Posted: Mon Feb 13, 2006 4:32 pmPage 1 of 2
Posted: Mon Feb 13, 2006 4:32 pmPosted: Mon Feb 13, 2006 4:54 pmPosted: Mon Feb 13, 2006 5:26 pmPosted: Mon Feb 13, 2006 6:17 pmPosted: Mon Feb 13, 2006 10:18 pmPosted: Tue Feb 14, 2006 7:13 amPosted: Tue Feb 14, 2006 11:07 amPosted: Wed May 10, 2006 7:07 amAre the AN bolts all made from a certain grade metal? Or do we need to request a certain grade? i.e. stainless, etc
Posted: Wed May 10, 2006 12:20 pmThis should help:
Standard aircraft bolt, hex head. Made of high strength 8740 or 4037 alloy steel with 8740 being the most common. The length of an AN bolt is measured from under the head of the bolt to the end of the shank. The grip is the part of the bolt that is not threaded. The minimum tensile strength of an AN aircraft bolt is 125,000 PSI
Follow link:
AN Bolts
Karl
Standard aircraft bolt, hex head. Made of high strength 8740 or 4037 alloy steel with 8740 being the most common. The length of an AN bolt is measured from under the head of the bolt to the end of the shank. The grip is the part of the bolt that is not threaded. The minimum tensile strength of an AN aircraft bolt is 125,000 PSI
Follow link:
AN Bolts
Karl
Posted: Wed May 10, 2006 4:49 pmHere's another link you will find good information at.
http://www.dscp.dla.mil/gi/cbu/n/an3.html
George
http://www.dscp.dla.mil/gi/cbu/n/an3.html
George