ready to do some final Torquing of nuts on some areas in the wing.... if they are Lock nuts or bolts going into lock nut plates, how does one set the torque on the wrench???
Mike B.
Mike B.
use the chart in the aircraft standards handbook for the size of nut and bolt, make sure to add the torque from the nut drag. easiest with a dial type torque wrench. you just read the nut drag directly, and add that value to the final torque value in the chart.
e.g. i just torqued my tie downs. the nut drag registered 7 in-lbs. the range for the 10-32 nut is 20-25 in-lbs. so, i used 30 in-lbs as a final value (7 + mid-range value of 23 = 30).
hope that helps.
e.g. i just torqued my tie downs. the nut drag registered 7 in-lbs. the range for the 10-32 nut is 20-25 in-lbs. so, i used 30 in-lbs as a final value (7 + mid-range value of 23 = 30).
hope that helps.

- captain_john
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The inherent "problem" with torquing a fastener the way we do is that we are measuring a by product.
The thing we want to gauge is fastener tension. That is, in this case... bolt stretch. There is no way to do this in a practical fashion because the fastener is installed in aluminum. How are ya gonna see if it is stretched enough?
You measure the rotational force applied to it. With all things being "standard" (lubricity, free of dirt and debris) it should be consistent and accurate.
We are building a plane that isn't in a laboratory and the environment isn't textbook. Staying as close to the intention of the "standard" is the best we can hope for.
CJ
The thing we want to gauge is fastener tension. That is, in this case... bolt stretch. There is no way to do this in a practical fashion because the fastener is installed in aluminum. How are ya gonna see if it is stretched enough?
You measure the rotational force applied to it. With all things being "standard" (lubricity, free of dirt and debris) it should be consistent and accurate.
We are building a plane that isn't in a laboratory and the environment isn't textbook. Staying as close to the intention of the "standard" is the best we can hope for.

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Garmin G3X with VP-X & a TMX-IO-360 with G3i
It's all over but the flying! 800+ hours in only 3 years!
John you are exactly right about that. While talking with many people, mostly non pilot non builder types, I get the impression that a good number of people think that we aircraft builders must be working with some impossible tolerances. Looking at our torque chart all of our bolts have a range. In practice I choose a torque that puts me mid range on the charted torque for a particular bolt. But at either extreme the torque would be just right. I don't know this for sure but it is my suspicion that the nyloc nuts are designed to allow for less grip as the nut is turned over the end of the bolt and develop a tighter grip as the nut is coming to torque.We are building a plane that isn't in a laboratory and the environment isn't textbook. Staying as close to the intention of the "standard" is the best we can hope for.
- TomNativeNewYorker
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I was taught on fasteners requiring torque, if torquing from the head side to go to the high end of torque value; nut side - mid to upper value, and for castle/castlelated nuts requiring cotter pins or safety wire to torque to the low end of the value, then tighten if needed to line up cotterpin hole.jim_geo wrote: Looking at our torque chart all of our bolts have a range. In practice I choose a torque that puts me mid range on the charted torque for a particular bolt. But at either extreme the torque would be just right.
As far as nyloc is concerned, we dont use at al so am not really familar with them.
- TomNativeNewYorker
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Same here, but some cases it just cant be avoided and it must be on the head side. Thus the high end of the value is used.jim_geo wrote:Tom I was taught to strongly avoid tightening from the bolt side and if need be use torque wrench attachments and recalculate the torque in order to torque from the nut side. I don't know much about it but the shank has always seemed an unreliable and variable source of drag.