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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 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 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 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 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 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 specification covers a process for surface-hardening parts, made from appropriate low-alloy steels (See 8.4), by the introduction of nitrogen from ammonia
AMS B Finishes Processes and Fluids Committee
This specification covers two types of magnetic nickel-iron alloy in the form of sheet and strip
AMS E Carbon and Low Alloy Steels Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a low-alloy steel in the form of sand castings
AMS E Carbon and Low Alloy Steels Committee
This specification covers a propylene-glycol base, deicing/anti-icing fluid in the form of a concentrated liquid
G-12ADF Aircraft Deicing Fluids
The purpose of this document is to present general considerations for the design and use of aircraft wheel chocks. The design and use of aircraft wheel chocks is a good deal more complicated than it may appear at first glance
AGE-3 Aircraft Ground Support Equipment Committee
This Aerospace Recommended Practice (ARP) provides criteria for operational characteristics to be considered in the design of individual, inflatable life preservers intended for air transport safety
S-9A Safety Equipment and Survival Systems Committee
This specification covers a low-alloy steel in the form of covered welding electrodes
AMS F Corrosion and Heat Resistant Alloys Committee
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers the specific requirements for 2024 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy 2024 core with thin layers of an aluminum alloy 1230 (99.30 percent minimum aluminum) anodic to the core and of approximately equal thickness, bonded to both surfaces
AMS D Nonferrous Alloys Committee
This specification covers steel of aircraft quality for use in the manufacture of nitrided parts (see 6.1
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of seamless tubing
AMS F Corrosion and Heat Resistant Alloys 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 chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality
AMS E Carbon and Low Alloy Steels 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
The purpose of this standard is to provide uniform physical item identification marking, in constantly recurring symbols, of nickel and nickel alloy mill products procured and issued for government agencies and their contractors. Applicability shall be by specific reference to this standard in specification, contract, or purchase order. Shipment and inspection acceptance markings are not within the scope of this document
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings and stock for flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers the specific requirements for 5083 aluminum alloy plate and sheet; the general requirements are covered in AMS-QQ-A-250
AMS D Nonferrous Alloys Committee
This specification covers one weight of low-modulus aramid tape
AMS P Polymeric Materials Committee
This specification covers one type of nylon webbing
AMS P Polymeric Materials Committee
This specification covers an elastomeric silicone insulating and sealing compound, supplied as a two-component system. The compound may be either an addition- or a condensation-cure type
AMS G9 Aerospace Sealing Committee
This specification covers a silicone resin in the form of a two-component liquid
AMS G9 Aerospace Sealing Committee
This specification covers a silicone rubber in the form of a two-component liquid compound
AMS G9 Aerospace Sealing Committee
This specification covers a room-temperature-vulcanizing, elastomeric silicone compound in the form of a base compound and a catalyst
AMS G9 Aerospace Sealing Committee
This specification covers a room-temperature-vulcanizing, elastomeric silicone compound
AMS G9 Aerospace Sealing Committee
This specification covers an alkaline cleaner in the form of a liquid for use above 65 °C (154 °F
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife
AMS G9 Aerospace Sealing Committee
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