SAE International Datasheets for Standards and Technical Documents
Standards and technical documents includes standards, codes, regulation, handbooks, manuals, comprehensive guides and other formal publications. Standards, codes, and regulation establish uniform specifications, procedures or technical criteria.
Standards and Technical Documents: Learn more
| Product Name | Notes |
|---|---|
| Amendment 1 of AS70991A. | |
| Counterfeiting of refrigerants has seen a dramatic rise over the past two decades. This rise can be partially attributed to global restrictions placed on production and use of refrigerants by... | |
| Enhanced License and UML Model for Data Dictionary for Quantities Used in Cyber Physical Systems (AS6969) allowing for greater usage as outlined in the terms of the Enhanced License. Data... | |
| Enhanced License for Data Dictionary for Quantities Used in Cyber Physical Systems (AS6969) allowing for greater usage as outlined in the terms of the Enhanced License. Terms can be reviewed... | |
| Enhanced License for Data Dictionary for Quantities Used in Cyber Physical Systems (AS6969B) allowing for greater usage as outlined in the terms of the Enhanced License. Terms can be reviewed... | |
| No scope available. | |
| Scope is unavailable. | |
| Seat furnishings are installed around seats and are intended to enhance passenger privacy and comfort. They may have provisions for additional occupants to be seated when the aircraft is in-flight,... | |
| Technical Standard | |
| The focus of this SAE Aerospace Standard (AS) is the integration of thermally actuated pressure release devices, hereafter referred to as fuse plugs, with the wheel and brake assembly. It... | |
| The purpose of this document is to provide a standard for aircraft fuselage markings located at the doors used for ground servicing operations. These markings can be used by all... | |
| The purpose of this standard is to aid manufacturers in creating devices that will provide maintenance staff with objective, reliable data consistent with certain types of airborne contaminants ("sources"), captured... | |
| The purpose of this standard is to provide uniform methods for defining, quantifying, and classifying the residual stress in metallic structural alloy products and finished parts. These stresses may exist... | |
| This Aerospace Standard (AS) defines the requirements for a metallic reinforced, duct assembly suitable for use in low pressure, 350 °F ground heaters. | |
| This Aerospace Standard (AS) documents the operating instructions, rules, policies, and practices of the Performance Review Institute (PRI), an affiliate of SAE. Covered in this standard are the operations of... | |
| This Aerospace Standard (AS) documents the procedures for implementing third-party accreditation programs administered by NADCAP. | |
| This Aerospace Standard (AS) documents the requirements for implementing NADCAP industry consensus-based accreditation programs. | |
| This Aerospace Standard (AS) documents the requirements for implementing Nadcap industry consensus-based accreditation/certif ication programs. | |
| This Aerospace Standard (AS) establishes the minimum requirements for suppliers of heat treat services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). These requirements may... | |
| This Aerospace Standard (AS) establishes the minimum requirements for the quality assurance program of a distributor of factory new material and excess inventory, assembled, altered, new, used, remanufactured, repaired, rebuilt... | |
| This Aerospace Standard (AS) establishes the requirements for Heat Treating Accreditation by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). These requirements may be supplemented by additional requirements specified... | |
| This Aerospace Standard (AS) establishes the requirements for hydraulic start motors suitable for use in starting a gas turbine engine, and the methods to be used for demonstrating compliance with... | |
| This Aerospace Standard (AS) establishes the requirements for manufacture of Elastomer Seals to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted in... | |
| This Aerospace Standard (AS) establishes the requirements for manufacturers of Fasteners to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted in accordance... | |
| This Aerospace Standard (AS) establishes the requirements for manufacturers of Fluid System Components to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers for Etching Processes to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). These requirements may be supplemented... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Chemical Processing Services to be accredited by Nadcap. Nadcap accreditation is granted in accordance with SAE AS7003 after demonstrating compliance... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Chemical Processing Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of coatings services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP) in accordance with SAE AS7003. | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Composites to be accredited by Nadcap. Nadcap accreditation is granted in accordance with SAE AS7003 after demonstration of compliance with... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Electronics Printed Circuit Boards to be accredited by Nadcap. Nadcap accreditation is granted in accordance with SAE AS7003 after demonstrating... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Nonconventional Machining Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of nondestructive testing (NDT) to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP) in accordance with the... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Shot Peening Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Welding Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). These requirements may be supplemented... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Welding/Brazing Services to be accredited by Nadcap. These requirements may be supplemented by additional requirements specified by Nadcap Welding Task... | |
| This Aerospace Standard (AS) establishes the requirements for suppliers of Welding/Brazing Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). These requirements may be supplemented... | |
