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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 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 specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures
AMS P Polymeric Materials Committee
AS9131 - This standard defines the common nonconformance data definition and documentation that an internal or external supplier or sub-tier supplier must submit when informing a customer of a nonconformity. The requirements shall be are applicable for reporting a nonconforming product to the owner/operator (i.e., end item user), if specified by contract. Reporting of nonconformance data, either electronically or conventionally on paper, is subject to the terms and conditions of the contract. This also includes, where applicable, data access under export control regulations
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine
E-30 Propulsion Ignition Systems Committee
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry
Engine Power Test Code Committee
This specification covers an aluminum alloy in the form of sheet and plate from 0.020 to 1.000 inch (0.51 to 25.4 mm) thick (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings
AMS E Carbon and Low Alloy Steels Committee
This specification covers the engineering requirements for producing a carbon-oxygen-nitrogen-bearing case on titanium and titanium alloys by means of a molten salt bath, and the properties of the case
AMS B Finishes Processes and Fluids Committee
This specification covers a low-modulus aramid in the form of tubular webbing
AMS P Polymeric Materials Committee
This specification establishes the requirements and procedures for producing a hard, wear resistant ion nitrided surface on steel parts
AMS B Finishes Processes and Fluids Committee
This specification covers one width and one breaking strength of low modulus aramid tubular webbing
AMS P Polymeric Materials Committee
The intent of this specification is for the procurement of the material listed on the QPL; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the Quality Assurance section of this base specification, AMS6891
AMS P17 Polymer Matrix Composites Committee
This specification covers a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness (see 8.7
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties
AMS G8 Aerospace Organic Coatings Committee
Aluminum Alloy Plate 4.3Zn - 3.3Mg - o.6Cu - o.2Mn - 0.17Cr (7o79-T651) Stress-Relief Stretched
AMS D Nonferrous Alloys Committee
This specification covers a low-alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
This specification covers a petroleum-based reference oil
AMS CE Elastomers Committee
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings
AMS E Carbon and Low Alloy Steels Committee
This Material Specification defines the requirements of carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures, qualified according to AMS2980/1 and AMS2980/2. Unless otherwise specified by the drawing, the order or the inspection schedule, the present specification shall be used in conjunction with the referenced documents
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification has been "Cancelled" by the Aerospace Materials Division, SAE, as of January 1997
AMS CE Elastomers Committee
AMS B Finishes Processes and Fluids Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE
AMS B Finishes Processes and Fluids Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification covers a copper alloy (phosphor bronze) in the form of sheet, strip, and plate
AMS D Nonferrous Alloys Committee
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt%) greater than 40 mesh (425 µm) is allowed
AMS AM Additive Manufacturing Metals
This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of high density ceramic shot
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of seamless, drawn tubing from 0.025 to 0.500 inches (0.64 to 12.70 mm) in wall thickness (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005-inch (0.13-mm) in nominal thickness (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a low expansion iron alloy in the form of sheet or strip 0.250 inch (6.35 mm) and under in nominal thickness (see 8.7
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a tetrafluoroethylene/propylene rubber (FEPM) in the form of molded rings
AMS CE Elastomers Committee
This specification covers a silicone rubber in the form of a two-component liquid compound
AMS G9 Aerospace Sealing Committee
This specification covers low-carbon steel in the form of bars, forgings, mechanical tubing, sheet, strip, plate, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers low-alloy steel springs made of annealed round wire heat treated after forming
AMS E Carbon and Low Alloy Steels Committee
This specification covers a two-component silicone rubber sealant and compatible primers
AMS G9 Aerospace Sealing Committee
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
AMS6885/5 is the Material Specification (MS) which defines the requirements of a unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. It also defines the requirements of an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of martensitic corrosion-resistant steel parts. Parts are defined in AMS2759. General ordering instructions are specified in AMS2759
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the specific requirements for aluminum alloy 5086, plate and sheet for applications requiring a weldable moderate strength alloy having comparatively and corrosive resistance
AMS D Nonferrous Alloys Committee
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