AIA/NAS NAS 6409-2002
Bolt, Tension, Hex Head, Close Tolerance, 6AL-4V Titanium Alloy, Short Thread, Reduced Major Thread Diameter, Self-Locking and Nonlocking, 160 ksi Ftu Rev. 11; FSC 5305

Standard No.

AIA/NAS NAS 6409-2002

Release Date

2002

Published By

Aerospace Industries Association/ANSI Aerospace Standards

Status

Withdraw

Latest

AIA/NAS NAS 6409-2002

Scope

NAM13 12-105, “Fastener Test Methods Method 105 Stress Durability” was adopted on 29 August 1997 for use by the Department of Defense @OD). Proposed changes by DoD activities must be submitted to the DoD Adopting Activity: Commander, Naval Air Warfare Center Aircraft Division, Code 4141OOB120-3 Highway 547, Lakehurst, NJ 08733-5100. DoD activities may obtain copies of this standard fi-om the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 191 11-5094. The private sector and other Government agencies may purchase copies fi-om the Aerospace Industries Association, 1250 Eye Street NW, Washington, DC 20005.

AIA/NAS NAS 6409-2002 history

• 2002 AIA/NAS NAS 6409-2002 Bolt, Tension, Hex Head, Close Tolerance, 6AL-4V Titanium Alloy, Short Thread, Reduced Major Thread Diameter, Self-Locking and Nonlocking, 160 ksi Ftu Rev. 11; FSC 5305