| This Aerospace Standard (AS) is to be sued to supplement AS7110. In addition to the requirements contained in AS7110, the requirements contained herein shall apply to suppliers seeking NADCAP accreditation... | |
| This Aerospace Standard (AS) is to be used as a supplement to AS7114. In addition to the requirements contained in AS7114, the requirements contained herein shall apply to suppliers seeking... | |
| This Aerospace Standard (AS) is to be used as a supplement to either SAE AS7106 or SAE AS7107 for suppliers who have software (to include firmware) that comprises all or... | |
| This Aerospace Standard (AS) is to be used as a supplement to SAE AS7109. In addition to the requirements contained in AS7109, the requirements contained herein shall apply to suppliers... | |
| This Aerospace Standard (AS) is to be used as a supplement to SAE AS7112. In addition to the requirements contained in AS7112, the requirements contained herein shall apply to suppliers... | |
| This Aerospace Standard (AS) is to be used as a supplement to SAE AS7112. In addition to the requirements specified in AS7112, the requirements specified herein shall apply to suppliers... | |
| This Aerospace Standard (AS) is to be used to supplement AS7108. In addition to the requirements contained in AS7108, the requirements contained herein shall apply to suppliers seeking NADCAP accreditation... | |
| This Aerospace Standard (AS) is to be used to supplement AS7110, and/or any Nadcap recognized quality system. In addition to the requirements contained in AS7110, the requirements contained herein shall... | |
| This Aerospace Standard (AS) is to be used to supplement AS7110, and/or any other Nadcap recognized quality system. In addition to the requirements contained in AS7110, the requirements contained herein... | |
| This Aerospace Standard (AS) is to be used to supplement AS7110. In addition to the requirements contained in AS7110, the requirements contained herein shall apply to suppliers seeking NADCAP accreditation... | |
| This Aerospace Standard (AS) is to be used to supplement AS7114. In addition to the requirements contained in AS7114, the requirements contained herein shall apply to suppliers seeking NADCAP accreditation... | |
| This Aerospace Standard (AS) is to be used to supplement AS7116. In addition to the requirements contained in AS7116, the requirements contained herein shall apply to suppliers seeking NADCAP accreditation... | |
| This Aerospace Standard establishes the common requirements for hydraulic starters, suitable for use in aircraft and missiles, and the methods to be used for demonstrating compliance with these requirements. | |
| This Aerospace Standard establishes the minimum requirements necessary for NADCAP accreditation of a General Quality System the meets, at a minimum, MIL-Q-9858. These requirements may be supplemented by additional requirements... | |
| This Aerospace Standard establishes the minimum requirements necessary for NADCAP accreditation of an Inspection System that meets, at a minimum, MIL-I-45208. These requirements may be supplemented by additional requirements at... | |
| This Aerospace Standard is to be used as a supplement to either PRI AC7106 or PRI AC7107 by suppliers that have customer approval for self-release of finished product. This standard... | |
| This Aerospace Standard is to be used as a supplement to either SAE AS7106 or SAE AS7107 to demonstrate compliance to MIL-STD-1535. This Standard is required for all suppliers seeking... | |
| This Aerospace Standard is to be used as a supplement to either SAE AS7106 or SAE AS7107. This Standard is required for all suppliers seeking NADCAP General Quality Systems accreditation... | |
| This Aerospace Standard is to be used as a supplement to SAE AS7109. In addition to the requirements contained in AS7109, the requirements contained herein shall apply to suppliers seeking... | |
| This Aerospace Standard is to be used as a supplement to SAE AS7114. In addition to the requirements contained in AS7114, the requirements contained herein shall apply to suppliers seeking... | |
| This aerospace standard outlines minimum quality assurance requirements common to commodities which must be met by a "PASS-THRU" distributor for third party accreditation. | |
| This aerospace standard outlines minimum quality assurance requirements common to commodities which must be met by a "Value Added" distributor for third party accreditation. | |
| This aerospace standard outlines the minimum requirements for the quality assurance program of a distributor of new aircraft or aerospace parts and material. It is designed to aid in the... | |
| This data dictionary provides definitions for quantities, measurement units, reference systems, measurands, measurements and quantity modalities commonly used in the command and control of cyber physical systems. A cyber physical... | |
| This data dictionary provides definitions for quantities, measurement units, reference systems, measurands, measurements and quantity modalities commonly used on the command and control of cyber physical systems. A cyber physical... | |
| This data dictionary provides definitions for quantities, measurement units, reference systems, measurands, measurements, and quantity modalities commonly used in the command and control of cyber-physical systems. A cyber-physical system is... | |
| This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the... | |
| This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made of a corrosion and heat resistant nickel-base alloy of the type identified under... | |
| This document covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. | |
| This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. | |
| This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable, iron base alloy of the type identified under the Unified Numbering System as UNS S66286. | |
| This document describes a method for measuring forces during an impact between a soft or frangible projectile and a relatively rigid flat normal surface. The document describes the hardware and... | |
| This document describes methods for measuring dynamic forces, pressures, and projectile fragment distribution patterns during an impact between a soft or frangible projectile and a rigid flat inclined surface. It... | |
