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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 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 standard specifies the communications hardware and software requirements for fueling hydrogen surface vehicles (HSV), such as fuel cell vehicles, but may also be used where appropriate with heavy-duty vehicles (e.g., buses) and industrial trucks (e.g., forklifts) with compressed hydrogen storage. It contains a description of the communications hardware and communications protocol that may be used to refuel the HSV. The intent of this standard is to enable harmonized development and implementation of the hydrogen fueling interfaces. This standard is intended to be used in conjunction with the hydrogen fueling protocols in SAE J2601 and nozzles and receptacles conforming with SAE J2600
Fuel Cell Standards Committee
This specification covers a water-base cleaner in the form of a concentrated liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers expanded honeycomb core made of fibrous aramid paper sheets and supplied in the form of blocks, slices, and ordered shapes
AMS P17 Polymer Matrix Composites Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 10/17/90
AMS CE Elastomers Committee
This specification covers one type of polyethylene film in the form of rolls of sheeting or reels of unperforated tape of the width specified
AMS P17 Polymer Matrix Composites 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 polythioether sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature. The compound has been used typically for faying surface sealing and for wet-installation of fasteners in aircraft structural joints, but usage is not limited to such applications. This compound is also suitable for fillet sealing and overcoating fasteners in nonfuel areas. The sealing compounds are usable from -65 to +320 degrees F (-54 to +160 degrees C) with short term (six hour) exposures up to 36 degrees F (182 degrees C
AMS G9 Aerospace Sealing Committee
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5598 is the inch/pound version of this MAM
AMS F Corrosion and Heat Resistant Alloys Committee
This specification provides requirements and procedures for air-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers a low-alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
This specification provides requirements and procedures for air-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers two types of thickened, water base temporary coating remover in the form of an alkaline liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified
AMS P17 Polymer Matrix Composites Committee
This specification and its supplementary detail specifications cover interleaf carrier materials in the form of polyethylene film or coated paper tape or sheeting
AMS P17 Polymer Matrix Composites Committee
This specification covers an aluminum bronze alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of July 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED
AMS G9 Aerospace Sealing Committee
This specification covers an arc-cast molybdenum alloy in the form of sheet, strip, and plate
AMS G Titanium and Refractory Metals Committee
This specification covers the requirements for one grade of a specialty lubricating oil for use in precision instrument and miniature ball bearings
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
No Scope available
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers low, medium, and high density polyethylene and copolymers molding and extrusion material for general purpose use, for use as dielectric material, and for weather-resistant applications (see 6.1). For the purpose of this specificaiton, the term polyethylene is used when referring to any of the types, classes, grades, and categories
AMS P Polymeric Materials Committee
This specification covers a corrosion and heat-resistant steel in the form of seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system
AMS G9 Aerospace Sealing Committee
This specification provides requirements and procedures for gas-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers corrosion-preventive organic substances dissolved or emulsified in a volatile solvent and supplied in the form of a ready-to-use liquid
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of bars and rods 0.375 to 0.874 inch (9.52 to 22.20 mm) in nominal diameter or least distance between parallel sides
AMS D Nonferrous Alloys Committee
This standard establishes uniform physical item identification marking in constantly recurring symbols for selected iron and steel products which are procured and issued for Government agencies. Shipment and inspection acceptance marking are not within the scope of this standard. The marking requirements of this standard are applicable when included in the item specification or individual contract. Government decision to include the marking requirements of this standard in a Government specification for iron and steel products shall be subject to coordination between the Government and the iron and steel industry
AMS E Carbon and Low Alloy Steels Committee
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers a low-alloy steel in the form of bars, forgings, and forging stock. Primarily for parts of small cross-section, such as needle bearings, requiring a through-hardening steel usually with hardness of approximately 60 HRC and subject to very rigid inspection standards
AMS E Carbon and Low Alloy Steels Committee
This specification covers a premium aircraft-quality alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
This specification covers a magnesium alloy in the form of die forgings, hand forgings, rolled rings, and forging stock
AMS D Nonferrous 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 one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3138D. Cancelled specifications are available from SAE
AMS G8 Aerospace Organic Coatings Committee
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 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 a cleaner in the form of a ready-to-use liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a corrosion and moderate heat resistant steel in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system
AMS G9 Aerospace Sealing Committee
This specification covers an alkaline rust remover compound in the form of a liquid concentrate or a water-soluble powder for dilution with water
AMS J Aircraft Maintenance Chemicals and Materials 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 standard establishes the procedure for qualification of welders and welding operators engaged in the welding of aircraft, missiles, other aerospace equipment, and their parts and accessories by fusion welding processes. This standard is applicable to aircraft, missile, and aerospace ground support equipment or other welding, when included in the contracting documents or when invoked in the absence of a specified welder qualification document
AMS B Finishes Processes and Fluids Committee
This specification covers alloy and carbon steel castings made by the investment precision casting process. (See 6.1
AMS E Carbon and Low Alloy Steels Committee
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