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This SAE AIR covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. It is intended to provide pressure and temperature (temps pages 26 & 31) information and minimum safety guidelines regarding use of equipment to remove frozen contaminants related to: i) Forced air ii) Forced air/fluid iii) Deicing fluid
G-12M Methods Committee
This information report covers all known aircraft with respect to deicing operations, especially with regard to OEM pressure and temperature limitations on the airframe. It provides data for airlines/operators on compliance with OEM limits and confirms that OEM limits are not exceeded during deicing operations.
G-12M Methods Committee
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
A-5 Aerospace Landing Gear Systems Committee
This specification covers a corrosion-resistant steel in the form of wire.
AMS F Corrosion and Heat Resistant Alloys Committee
The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.
Automatic Transmission and Transaxle Committee
This specification covers a columbium alloy in the form of bars, rods, and extrusions.
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium (niobium) alloy in the form of sheet, strip, and plate.
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium (niobium) alloy in the form of bars, rods, and extrusions.
AMS G Titanium and Refractory Metals Committee
Inclement weather can have a significant impact on surface transportation systems. It can result in hazardous conditions for travelers due to poor visibility, or wet or icy roadways. Weather applications have the potential to provide additional data to surface transportation infrastructure owners and operators, allowing them to better assess the impacts of the weather environment on or around the roadway and to better manage the surface transportation system. Such weather applications can: Collect road weather data from connected vehicles and mobile devices, increasing the number of data sources available. Provide road weather related traveler information to travelers via connected vehicles and devices, such as when and where a hazardous condition exists. Provide the ability to manage road weather response on specific roadways. This SAE Standard specifies interface requirements between vehicles and infrastructure for weather applications, including detailed systems engineering
V2X Core Technical Committee
This document covers the requirements for SAE implementations based on ISO 17987. Requirements stated in this document will provide a minimum standard level of performance to which all compatible systems, design and development tools, software, ECUs, and media shall be designed. This will assure consistent and unambiguous serial data communication among all connected devices regardless of supplier. This document may be referenced by any vehicle OEM component technical specification that describes any given ECU in which the single wire data link controller and physical layer interface is located. The intended audience includes, but is not limited to, ECU suppliers, LIN controller suppliers, LIN transceiver suppliers, component release engineers, and vehicle system engineers. The term “master” has been replaced by “commander” and term “slave” with “responder” in the following sections.
Vehicle Architecture For Data Communications Standards
This SAE Aerospace Information Report (AIR) contains data relative to the chemical nature of aerospace fluids and relates each to its empirical effect upon elastomeric components. Since the compatibilities of elastomers are determined by the compounding as well as the nature of the base polymer, the elastomers considered are limited to finished compounds for which material or performance specifications can be referenced.
A-6C2 Seals Committee
This SAE Recommended Practice establishes uniform requirements and guidelines for the display of capacity information of personal watercraft.
Personal Watercraft Committee
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
This handbook is intended to assist the user to understand the ANSI/EIA-649B standard principles and functions for Configuration Management (CM) and how to plan and implement effective CM. It provides CM implementation guidance for all users (CM professionals and practitioners within the commercial and industry communities, DoD, military service commands, and government activities (e.g., National Aeronautics and Space Administration (NASA), North Atlantic Treaty Organization (NATO)) with a variety of techniques and examples. Information about interfacing with other management systems and processes are included to ensure the principles and functions are applied in each phase of the life cycle for all product categories.
G-33 Configuration Management
This specification covers an aircraft-quality, low-alloy steel in the form of bars.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
AMS E Carbon and Low Alloy Steels Committee
This SAE Standard provides test procedures for air and air-over-hydraulic disc or drum brakes used for on-highway commercial vehicles over 4536 kg (10000 pounds) GVWR. This recommended practice includes the pass/fail criteria of Federal Motor Vehicle Safety Standard No. TP-121D-01.
Truck and Bus Foundation Brake Committee
This specification covers a nickel-copper alloy in the form of castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers molded or extruded bar, rod, and shapes produced from a polyamide-imide (PAI) polymer filled with 30% glass fiber. This is designated as Grade 4 material per AMS3670.
AMS P Polymeric Materials Committee
This specification covers an unfilled polyamide-imide plastic in the form of molded or extruded bar, rod, and shapes. This is designated as Grade 2 material per AMS3670.
AMS P Polymeric Materials Committee
This specification covers polyfluoroethylenepropylene in the form of film and sheet 0.020 inch (0.51 mm) and under in nominal thickness.
AMS P Polymeric Materials Committee
This specification covers the requirements for electrodeposition of tin on metals and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.249 inch (1.02 to 6.32 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars.
AMS E Carbon and Low Alloy Steels Committee
This standard is intended to provide guidance for selecting standardized methods for estimating the proportion nonconforming expressed as PPM. These methods are contained in EIA 554-1, EIA 554-2 and EIA 591.
Systems Management Council
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
AMS P17 Polymer Matrix Composites Committee
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
AMS P17 Polymer Matrix Composites Committee
This specification covers a corrosion and moderate heat resistant steel in the form of plate.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
This specification covers a room-temperature-vulcanizing, elastomeric silicone compound.
AMS G9 Aerospace Sealing Committee
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
This specification covers an age-hardenable nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Figures 1 through 6 illustrate in simplified form some of the more common planetary gears, gearsets, and geartrain arrangements in order to establish applicable terminology. Figures 7 and 8 provide additional examples that use elements of those gear arrangements.
Automatic Transmission and Transaxle Committee
This specification covers a nickel in the form of round wire and rectangular ribbon.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers aircraft-quality bolts and screws having UNJ (MIL-S-8879) thread form, made from a corrosion-resistant, work-strengthened cobalt-chromium-nickel alloy and aged to develop the specified properties.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes.
AMS G Titanium and Refractory Metals Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted.
AMS D Nonferrous Alloys Committee
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