| This document establishes the requirements for Aeronautical National Form (ANPT) pipe threads, gages, and gaging methods for determining conformity of aeronautical taper pipe threads to this standard. | |
| This document has been declared "CANCELLED" as of April 2005 and has been superseded by PRI AC7108/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114/3. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114/4. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of February 2009 and has been superseded by PRI AC7109. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of January 2015 and has been superseded by PRI AC7119. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7102/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116/3. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116/4. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2009 and has been superseded by PRI AC7108/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/3. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/4. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/5. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/6. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/7. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/3. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/4. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7115. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7200/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7202. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI PD1100. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of June 2017. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/1. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/10. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/11. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/2. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/3. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/4. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/5. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/6. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/7. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/8. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/9. By this action, this document will remain listed in the Numerical Section of... | |
| This document has been declared "CANCELLED" as of November 2007. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are... | |
| This drawing specifies parts AS70000-0204, AS70000-0205, AS70000-0206, AS70000-0207, AS70000-0208, AS70000-0209, AS70000-0210, AS70000-0211, AS70000-0212, AS70000-0213, AS70000-0214, AS70000-0215, AS70000-0216, AS70000-0217, AS70000-0218, AS70000-0219, AS70000-0220, AS70000-0221, AS70000-0222, AS70000-0223, AS70000-0224, AS70000-0225, AS70000-0226, AS70000-0227, AS70000-0228, AS70000-0229,... | |
| This procurement specification covers aircraft premium quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675,... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable nickel base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant martensitic iron base alloy of the type identified under the Unified Numbering System as... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant precipitation hardenable iron base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and moderate heat resistant martensitic iron base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion and moderate heat-resistant martensitic iron base alloy of the type identified under the Unified Numbering System as... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant austenitic iron base alloy of the type identified as SAE 30302 and of 125 000 psi... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant austenitic iron base alloy of the type identified under the Unified Numbering System as UNS S30200... | |
| This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30035,... | |
| This procurement specification covers aircraft quality bolts and screws made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a... | |
| This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675, and... | |
| This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. The... | |
| This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. | |
| This procurement specification covers aircraft quality bolts and screws made from carbon steels, high expansion steels, or corrosion and heat resistant steels of the type identified under the Unified Numbering... | |
| This procurement specification covers aircraft quality retaining rings of the spiral wound type with uniform rectangular cross-sections and made from a corrosion resistant austenitic iron base alloy of the type... | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering... | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200. | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S34700. | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion- and heat-resistant nickel base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion-resistant steel of the type identified under the Unified Numbering System as UNS S30200. | |
| This procurement specification covers aircraft quality solid rivets made from a corrosion and heat resistant cobalt alloy of the type identified under the Unified Numbering System as UNS R30605. | |
| This procurement specification covers aircraft quality studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of... | |
| This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675, and of 135... | |
| This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. | |
| This procurement specification covers aircraft quality studs made from a low-alloy, heat-resistant steel of the type identified under the Unified Numbering System as UNS K14675. | |
| This procurement specification covers aircraft-quality bolts and screws made from 6Al - 4V titanium alloy of the type identified under the Unified Numbering System as UNS R56400. The following specification... | |
| This procurement specification covers aircraft-quality bolts and screws made from 6Al-4V titanium alloy of the type identified under the Unified Numbering System as UNS R56400. The following specification designation and... | |
| This procurement specification covers aircraft-quality bolts and screws made of 6.0Al - 4.0V titanium alloy and of 160 ksi tensile strength at room temperature. | |
