AIA/NAS NASM6812

FASTENERS, EXTERNALLY THREADED, ALLOY STEEL, CORROSION RESISTANT STEEL, ALUMINUM, 60,000 PSI TO 125,000 PSI - Rev 3

contributor author	AIA/NAS - Aerospace Industries Association of America Inc.
date accessioned	2017-09-04T15:28:29Z
date available	2017-09-04T15:28:29Z
date copyright	06/29/2012
date issued	2012
identifier other	NUMZWEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;quein/handle/yse/29542
description abstract	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 corrosion resistant steel (Type 2), and 62 ksi UTS min for aluminum (Type 3). Receiving contractors may reject any manufactured lot which does not conform. Workmanship of fasteners shall conform with aircraft manufacturing processes. Recommendations for improvements or corrections to this specification should be directed to the Executive Secretary of the National Aerospace Standards Committee or a using member company. Specifications listed herein, of the issue in effect on date of inquiry are a part of this specification to the extent indicated. In the case of conflict, the requirements herein shall take precedence.
language	English
title	AIA/NAS NASM6812	num
title	FASTENERS, EXTERNALLY THREADED, ALLOY STEEL, CORROSION RESISTANT STEEL, ALUMINUM, 60,000 PSI TO 125,000 PSI - Rev 3	en
type	standard
page	11
status	Active
tree	AIA/NAS - Aerospace Industries Association of America Inc.:;2012
contenttype	fulltext