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The scope of this SAE performance standard is to provide a simple, practical, and broadly applicable test procedure for appraising luminous Illuminant A reflectance of reflecting safety glazing materials for road vehicles. This SAE performance standard, which provides a simple test procedure widely used in the optics field, may be used to measure the reflectivity which films applied to safety glazing materials for road vehicles may enhance. This test procedure applies to conditions where feasibility, rather than accuracy of measurement, is of prime importance. Measurements can be made outside laboratories in a quality control environment and in similar applications, when glazings, instead of small test specimens, have to be tested.
Glazing Materials Standards Committee
This specification covers the requirements for procurement of one grade of powdered molybendum disulfide to be used in lubricants and greases for surfaces where boundary conditions exist.
AMS B Finishes Processes and Fluids Committee
This specification covers treated aluminum core material for structural sandwich construction.
AMS P17 Polymer Matrix Composites Committee
This specification covers cored and uncored open cell latex foam rubber sheets, molded and hand- built shapes having good shock-absorbing, vibration-damping, and comfort cushioning characteristics (see 6.1).
AMS P Polymeric Materials Committee
This specification covers the requirements for surface bonded laminated shim stock.
AMS D Nonferrous Alloys Committee
This specification covers the requirements for glass fabric base plastic honeycomb core materials for aircraft structural applications, including aircraft exterior parts, such as radio and radar antenna housings, and other parts.
AMS P17 Polymer Matrix Composites Committee
This specification presents the requirements for one type of a heat-sensitive recording paper, in roll form, that furnishes permanent marking or tracing on one side.
AMS P Polymeric Materials Committee
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
This specification covers electric furnace steel bars and reforging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
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 covers class L, low dielectric constant (12 or under), ceramic, electrical, insulating compounds, for use in electronic, communications, and allied electrical equipments, and the grading thereof (see 6.1).
AMS P Polymeric Materials Committee
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 microns) and that no powder (0.0 wt.%) greater than 40 mesh (425 microns) is allowed.
AMS AM Additive Manufacturing Metals
This specification covers steel forgings suitable for use in the construction of aircraft/aerospace equipment, special ordnance, and related accessories.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the requirements for electroless (autocatalytic chemical reduction) deposition of nickel-phosphorous alloy coatings on metal and composite surfaces.
AMS B Finishes Processes and Fluids Committee
This specification covers a magnesium alloy in the form of sand castings (see 8.6).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Standard (AS) provides design criteria for onboard stairways intended for use by passengers aboard multi-deck transport category airplanes. It is not intended for stairways designed for use only by crewmembers, supernumeries, or maintenance personnel. Additionally, this AS does not apply to fuselage mounted or external stairways used for boarding passengers, which are covered by ARP836.
S-9B Cabin Interiors and Furnishings Committee
This specification covers the requirements for a hard anodic coating on magnesium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of plate 3.000 to 6.000 inches (76.20 to 152.40 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers bonded honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered (see 8.5).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Recommended Practice (ARP) describes terminology specific to unmanned systems (UMSs) and definitions for those terms. It focuses only on terms used exclusively for the development, testing, and other activities regarding UMSs. It further focuses on the autonomy and performance measures aspects of UMSs and is based on the participants’ earlier work, the Autonomy Levels for Unmanned Systems (ALFUS) Framework, published as NIST Special Publication 1011-I-2.0 and NIST Special Publication 1011-II-1.0. This Practice also reflects the collaboration results with AIR5665. Terms that are used in the community but can be understood with common dictionary definitions are not included in this document. Further efforts to expand the scope of the terminology are being planned.
AS-4JAUS Joint Architecture for Unmanned Systems Committee
This SAE Aerospace Information Report (AIR) discusses the nature of landing gear stability, describes many common landing gear stability problems, and suggests approaches and methods for solving or avoiding them.
A-5 Aerospace Landing Gear Systems Committee
This specification covers grease for use within an aircraft. It also defines the quality control requirements to assure batch conformance and materials traceability and the procedures to manage and communicate changes in the grease formulation and brand. This specification invokes the Performance Review Institute (PRI) product qualification process. Requests for submittal information may be made to the PRI at the address in 2.2, referencing this specification. Products qualified to this specification are listed on a Qualified Products List (QPL) managed by the PRI. Additional tests and evaluations may be required by individual equipment builders before a grease is approved for use in their equipment. Approval and/or certification for use of a specific grease in aero and aero-derived marine and industrial applications is the responsibility of the individual equipment builder and/or governmental authorities and is not implied by compliance with or qualification to this specification.
AMS M Aerospace Greases Committee
This specification establishes the requirements for a waterborne, corrosion-inhibiting, chemical- and solvent-resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C).