| This procurement specification covers aircraft-quality bolts and screws made of 6.0Al-4.0V titanium alloy and of 160 ksi tensile strength at room temperature. | |
| This procurement specification covers aircraft-quality bolts and screws made of 6Al - 4V titanium alloy and of 160 ksi tensile strength at room temperature with a fatigue strength test rating. | |
| This procurement specification covers aircraft-quality bolts and screws made of 6Al - 4V titanium alloy of the type identified under the Unified Numbering System as UNS R56400. The following specification... | |
| This procurement specification covers aircraft-quality bolts and screws made of 6Al-4V titanium alloy and of 160 ksi tensile strength at room temperature. | |
| This procurement specification covers aircraft-quality bolts and screws made of corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a carbon steel of the type identified under the Unified Numbering System as UNS G10100. | |
| This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a corrosion- and heat-resistant nickel alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a corrosion-resistant steel of the type identified under the Unified Numbering System as UNS S34700. | |
| This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi... | |
| This procurement specification covers aircraft-quality solid rivets made from a corrosion- and heat-resistant cobalt alloy of the type identified under the Unified Numbering System as UNS R30605. | |
| This procurement specification covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made of a corrosion and heat resistant nickel-base alloy of the type identified... | |
| This procurement specification covers bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers bolts and screws made from a corrosion and heat resistant precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable, nickel base alloy of the type identified under the Unified Numbering System as UNS... | |
| This procurement specification covers bolts and screws made from a corrosion- and heat-resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. | |
| This procurement specification covers bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675, having UNJ profile... | |
| This procurement specification covers bolts and screws made from carbon steels, high expansion steels, or corrosion and heat resistant steels of the type identified under the Unified Numbering System as... | |
| This procurement specification covers bolts made from a corrosion and heat resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30159. The following... | |
| This procurement specification covers bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30035. The following specification designations... | |
| This procurement specification covers bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30035. | |
| This procurement specification covers bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30159. | |
| This procurement specification covers bolts made from a corrosion-resistant, work-strengthened, cobalt-chromium-nick el alloy of the type identified under the Unified Numbering System as UNS R30159. | |
| This procurement specification covers flat gaskets for aircraft engine accessory drive, Type XX, in accordance with AND20010. | |
| This procurement specification covers flat gaskets for aircraft engine accessory drive, Type XX, in accordance with AS20010 (replacing AND20010). | |
| This procurement specification covers plain helical lock washers fabricated from heat treated carbon steel. | |
| This procurement specification covers plain helical lock washers made of corrosion-resistant steel.of the type identified under the Unified Numbering System as UNS S30200. | |
| This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened. | |
| This procurement specification covers rivets fabricated from an aluminum alloy designated as 2117-T4, solution treated. | |
| This procurement specification covers rivets made from an aluminum alloy designated as 2117-T4, solution treated. The following specification designations and their rivet coatings are covered: | |
| This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286... | |
| This procurement specification covers split cotter pins made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S32100. | |
| This procurement specification covers split cotter pins made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200. | |
| This procurement specification covers split cotter pins with optional ends (see Figure 1 ), made from a corrosion and heat resistant steel of the type identified under the Unified Numbering... | |
| This procurement specification covers split cotter pins with optional ends (see Figure 1 ), made from a corrosion resistant steel of the type identified under the Unified Numbering System as... | |
| This procurement specification covers studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286 and... | |
| This procurement specification covers studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under Unified Numbering System as UNS S66286 and of... | |
| This procurement specification covers tubular sealing rings, commonly named METAL O-RING GASKETS, made from a corrosion and heat resistant steel tubing of the type identified under the Unified Numbering System... | |
| This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi... | |
| This procurement specification covers tubular-shaped, slotted spring pins made of a corrosion and moderate heat resistant, martensitic iron base alloy of the type identified under the Unified Numbering System as... | |
| This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting... | |
| This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive, self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting... | |
| This SAE Aerospace Standard (AS) establishes the requirements for suppliers of coatings services to be accredited by Nadcap in accordance with AS7003. The requirements contained herein may be supplemented by... | |
| This SAE Aerospace Standard (AS) establishes the requirements for various types of identification sleeving that will shrink to a predetermined size upon the application of heat after it has been... | |
