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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
SAE J3072 establishes requirements for a grid support inverter system function that is integrated into a plug-in electric vehicle (PEV), which connects in parallel with an electric power system (EPS) by way of conductively coupled, electric vehicle supply equipment (EVSE). This standard also defines the communication between the PEV and the EVSE required for the PEV onboard inverter function to be configured and authorized by the EVSE for discharging at a site. The requirements herein are intended to be used in conjunction with IEEE 1547-2018 and IEEE 1547.1-2020 or later versions
Hybrid - EV Committee
This specification covers tapes for masking during paint stripping operations (see 6.1
AMS G8 Aerospace Organic Coatings Committee
This specification covers “E” glass in the form of woven cloth
AMS P17 Polymer Matrix Composites Committee
This specification covers an ethylene propylene elastomer in the form of molded sheet and shapes, color coded purple per ARP1527
AMS CE Elastomers Committee
This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cords, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection this material
AMS CE Elastomers Committee
This specification covers an ethylene propylene (EPDM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes
AMS CE Elastomers Committee
This specification covers a silicone rubber sponge in the form of sheet, strip, extrusions, and molded shapes
AMS CE Elastomers Committee
This specification covers a silicone rubber sponge in the form of sheet, strip, extrusions, and molded shapes
AMS CE Elastomers 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 SAE Standard specifies the properties of chromate conversion coatings on aluminum and aluminum alloys. It details inspection and testing requirements for chromate conversion coatings
AMS B Finishes Processes and Fluids Committee
The foundation specification (AMS3050) and this category specification (AMS3050/6) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Nickel and Graphite only
AMS M Aerospace Greases Committee
This specification covers a magnesium alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.750 inch (0.25 to 44.45 mm) in thickness, supplied in the annealed (O temper) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers the specific requirements for aluminum alloy 5456 bar, rod, shapes, tube, and wire produced by extrusion
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars and forgings up through 10.000 inches (254.00. mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 79.0 in2 (506.45 cm2) and forging stock of any size (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion-resistant steel in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the specific requirements for 2024 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of castings
AMS D Nonferrous Alloys Committee
This specification covers a palladium-silver alloy in the form of round wire 0.004 to 0.080 inch (0.10 to 2.03 mm) inclusive, in nominal diameter (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant steel in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers established inch/pound manufacturing tolerances applicable to carbon and alloy tubing ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range
AMS E Carbon and Low Alloy Steels Committee
This specification covers a high-expansion steel in the form of bars 1.063 inch (27 mm) and under in nominal diameter or distance between parallel sides
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the specific requirements for seamless tube drawn from aluminum alloy 2024
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat resistant steel in the form of bars, wire, and forgings 7.0 inches (178 mm) and under in nominal diameter or least distance between parallel sides, and forging stock of any size (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for electroless nickel deposited on various materials
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant alloy ductile iron in the form of sand castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification and its supplementary detail specifications cover carbon fibers in the form of continuous multifilament tow and yarn
AMS P17 Polymer Matrix Composites Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials Committee
This specification covers one width and one breaking strength of low-modulus aramid webbing
AMS P Polymeric Materials 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 magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles
AMS D Nonferrous Alloys Committee
This specification covers one type of quartz cloth impregnated with a heat-reactive, thermosetting, hot-melt, addition-type, polyimide resin system, furnished in continuous rolls of full width material
AMS P17 Polymer Matrix Composites Committee
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation
AMS P17 Polymer Matrix Composites Committee
This specification covers virgin, unfilled polytetrafluoroethylene (PTFE) in the form of extruded rods, tubes, and profiles
AMS P Polymeric Materials Committee
This specification covers nylon-cloth-reinforced acrylonitrile-butadiene (NBR) rubber in the form of sheet and of shapes molded and cured from partly cured sheet
AMS P Polymeric Materials Committee
This specification covers a woven nylon cloth coated with polyether (EU)urethane
AMS P Polymeric Materials Committee
This specification covers a woven nylon cloth coated with polyether (EU) urethane
AMS P Polymeric Materials Committee
This specification covers a glass cloth impregnated with a heat-curable epoxy resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls
AMS P17 Polymer Matrix Composites Committee
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