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Printed from: F-16.net - The Ultimate F-16 Reference [http://www.f-16.net]
Document title: F-16.net - Safety Wiring/Torquing Hardware Procedures :: F-16.net :: The Ultimate F-16 Reference
Original URL: http://www.f-16.net/f-16_forum_viewtopic-t-3145-start-15-sid-786351b9e7b59e3ef995c043b3289f8f.html
Printed on: 06 September 2008
F-16 Reference
5th Gen Fighters
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IDCrewDawg
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 Posted: May 27, 2005 - 08:22 AM
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Elite
Joined: Apr 22, 2004
Posts: 860
Location: Florida
Status: Offline
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| The 1-1A-8 will give torque values based on bolt size and type. It goes into material used as well, but not as specific. I don't have the TO with me so I can't quote it, but that is what I remember. |
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Sponsor
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 Posted: Sep 06, 2008 - 6:50 PM
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F-16.net Sponsor
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allenperos
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Posted: May 27, 2005 - 09:08 AM
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Elite
Joined: Feb 24, 2005
Posts: 631
Location: Philadelphia, PA USA
Status: Offline
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| Apparently this equation is a universal torque value for "standard torques" without a specified value in an instruction. It applies to engineering as well as SAE and maintenance standards. What that particuliar value of "torque" is, well thats the big question; it's the value you get on the torque wrench when you have a "snug" fit. The material is considered to be steel, as far as bolt size and material it is considered to be irrelevant because you're not over torquing nor under torquing, it's simply a snug fit. |
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F-16B, CC 80-0623 ERAU ROTC
MD-11, 90, 80, Cognizant Aerospace Technical Writer - Powerplant RR, GE, and P&W
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