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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 requirements for the acquisition of two types and two classes of material that will remove or loosen carbon from components of internal combustion engines and compressor sections of jet engines
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers three types of semi-solid skin protective compounds in the form of barrier creams
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a concentrated rust removing compound in the form of a liquid to be diluted with water for use either at ambient or elevated temperature
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an acidic deoxidizer in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a polishing compound for aircraft metals in the form of a liquid or paste
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an anti-galling compound remover in the form of a water-soluble powder, a concentrated liquid for dilution with water, or a ready-to-use liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a shampoo type carpet cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a strongly alkaline scale conditioner in the form of a liquid or a water-soluble powder
AMS J Aircraft Maintenance Chemicals and Materials 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 an emulsion-type, low-foaming cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials 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
This specification covers a non-phenolic, non-chromated, thickened paint remover in the form of a solvent-base liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a glass-roving-filled silicone resin in the form of compression moldings or transfer moldings
AMS P Polymeric Materials Committee
This specification covers polytetrafluoroethylene resin in the form of extruded rods, tubes, and shapes
AMS P Polymeric Materials Committee
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 ready-mixed thixotropic compound in the form of a stable film-forming compound suitable for application by brushing or spraying
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a water-miscible, foam-on, pressure spraying cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification establishes the requirements for cleaning compounds, used in parts washers and spray cabinets for cleaning aircraft components
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an emulsion-type, foam-on, pressure-spray cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a water-miscible, low-foaming cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a paint remover in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an alkaline-type, thickened paint remover in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
The task of chemical process operator in the parts cleaning area is generally considered unskilled labor and in the past, little or no training had been provided or recommended. Since overhaul cleaning is a critical process step prior to visual and fluorescent penetrant inspection processes, consideration must be given to minimum levels of training for these process operators. It is the responsibility of the department supervisor to ensure that all personnel within the department are trained to acceptable level in all general aspects of health and safety and basic operating procedures. This document is intended to augment the local quality control system which will control the application and frequency of the guidelines stated within
AMS J Aircraft Maintenance Chemicals and Materials Committee
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 SAE Aerospace Recommended Practice (ARP) covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in a starter crank/soak/rinse application
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a corrosion and heat resistant steel in the form of bars, forgings, and forging stock
AMS F Corrosion and Heat Resistant 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
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