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AIA/NAS - NASM6812

Bolts, Aircraft

inactive
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Organization: AIA/NAS
Publication Date: 1 February 1999
Status: inactive
Page Count: 19

Document History

June 30, 2016
FASTENERS, EXTERNALLY THREADED, ALLOY STEEL, CORROSION RESISTANT STEEL, ALUMINUM, 60,000 PSI TO 125,000 PSI
SCOPE AND CLASSES This specification defines the requirements for externally threaded fasteners manufactured from three different material types identified in Table I: 125 ksi UTS min for alloy...
June 30, 2016
FASTENERS, EXTERNALLY THREADED, ALLOY STEEL, CORROSION RESISTANT STEEL, ALUMINUM, 60,000 PSI TO 125,000 PSI
SCOPE AND CLASSES  This specification defines the requirements for externally threaded fasteners manufactured from three different material types identified in Table I: 125 ksi UTS min for alloy...
June 29, 2012
FASTENERS, EXTERNALLY THREADED, ALLOY STEEL, CORROSION RESISTANT STEEL, ALUMINUM, 60,000 PSI TO 125,000 PSI
This specification defines the requirements for externally threaded fasteners manufactured from three different material types identified in Table I: 125 ksi UTS min for alloy steel (Type 1) and...
March 1, 2006
Fasteners, Externally Threaded Alloy Steel, Corrosion Resistant Steel, Aluminum 60,000 PSI to 125,000 PSI
SCOPE AND CLASSES This specification defines the requirements for externally threaded fasteners manufactured from three different material types identified in TABLE I: 125 KSI UTS Min for alloy steel...
March 22, 2000
Fasteners, Externally Threaded Alloy Steel, Corrosion Resistant Steel, Aluminum 60,000 PSI to 125,000 PSI
This specification defines the requirements for externally threaded fasteners manufactured from three different material types identified in TABLE I: 125 KSI UTS Min for alloy steel (TYPE 1) and...
NASM6812
February 1, 1999
Bolts, Aircraft
A description is not available for this item.

References

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