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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 established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range
AMS D Nonferrous Alloys Committee
This specification covers cotter pins made to metric dimensions from a corrosion and heat resistant steel
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of bars, rods, and wire 8.000 inches (203.20 mm) and under in nominal diameter and for squares, hexagons, octagons, and rectangles 50 in2 (322 cm2) and under in cross-sectional area and 8.000 inches (203.20 mm) and under in least distance between parallel sides (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in diameter or least distance between parallel sides and stock for forging or flash welded rings of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
This specification covers a heat-resistant iron-nickel alloy in the form of bars, wire, forgings, flash welded rings. Product covered by this specification is limited to 8.0 inches (203 mm) and under in nominal diameter or maximum cross sectional dimension between parallel sides (thickness), and stock of any size for forging or flash welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers pyrometric requirements for equipment used for the thermal processing of metallic materials. Specifically, it covers temperature sensors, instrumentation, thermal processing equipment, correction factors and instrument offsets, system accuracy tests, and temperature uniformity surveys. These are necessary to ensure that parts or raw materials are heat treated in accordance with the applicable specification(s
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of two types of tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a zinc alloy in the form of die castings
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings 8.0 inches (200 mm) and under in in thickness, diameter or for hexagons least nominal cross-sectional dimension, and stock of any size for forging or flash welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for preparation of aluminum and aluminum alloys for soldering by zinc immersion pre-treatment followed by copper plating and tin or tin-zinc alloy plating
AMS B Finishes Processes and Fluids Committee
This Aeronautical Standard covers terms frequently applied to aircraft gas turbine engines and their operation but does not include names of particular parts, the latter being covered by AS 341, Drawing Title Rules and Nomenclature for Aircraft Engine Parts
AGE-4 Packaging, Handling and Transportability Committee
These products have been used typically for electrodeposited nickel plating on steel, copper and copper alloys, and zinc and zinc alloys, but usage is not limited to such applications
AMS B Finishes Processes and Fluids Committee
This specification covers a nitrile rubber (NBR) in the form of molded compression seals such as O-rings, T-seals, and molded-in-place gaskets for aeronautical and aerospace applications. For sheet, strip, tubing, extrusions, and molded shapes, use the AMS3786 specification, which is intended for that use
AMS CE Elastomers Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.1874 inch (4.76 mm) and under in nominal thickness
AMS F Corrosion and Heat Resistant Alloys Committee
This Purchasing Specification, AMS6885/3, specifies the batch release and delivery requirements for unidirectional carbon fiber tape epoxy prepreg used for repair. This specification is applicable only when the unidirectional carbon fiber tape epoxy prepreg is used as part of the repair system defined in AMS6885 and AMS6885/1. This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885) and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 5.000 inches (127.00 mm), inclusive in nominal diameter or least thickness (bars, rods, wire, profiles) or nominal wall thickness (tubing) (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, profiles, and tubing
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of die forgings and hand forgings up to 6.000 inches (152.40 mm) in nominal thickness at the time of heat treatment (see 8.4
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in diameter, or least distance between parallel sides and stock of any size for forging or flash welded rings (see 8.8
AMS G Titanium and Refractory Metals Committee
This specification covers the specific requirements for 5086 aluminum alloy plate and sheet; the general requirements are covered in AMS-QQ-A-250
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of sheet 0.020 to 0.1874 inch (0.51 to 4.760 mm), inclusive, in nominal thickness. (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion and heat-resistant cobalt alloy in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aircraft quality, low alloy chrome-nickel-molybdenum steel (8620) in the form of bars
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of sheet 0.040 to 0.249 inch (1.02 to 6.32 mm) in nominal thickness (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel product 8 inches (203 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 64 square inches (413 cm2) in the solution and precipitation heat treated (H900) condition
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
This specification establishes testing methods for testing chemical composition in nickel- and cobalt-based alloys
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for producing brazed joints of aluminum and aluminum alloys by immersion in a molten flux bath
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion and heat-resistant steel in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
Primarily for use as filler metal for gas-metal-arc and gas-tungsten-arc welding, including repair welding, of aluminum alloy castings. Where casting service conditions require good corrosion resistance, maximum strength, and homogeneity, filler metal should be of the same alloy as the casting
AMS D Nonferrous Alloys Committee
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4045, ALUMINUM ALLOY SHEET AND PLATE (7075; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4045 shall be fulfilled whenever reference is made to this specification
AMS D Nonferrous Alloys Committee
This specification covers a low-alloy strip clad on one or both faces with silver in the form of bearing stock or finished bearings
AMS D Nonferrous Alloys Committee
This specification covers the requirements for an aluminum brazing flux in the form of powder or paste
AMS B Finishes Processes and Fluids Committee
This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of round, seamless tubing having a wall thickness not greater than 0.188 inch (4.78 mm
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion and heat resistant steel in the form of sand castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers one type of copper-nickel alloy in the form of wire and ribbon
AMS D Nonferrous Alloys Committee
This specification covers a moderate corrosion and heat resistant alloy iron in the form of sand castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of extruded or drawn welding wire
AMS D Nonferrous Alloys Committee
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