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This specification covers an irradiated, thermally-stabilized, modified polyolefin plastic in the form of a thin-wall, heat-shrinkable tubing with a low recovery temperature
AE-8D Wire and Cable Committee
This specification covers epoxy-resin-impregnated glass fabric laminates in the form of sheet clad on one or both sides with electrolytically-deposited copper foil
AMS P Polymeric Materials Committee
This specification covers a non-crosslinked polyvinyl chloride plastic in the form of flexible, thinwall, heat-shrinkable tubing with a low recovery temperature
AE-8D Wire and Cable Committee
This specification covers the requirements for equipment, materials and procedures to be used in anodic treatments for magnesium base alloys for the purpose of increasing their corrosion resistance or producing surfaces suitable for the application of a protective organic finish
AMS B Finishes Processes and Fluids Committee
This specification covers flexible extruded, vinyl plastic tubing
AE-8D Wire and Cable Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder
AMS G Titanium and Refractory Metals Committee
This specification defines the procedures and requirements for joining metals and alloys using the electron-beam (EB) welding process
AMS B Finishes Processes and Fluids Committee
This specification defines the procedures and requirements for joining metals and alloys using the electron beam welding process
AMS B Finishes Processes and Fluids Committee
The GNSS sensor standard integrates Global Positioning System/Global Orbiting Navigation Satellite System (GLONASS) sensors. The sensor provides position information for display to pilots, and data to other navigation systems on the airplane
Airlines Electronic Engineering Committee
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements and procedures for three classes of gas, vacuum, liquid, and low pressure (LPC) carburizing and related heat treatment of parts fabricated from carburizing grade steels. Parts made from steels other than those specified in the detail specifications may be heat treated in accordance with the applicable requirements using processing temperatures, times, and other parameters recommended by the material producer unless otherwise specified by the purchaser. This specification does not cover pack carburizing
AMS B Finishes Processes and Fluids Committee
This specification covers an irradiated, thermally-stabilized, flame-resistant modified-polychloroprene rubber in the form of thin-wall tubing
AE-8D Wire and Cable Committee
This specification establishes process controls for the repeatable production of aerospace parts by Electron Beam Powder Bed Fusion (EB-PBF). It is intended to be used for aerospace parts manufactured using additive manufacturing (AM) metal alloys, but usage is not limited to such applications
AMS AM Additive Manufacturing Metals
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
AMS P Polymeric Materials Committee
The requirements for acquiring the sleeving described herein shall consist of this specification sheet and the issue of the following specification listed in that issue of the Department of Defense Index of Specifications and Standards (DODISS) specified in the solicitation: MIL-DTL-23053
AE-8D Wire and Cable Committee
This specification covers procedures for ultrasonic inspection of thin wall metal tubing of titanium, titanium alloy, and corrosion- and heat-resistant steels and alloys having nominal OD over 0.1875 inch (4.762 mm) with OD to wall thickness ratio of 8 or greater and wall thickness variation not exceeding ±10% of nominal
AMS K Non Destructive Methods and Processes Committee
This procedure covers ultrasonic inspection of tubular, centrifugally-cast, corrosion-resistant steel cylinders
AMS K Non Destructive Methods and Processes Committee
ARINC Specification 485, Part 2 specifies the ARINC 485-control protocol used by the LRUs described in ARINC Specification 628 Part 2. This document defines a multi-drop bus. The point-to-point configuration is also supported. The point-to-point bus is treated simply as a multi-drop bus with only one drop. There is one master LRU and one or more slave LRUs present on the bus. However; multiple buses may be connected in parallel, where each parallel bus operates independently from each other
Airlines Electronic Engineering Committee
This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier use
Truck Bus Control and Communications Network Committee
This document provides general and specific design guidance for the development of software data loading equipment for all types of aircraft. The primary purpose of data load is to upload loadable software parts to airborne computers. A secondary function of data load is downloading data from airborne computers. Software data load functionality generally falls into the following categories: Portable Data Loader (PDL) for loading equipment on the ground or carried onto aircraft to perform onboard loading. Airborne Data Loader (ADL) for installation on aircraft to perform onboard loading. Data Load Function (DLF) is software that performs the data loading. This document defines data loaders designed to load avionics equipment over a high-speed interface using an Ethernet network protocol. This document defines media interfaces and protocol requirements specific to all data load functions, whether portable or airborne. This document also describes the desired capabilities of data loading
Airlines Electronic Engineering CommitteeAvionics Maintenance CommitteeFlight Simulator Engineering and Maintenance Committee
The purpose of this SAE Aerospace Information Report (AIR) is to provide guidance for aircraft engine and propeller systems (hereafter referred to as propulsion systems) certification for cybersecurity. Compliance for cybersecurity requires that the engine control, propeller control, monitoring system, and all auxiliary equipment systems and networks associated with the propulsion system (such as nacelle systems, overspeed governors, and thrust reversers) be protected from intentional unauthorized electronic interactions (IUEI) that may result in an adverse effect on the safety of the propulsion system or the airplane. This involves identification of security risks, their mitigation, verification of protections, and their maintenance in service. This document is intended to serve as suitable guidance for propulsion system manufacturers and applicants for propulsion system type certification. It is also intended to provide guidance for subsequent propulsion system integration into
E-36 Electronic Engine Controls Committee
This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat-resistant steel. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes process controls for the repeatable production of preforms/parts using the laser directed energy deposition (L-DED-) process for additive manufacturing. Preforms are intended to be used to manufacture aerospace parts, but usage is not limited to such applications. Feedstock may be either wire (for L-DED-Wire) or powder (for L-DED-Powder
AMS AM Additive Manufacturing Metals
