Search
Advanced Search
of the following are true

Results

Items (207,248)
This specification covers a corrosion-resistant steel in the form of wire
AMS F Corrosion and Heat Resistant Alloys Committee
To provide specifications for lighting and marking of industrial wheeled equipment whenever such equipment is operated or traveling on a highway
OPTC3, Lighting and Sound Committee
This specification covers a corrosion- and heat-resistant steel in the form of seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings 1.50 inches or less in diameter or least distance between parallel sides (thickness
AMS E Carbon and Low Alloy Steels Committee
This specification covers a rust removing compound in the form of a solid, generally powdered, to be dissolved in water, and heated
AMS J Aircraft Maintenance Chemicals and Materials Committee
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design of flanges on temperature sensors intended for use in gas turbine engines. Three figures detail the configuration of standard size flange mounts with bolt holes, slotted flanges, and miniaturized flanges for small probes
E-32 Aerospace Propulsion Systems Health Management
This SAE Aerospace Recommended Practice (ARP) defines the nomenclature of temperature measuring devices. General temperature measurement related terms are defined first, followed by nomenclature specifice to temperature measuring devices, particularly thermocouples
E-32 Aerospace Propulsion Systems Health Management
This Aerospace Recommended Practice (ARP) is a general overview of typical airborne engine vibration monitoring (EVM) systems applicable to fixed or rotary wing aircraft applications, with an emphasis on system design considerations. It describes EVM systems currently in use and future trends in EVM development. The broader scope of Health and Usage Monitoring Systems, (HUMS) is covered in SAE documents AS5391, AS5392, AS5393, AS5394, AS5395, AIR4174. This ARP also contains the essential elements of AS8054 which remain relevant and which have not been incorporated into Original Equipment Manufacturers (OEM) specifications
E-32 Aerospace Propulsion Systems Health Management
This document has been prepared and issued to provide information and guidance on the application of AQAP 2110 when the Supplier adheres to the provisions of 9100. This document is published as AQAP 2009 Annex F and 9137. It was jointly developed by NATO and industry representatives for use by NATO and industry to facilitate the use and understanding of the relationship between the AQAP 2110 and 9100
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE practice is intended for the sample preparation of test pieces for automotive wheels and wheel trim. The practice provides a consistent scribing method for use on test panels and or component parts with substrate chemical pretreatment and coating systems. Test specimens can then be subjected to various corrosion tests in order to evaluate performance without significant variations of the degree of exposure of the substrate. The scribing is used to create a break in the coating/finishing as can occur in the field through gravel and other damaging conditions. NOTE— Significant variability is attributed to surface contour, coating hardness/softness, operator reproducibility, and the scribing tool and it’s condition
Wheel Standards Committee
This document establishes the requirements for a lightweight, nonkink, flexible elastomeric hose. This hose is typically used with air-operated aircraft ice-preventive systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
AGE-4 Packaging, Handling and Transportability Committee
This SAE Aerospace Information Report (AIR) addresses the following: a Perceptions which inhibit the introduction of probabilistic methods b Technical limitations of probabilistic methods c Recommendations to help promote the use of probabilistic methods The document does not contain technical details of probabilistic methods, applications or benchmarking of specific approaches. These subjects are covered in other AIRs, referenced in Section 2 and prepared by the Probabilistic Methods Committee of the G-11 Reliability, Maintainability, Supportability and Logistics (RMSL) Division of SAE
G-11 Probabilistic Methods and Uncertainty Quantification
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
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 130 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F
E-25 General Standards for Aerospace and Propulsion Systems
To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of seamless tubing
AMS G Titanium and Refractory Metals Committee
This specification covers a premium-aircraft-quality, low-alloy steel in the form of sheet, strip, and plate
AMS E Carbon and Low Alloy Steels Committee
To provide a recommended practice covering the method criteria for defining 'wear limit' on involute splines. This recommended practice is applicable to all involute splines used in Aerospace Propulsion Units
EG-1 Aerospace Propulsion Systems Support Equipment
This SAE Aerospace Recommended Practice (ARP) recommends criteria for an Electronic Data Management System (EDMS) for use on the flight deck of transport aircraft. The EDMS may be the primary, and in some cases sole, on board source of documentation and information for flight operations, engineering, aircraft maintenance, cabin services, and training. This document addresses flight operations applications only. It addresses the requirements for the flight deck characteristics of airborne equipment elements for an Electronic Data Management System (EDMS), but not the ground support system requirements. Development of ground support systems for EDMS will be a significant task, which must take account of the end-user information handing requirements specified here. An Electronic Library System (ELS) is a partial implementation of EDMS, which incorporates only the data storage, retrieval and display functions. The appropriate aspects of this document are applicable to Electronic Library
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
This procedure is intended to apply to fuel pumps. This procedure will be defined in terms of recommended test fluid, test setup, test conditions, and test method. This procedure may be used for other fuel system components, by testing in conjunction with the pump, which normally supplies the component inlet flow, or a substitute test pump of similar capacity. This procedure may be used, with variations in test conditions and test fluid for performing pump evaluation tests. Tests at progressively increasing pump speeds and pressures will provide design limitation data. Alternate test periods on a test pump and another pump, of a design for which actual service durability is known, will provide useful comparison data
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity) in the forward field of view. The HUD total system requirement recommendations shall primarily lead to certifiable fail-passive CAT III characteristics and performance. This document forms a part of these recommendations. This document does not address devices for peripheral vision of displays worn by the pilot, nor the presentation of Enhanced Vision System (EVS) information
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
This SAE Aerospace Recommended Practice (ARP) establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 345 to 689 kPa (50 to100 psig
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
This document establishes the temperature types and pressure classes that are commonly used in aerospace fluid systems. The temperature types and pressure classes are equivalent, but not identical, to the SI units defined in MA2001 (ISO 6771). For exact conversion use NAS 10000
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
E-25 General Standards for Aerospace and Propulsion Systems
This document specifies that black is the only color that can be used for the insulator at the bottom of the base of T-1 and T-1 ¾ Flanged Base lamps
A-20A Crew Station Lighting
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of November 1994. It is recommended, therefore, that this specification not be specified for new designs
AMS E Carbon and Low Alloy Steels 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
This standard defines the air transport industry's standards for the transfer of digital data between avionics system elements. Part 2 provides the formats of data words with discrete bit encoding
Airlines Electronic Engineering Committee
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer
Airlines Electronic Engineering Committee
This standard defines standards for loadable software parts and software transport media. It describes the principles and rules to be applied to any part of a data load system, to ensure compatibility and interoperability. It includes part numbering, content, labeling and formatting of loadable software parts and software transport media
Airlines Electronic Engineering CommitteeAvionics Maintenance Committee
This standard covers stall warning instruments to provide positive warning to the pilot of an impending stall. Stall, as defined for the purpose of this standard, is the minimum steady flight speed at which the airplane is controllable
A-4 Aircraft Instruments Committee
This SAE Aerospace Recommended Practice (ARP) lists wrenching surface sizes and tolerances for fluid fittings which utilize machined or unmachined hex bar dimensions and machined or forged wrenching surfaces across the center body section of shape fittings
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Items per page:
1 – 50 of 207248