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This specification covers design requirements, performance requirements, and methods of procurement for tools and associated accessories used to strip aerospace vehicle electrical wire and cable. Aerospace vehicle electrical wire has stranded conductors with protective plating and specialized insulation. Poor quality wire strippers or mismatched blades can compromise the performance of wiring
AE-8C2 Terminating Devices and Tooling Committee
This specification covers the requirements for black oxide coatings on parts
AMS B Finishes Processes and Fluids Committee
This SAE Aerospace Recommended Practice (ARP) details the recommended process for correcting measured non-volatile particulate matter (nvPM) mass and number data for particle losses in the sampling and measurement system specified in ARP6320B. This technique is only recommended for conditions where both nvPM mass and number concentration measurements are in the valid measurement ranges of the instruments that are discussed in the tool limitations section. This ARP also supplies an Excel software tool with documentation to automate the process. The body of this ARP details the recommended calculation method, uncertainties, and limitations of the system loss correction factors. It explains, in detail, the required inputs and outputs from the supplied Excel software tool (developed on Windows 7, Excel 2016). Also included are: The Excel correction tools (refer to Attachments I and V). Installation instructions for a Windows-based computer (refer to Attachment II). A user technical manual
E-31P Particulate Matter Committee
This specification covers an aluminum alloy in the form of clad sheet from 0.006 to 0.249 inches (0.15 to 6.32 mm), inclusive, in thickness (see 8.6
AMS D Nonferrous Alloys Committee
The purpose of this SAE Recommended Practice is to provide guides toward standard conditions for operating marine hydraulic transmissions where push-pull cable control is applicable. For control cable information see SAE J917
Marine Technical Steering Committee
This specification establishes the requirements for etch inspection of steel parts to detect overheating (rehardening or over-tempering) caused by abusive machining or grinding or to detect localized discontinuous carburization
AMS B Finishes Processes and Fluids Committee
This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing supplied in the annealed (O temper) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper
AMS D Nonferrous Alloys Committee
The purpose of this SAE Recommended Practice is to provide guides toward standard conditions for operating marine engine throttles (gasoline or diesel) where push-pull cable control is applicable. For control cable information see SAE J917
Marine Technical Steering Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles up to 0.499 inches (12.67 mm) in nominal diameter, or least thickness, and under 10 in2 (65 cm2) in cross-sectional area
AMS D Nonferrous Alloys Committee
This document defines cables that are used to provide electrical power for U.S. Department of Defense avionics support and test equipment
AGE-3 Aircraft Ground Support Equipment Committee
This SAE Aerospace Standard (AS) establishes the requirements for internally or externally swaged or welded sleeves or tube end adapters for use with 24° cone flareless fluid connection fittings per AS18280
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers an aluminum alloy in the form of extruded profiles (shapes) 0.063 to 0.375 inch (1.6 to 10 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
This SAE Aerospace Information Report (AIR) considers the following major areas: 1 major components and their ratings; 2 selection criteria for optimum design balance for electrical systems; 3 effects of operating conditions and environment on both maintenance and life of components; 4 trouble signals - their diagnosis and cure
AGE-3 Aircraft Ground Support Equipment Committee
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry
Engine Power Test Code Committee
E-25 General Standards for Aerospace and Propulsion Systems
No Scope available
Engine and Airframe Technical Standards Committee (TSC)
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 prior to purchase once item is added to the cart. Data Dictionary for Quantities Used in Cyber Physical Systems (AS6969B) This data dictionary provides definitions for quantities commonly used in the command and control of cyber physical systems. It defines mathematical and logical terms, quantities, measurement units, reference systems, measurands, and measurements. It also defines common quantity modalities. The dictionary is structured to be convenient to data modelers. It is also extendable so that users can create their own quantity domains
AS-4UCS Unmanned Systems Control Segment Architecture
This specification covers an AlSi10Mg alloy produced by laser powder bed fusion (L-PBF) additive manufacturing and subjected to stress relief, hot isostatic press (HIP), solution treat, and artificial aging
AMS AM Additive Manufacturing Metals
No scope available
Engine and Airframe Technical Standards Committee (TSC)
This set of Abstract Syntax Notation (ASN.1) modules contains the precise definitions of data structures used in the SAE J3287 standard. Using the ASN.1 specification, a compiler tool can produce libraries that enable software applications to use the data structures and produce corresponding encodings using the Octet Encoding Rules (OER). For further information see the body of SAE J3287. You may also be interested in: V2X Misbehavior Reporting™ the J3287 PDF. V2X Misbehavior Reportingt™ SET File that includes the J3287 ASN File and the J3287 PDF (ZIP format) - download purchase only
V2X Security Technical Committee
This specification covers metal products fabricated by direct metal deposition
AMS AM Additive Manufacturing Metals