| This SAE Aerospace Standard (AS) is to be used as a supplement to AS7109. In addition to the requirements contained in AS7109, the requirements contained herein shall apply to suppliers... | |
| This SAE Aerospace Standard (AS) provides dimensions for a standardized test fixture that can be used to evaluate the dynamic performance requirements defined in some elastomer material standards of O-rings... | |
| This SAE Aerospace Standard (AS) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives. | |
| This SAE Aerospace Standard defines the requirements for establishing a nondestructive inspection (NDI) program for aerospace systems to include but not limited to aircraft structure, aircraft stores (external structures such... | |
| This SAE Aerospace Standard defines the requirements for establishing a Nondestructive Inspection (NDI) program for aerospace systems to include but not not be limited to aircraft structure, aircraft stores (external... | |
| This specification covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made of a carbon or low alloy steel. | |
| This specification covers bolts and screws made from a corrosion and heat resistant, martensitic iron base alloy of the type identified under the Unified Numbering System as UNS S17400. The... | |
| This specification covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286,... | |
| This specification covers closely-wound helical coil, screw thread inserts made from a corrosion resistant steel formed wire of the type identified under the Unified Numbering System as UNS N30400. The... | |
| This specification covers closely-wound helical coil, screw thread inserts made from an age hardenable nickel base alloy formed wire of the type identified under the Unified Numbering System as UNS... | |
| This specification covers closely-wound helical coil, screw thread inserts made of a corrosion resistant steel formed wire with a chemical composition in accordance with Table 1 and identified under the... | |
| This specification covers crimp style aluminum lug terminals and conductor splices for aluminum aircraft wire. Lug terminals and conductor splices are hereafter called "terminals". | |
| This specification covers crimp-style aluminum lug terminals and conductor splices for aluminum aircraft wire. Lug terminals and conductor splices are hereafter called "terminals." | |
| This specification covers studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following... | |
| This specification covers studs made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. | |
| This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft. | |
| This specification covers the requirements for one type of water repellent compound. | |
| This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole. | |
| This specification establishes requirements for automatic shutoff, quick-disconnect coupling assemblies for fuel and oil lines. | |
| This specification establishes the performance, qualification, acceptance limits, and identification for aeronautical engine high tension spark igniters. | |
| This specification establishes the qualification and acceptance limits for aeronautical engine high tension spark igniters. | |
| This standard describes the National Aerospace and Defense Contractors Accreditation Program (NADCAP) to accredit the capability of suppliers furnishing processes, products, and services for the aerospace and defense industries as... | |
| This standard establishes minimum design, installation, qualification, and operational requirements for thermally actuated, pressure release devices for use only in tubeless tire type aircraft wheels. These devices are designed to... | |
| This standard establishes rules for the implementation of the National Aerospace and Defense Contractors Accreditation Program (NADCAP) to accredit the capability of suppliers furnishing processes, products, and services for the... | |
| THIS STANDARD ESTABLISHES THE DIMENSIONAL AND VISUAL QUALITY REQUIREMENTS, LOT REQUIREMENTS AND PACKAGING AND LABELING REQUIREMENTS FOR O-RINGS MOLDED FROM AMS7361 (ETHYLENE-PROPYLENE) RUBBER WHICH IS ABLE TO PROVIDE THE REQUIRED... | |
| THIS STANDARD ESTABLISHES THE DIMENSIONAL AND VISUAL QUALITY REQUIREMENTS, LOT REQUIREMENTS, AND PACKAGING AND LABELING REQUIREMENTS FOR O-RINGS MOLDED FROM AMS7410 FLUOROCARBON (FKM) RUBBER. IT SHALL BE USED FOR PROCUREMENT... | |
| This standard establishes the inspection requirements and acceptance standards for optimum surface finish O-ring packings and gaskets. (This is not an O-ring specification as such.) | |
| This standard establishes the inspection requirements and acceptance standards for optimum surface finish O-ring packings and gaskets. (This is not an O-ring specification per se.) | |
| This standard establishes the minimum requirements for materials testing laboratories (MTL) accredited by NADCAP. The following test methods and processes for metallic material systems are covered in this standard. a... | |
| This standard establishes the minimum requirements for training, examination, and certification of aerospace coatings application personnel applying liquid organic coatings to interior structural or exterior substrates. It establishes criteria for... | |
| This standard includes the forms to be used by a third party for auditing and on-going inspection for assessing the capability of sealant suppliers to furnish product to indicated standards. | |
| This standard includes the forms to be used by a third party to survey a nondestructive test facility with respect to penetrant, magnetic particle, ultrasonic, and/or radiographic methods. | |
| This standard includes the procedures and forms to be used by a third party for auditing and on-going inspection for assessing the capability of sealant manufacturers to furnish products to... | |
| This standard presents the designer with sufficient information to fully define the configuration of the connection and to determine the limits of application for given conditions. | |
| This test method covers procedures to qualitatively determine the visual and physical condition of a liquid organic coating component (pigmented base, base without pigment, curing solution, or thinner) in a... |
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