This specification covers pasted-mica electrical insulation for molded armature slot bases, commutator insulation, shells, heating elements, and other similar insulating purposes
AMS P Polymeric Materials Committee
This specification and its supplementary detail specifications cover a woven nylon cloth coated with polyether (EU) urethane
AMS P Polymeric Materials Committee
This specification covers electrical connections made with single, solid, round copper or copper alloy wire wrapped around copper alloy terminals without the use of solder
AMS B Finishes Processes and Fluids Committee
This specification covers a thermally-stabilized, irradiated, modified fluoropolymer in the form of very-thin-wall tubing
AE-8D Wire and Cable Committee
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified silicone rubber in the form of heat shrinkable tubing
AE-8D Wire and Cable Committee
This SAE Standard defines the general requirements and provides a system for the control of quality for conformal coatings suitable for application to printed circuit assemblies
AMS G8 Aerospace Organic Coatings Committee
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified-polyvinylidene-fluoride plastic in the form of extra-thin-wall tubing
AE-8D Wire and Cable Committee
This specification covers an irradiated, thermally-stabilized, modified polyolefin plastic in the form of thin-wall, heat-shrinkable tubing with a low recovery temperature
AE-8D Wire and Cable Committee
This specification covers polytetrafluoroethylene-impregnated glass laminates in the form of sheet clad on one or both sides with electrolytically deposited copper foil
AMS P Polymeric Materials Committee
This SAE Aerospace Information Report (AIR) focuses on opportunities, challenges, and requirements in use of blockchain for Unmanned Aircraft Systems (UAS) operating at and below 400 feet above ground level (AGL) for commercial use. UAS stakeholders like original equipment manufacturers (OEMs), suppliers, operators, owners, regulators, and maintenance repair and overhaul (MRO) providers face many challenges in certification, airspace management, operations, supply chain, and maintenance. Blockchain—defined as a distributed ledger technology that includes enterprise blockchain—can help address some of these challenges. Blockchain technology is evolving and also poses certain concerns in adoption. This AIR provides information on the current UAS challenges and how these challenges can be addressed by deploying blockchain technology along with identified areas of concern when using this technology. The scope of this AIR includes elicitation of key requirements for blockchain in UAS across
G-31 Digital Transactions for Aerospace
This SAE Standard establishes practices to: a Manage risk and ensure security of a cyber-physical system (CPS) throughout its life cycle by utilizing systems engineering principles; b Assess the impact of cyber-physical systems security (CPSS) objectives and requirements; c Assess the security risks to CPS technical effectiveness and functions, and address weaknesses and vulnerabilities; d Address various domains of consideration (see 3.1) that take into account operating conditions of the system, command and control, configuration management (refer to SAE EIA649), etc., that could negatively impact CPSS or CPS-designed purpose; e Perform design validation and verification to assess security and risk of the CPS
G-32 Cyber Physical Systems Security Committee
This specification covers the requirements for computer-controlled laser peening of metal part surfaces to induce residual compressive stresses at and beneath the surface
AMS B Finishes Processes and Fluids Committee
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications
AMS AM Additive Manufacturing Metals
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
AMS P Polymeric Materials Committee
This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products
AMS K Non Destructive Methods and Processes Committee
This specification covers one type of high-contrast, fine-grain radiographic film in the form of cut sheets or rolls
AMS K Non Destructive Methods and Processes Committee
This document defines an ILS/MLS/GLS multi-mode receiver that provides the flight path deviation guidance to the aircraft during the final approach and landing phase. The data sources may be Instrument Landing System (ILS), Microwave Landing System (MLS) or GNSS Landing System (GLS). Supplement 4 adds ILS look-alike data (ARINC 429) in support of GLS CAT II/III operation. It also defines Final Approach Segment Data Messages (FASDM) input labels to the MMR for new aircraft
Airlines Electronic Engineering Committee
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
AMS P Polymeric Materials Committee
This specification covers a crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-shrinkable tubing
AE-8D Wire and Cable Committee
This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications
AMS AM Additive Manufacturing Metals
This brief User Guide recaps the content of the AS6518B UCS Architectural Model. The purpose of the UCS Architecture Model is to provide the authoritative source for other models and products within the UCS Architecture as shown in the AS6512B UCS Architecture: Architecture Description
AS-4UCS Unmanned Systems Control Segment Architecture
This specification establishes testing methods for testing chemical composition in nickel- and cobalt-based alloys
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers pyrometric requirements for equipment used for the thermal processing of metallic materials. Specifically, it covers temperature sensors, instrumentation, thermal processing equipment, correction factors and instrument offsets, system accuracy tests, and temperature uniformity surveys. These are necessary to ensure that parts or raw materials are heat treated in accordance with the applicable specification(s
AMS B Finishes Processes and Fluids 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 document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft
Airlines Electronic Engineering Committee
ARINC Specification 802 defines standard fiber optic cable meeting the operational and environmental requirements for the air transport industry. The purpose of this document is to avoid the proliferation of different designs of cables serving the same functions on different airplane models. ARINC Specification 802 comprises three sections. Section 1 provides a general description of the objectives, scope, the types of cable, and the applicable environmental categories. Section 2 addresses the desired physical properties of the fiber optic cables. Section 3 defines the qualification tests that may be used to ensure the cables meet the characteristics provided by this document. A glossary is provided in Appendix A
Airlines Electronic Engineering Committee
This standard provides guidance to those who develop avionics test programs and the source documentation on which they are based. This includes guidelines for all steps and phases within the TPS life cycle
Avionics Maintenance Committee
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