AMS G8 Aerospace Organic Coatings Committee
This specification covers grease for use on aircraft wheel bearings. It also defines the quality control requirements to assure batch conformance and materials traceability and the procedures to manage and communicate changes in the grease formulation and brand. This specification invokes the Performance Review Institute (PRI) product qualification process. Requests for submittal information may be made to the PRI at the address in 2.2, referencing this specification. Products qualified to this specification are listed on a qualified products list (QPL) managed by the PRI. Additional tests and evaluations may be required by individual equipment builders before a grease is approved for use in their equipment. Approval and/or certification for use of a specific grease in aero and aero-derived marine and industrial applications is the responsibility of the individual equipment builder and/or governmental authorities and is not implied by compliance with or qualification to this
AMS M Aerospace Greases Committee
The document provides clarity related to multiple temperature coolant circuits used with on-highway and off-highway, gasoline, and light-duty to heavy-duty diesel engine cooling systems, or hybrid vehicle systems. These multiple temperature systems include engine jacket coolant plus at least one lower temperature system. Out of scope are the low temperature systems used in electric vehicles. This subject is covered in SAE J3073. Note that some content in SAE J3073 is likely to be of interest for hybrid vehicles. Out of scope are the terms and definitions of thermal flow control valves used in either low-temperature or high-temperature coolant circuits. This subject is covered in SAE J3142.
Cooling Systems Standards Committee
This SAE Recommend Practice establishes for passenger cars, light trucks, and multipurpose vehicles with GVW of 4500 kg (10000 pounds) or less, as defined by the EPA, and M1 category vehicles, as defined by the European Commission:
Interior Climate Control Vehicle OEM Committee
This specification establishes the requirements for fabricated products of vulcanized rubber, synthetic rubber or rubberlike compositions alone or in combination, together with procedures for the inspection of such products (see 6.1).
AMS CE Elastomers Committee
This specification covers the requirements of composite blankets suitable for acoustical and thermal insulation of the walls of aircraft compartments within the temperature range of -65°F to +175°F (-54°C to +80°C).
AMS CE Elastomers Committee
This specification covers the general requirements for aluminum and aluminum alloy tube; drawn, seamless (see 6.1.1). Specific requirements for these products in a particular alloy are covered by the applicable detail specification (see 6.3).
AMS D Nonferrous Alloys Committee
This AIR provides means of developing a composite training program, as stipulated by FAA AC 20-107B, FAA AC 65-33A, EASA AMC 20-29, and other similar regulatory guidance. Its approach is a comprehensive, sequential training curriculum build-up, customized to the specific needs of the organization (see Figure 2). It contains recommendations for the skill-building, training, and qualification of persons involved in the design, fabrication, maintenance, and repair of aircraft composite structures or other aviation composite components. It further addresses the qualification of administrative personnel and instructors. Flight operations are usually not in the scope of an SAE CACRC Standard; however, the recommendations of this report may be used also for this target audience. This report addresses persons responsible for the definition of training, qualification and authorization, or the supervision of aviation personnel. Its content intends to facilitate the development of a formal
AMS CACRC Commercial Aircraft Composite Repair Committee
This document covers the dimensional definition of the SAE J3400 (NACS) electric vehicle coupler, which includes the connector and inlet.
Hybrid - EV Committee
This specification presents requirements for thin-walled (inside diameter greater than four times the wall thickness and outside diameter 1/4 inch and larger) corrosion-resistant steel tubing in approximately the 1/8 hard condition, of special quality, suitable for use in high-pressure hydraulic systems.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Recommended Practice (ARP) establishes general criteria for the installation (e.g., type, location, accessibility, stowage) and crew member training needed for portable fire extinguishers.
S-9A Safety Equipment and Survival Systems Committee
This document recommends standard gland dimensions for static radial O-ring seal applications specifically for engine and engine control systems and provides recommendations for modifying these glands in special applications.
A-6C2 Seals Committee
This specification covers three types of rubber having good resistance to high and low temperature and hydrazine type propellants, but poor resistance to hydrocarbon oils or solvents. Hydrazines are hazardous chemicals. See “Dangerous Properties of Industrial Materials” by N. Irving Sax.
AMS CE Elastomers Committee
The purpose of this military standard is to prescribe the non-destructive testing acceptance criteria for the inspection of metal castings that are classified (see 1.3) in accordance with this standard.
AMS B Finishes Processes and Fluids Committee
This specification covers a series of iron-nickel, iron-nickel-cobalt, and iron-nickel-chromium alloys used for sealing to glasses and ceramics in electronic applications (see 6.1).
AMS F Corrosion and Heat Resistant Alloys Committee
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