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This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods used to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included
Aircraft Seat Committee
This SAE Aerospace Recommended Practice (ARP) provides recommendations for: The audit process in general A list of specific areas of attention to be audited Maintaining the test facility in such a manner that it meets audit requirements
EG-1E Gas Turbine Test Facilities and Equipment
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
This specification establishes the requirements, controls, procedures, and quality assurance requirements for fabrication of flat, adhesive-bonded, aluminum-alloy-faced sandwich structure panels using one of three basic core materials: paper honeycomb, polyurethane foam, or aramid-paper-base honeycomb
AMS P Polymeric Materials 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
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
OBJECT: Primarily to make porous magnesium alloy castings pressure tight
AMS D Nonferrous Alloys Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one type of nylon loop tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers a prepolymer in the form of a low molecular weight aromatic diglycidyl ester resin
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers an aluminum alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet
AMS D Nonferrous Alloys Committee
This specification covers a two-component system composed of a non-polyester urethane resin and a hardener, supplied in kit form
AMS P Polymeric Materials Committee
This specification and its supplementary detail specifications cover an aromatic polyamide in the form of cord
AMS P Polymeric Materials Committee
This specification covers one type of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification covers one type of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification and its supplementary detail specifications cover two types of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification covers two types of a twill nylon/rayon in the form of cloth
AMS P Polymeric Materials Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings
AMS E Carbon and Low Alloy Steels Committee
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 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 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 covers an aluminum alloy in the form of sheet
AMS D Nonferrous Alloys 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 specification covers an aluminum alloy in the form of sheet
AMS D Nonferrous Alloys Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one strength and weight of braided para-aramid cord
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers one strength and weight of braided para-aramid cord
AMS P Polymeric Materials Committee
This specification covers one strength and weight of braided para-aramid cord
AMS P Polymeric Materials Committee
This specification covers one strength and weight of braided para-aramid cord
AMS P Polymeric Materials Committee
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