This SAE Aerospace Standard (AS) establishes Minimum Performance Standards (MPS) for life rafts carried on board aircraft. This document is not intended to specify particular design methods, mechanisms, or equipment to be used to accomplish the objectives established herein
S-9A Safety Equipment and Survival Systems Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of wire up to and including 0.563 inches (14.30 mm) in diameter
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a magnesium alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990
AMS P17 Polymer Matrix Composites Committee
This document has been declared "CANCELLED" as of January 2009. By this action, this document will remain listed in the Numerical Section of the Aerosepace Standards Index
S-9A Safety Equipment and Survival Systems Committee
This AS provides the minimum performance requirements for the following types of inflatable emergency evacuation devices (hereinafter referred to as device[s]): 1 Type I - Inflatable Slide: A device suitable for assisting occupants in descending from a floor-level airplane exit or from an airplane wing to the ground. A Type I off-wing slide is a device that does not include a ramp. 2 Type II - Inflatable Slide/Raft: A device suitable for assisting occupants in descending from a floor-level airplane exit or an airplane wing to the ground that is also designed to be used as a life raft. A Type II off-wing slide/raft is a device that does not include a ramp. 3 Type III - Inflatable Exit Ramp: A device suitable for assisting occupants in descending from certain overwing exits to an airplane wing. 4 Type IV - Inflatable Ramp/Slide: A device suitable for assisting occupants from an overwing exit or airplane wing to the ground. It is a combination ramp and wing-to-ground device. 5 Type V
S-9A Safety Equipment and Survival Systems Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of March 1995. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications
AMS CE Elastomers Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This Aerospace Recommended Practice (ARP) is to establish criteria for design and installation of combination evacuation slide/raft devices for use both as ground and water escape devices in the event of emergency. NOTE: This document is not intended to specify design methods, mechanisms, or equipment to be used in accomplishment of the objectives set forth herein
S-9A Safety Equipment and Survival Systems Committee
This Aerospace Recommended Practice (ARP) establishes criteria for design and installation of devices which will ensure rapid and effective occupant evacuation in the event of an emergency. This ARP deals with emergency evacuation devices installed for the purpose of rapidly assisting the occupants to the ground or water from emergency exits and/or wings. NOTE: This document is not intended to specify design methods, mechanisms or equipment to be used in accomplishment of the objectives set forth herein
S-9A Safety Equipment and Survival Systems Committee
No Scope available
Engine and Airframe Technical Standards Committee (TSC)
No Scope available
Engine and Airframe Technical Standards Committee (TSC)
No Scope available
Engine and Airframe Technical Standards Committee (TSC)
This SAE Aerospace Standard (AS) provides design criteria and performance tests for portable, handheld, battery-powered, electronic megaphones used by aircraft crew members to provide information and guidance in the event of an aircraft emergency or other non-routine situation
S-9A Safety Equipment and Survival Systems Committee
This AS provides suitable test methods for measuring the dynamic coefficient of friction ("slip resistance" or "sliding friction") of aircraft flooring and walkway surfaces in accordance with 14 CFR and EASA CS 25.793 and 25.810(c). § 25.793 specifies the areas which are likely to become wet in service must have slip-resistant properties, and § 25.810 specifies an escape route must be established from each overwing emergency exit that is covered with a slip-resistant surface
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This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification covers a corrosion and heat-resistant alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of September 1996. It is recommended, therefore, that this specification not be specified for new designs. This specification covers a low-alloy steel in the form of sand castings. Primarily for cast parts requiring heat treatment to minimum yield strengths up to 180,000 psi (1240 MPa
AMS E Carbon and Low Alloy Steels Committee
This standard provides a specification of a general misbehavior report format suitable for reporting misbehavior observed by a system running SAE V2X applications, and specific report contents for specific instances of misbehavior. It also provides an overview of the architecture of a system-wide misbehavior management service for the V2X system and positions the misbehavior reporting services within that architecture
V2X Security Technical Committee
The complete requirements for procuring the product shall consist of this document and the latest Issue of the basic specification, AMS2431
AMS B Finishes Processes and Fluids Committee
This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of conditioned stainless steel cut wire shot
AMS B Finishes Processes and Fluids Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been supersed by AMS 3731 & /7
AMS P Polymeric Materials Committee
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 1996, and has been superseded by AMS 3731 & /1
AMS P Polymeric Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification covers an aluminum alloy procured in the form of extruded bars, rods, wire, profiles (shapes), and tubing up to 1.499 inches (38.07 mm), inclusive, in nominal diameter or least thickness (bars, rods, wire, or profiles) or nominal wall thickness (tubing) (see 8.6
AMS D Nonferrous Alloys Committee
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