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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 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 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)
This is the Microsoft Word® version of AS9101C, which defines the content and the presentation of the Assessment Report for the AS9100 standard. AS9101CW is an historical document; a newer version, AS9101DW, exists
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This Aerospace Standard establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module bolts and nuts
E-25 General Standards for Aerospace and Propulsion Systems
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 the requirements for four classes of machinable, high density tungsten base metal produced by consolidation of metal powder mixtures whose composition is mainly tungsten. This material may be used for uncoated parts or parts that may be coated with other materials for protection against corrosion and abrasion such as, electrodeposited and vacuum deposited cadmium and electrodeposited chromium. Detailed requirements for coatings should be covered in the applicable part drawing, when required
AMS G Titanium and Refractory Metals Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996
AMS P Polymeric Materials Committee
AMS P Polymeric Materials Committee
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1991
AMS P17 Polymer Matrix Composites Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
Primarily for preservation, during extended periods of shipment and/or storage, of miscellaneous metal parts, tools, subassemblies, and equipment where the compound is readily accessible for removal and removal does not damage the parts
AMS B Finishes Processes and Fluids Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification covers a biodegradable, formaldehyde-base material, containing additives, in the form of a concentrated liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE
AMS B Finishes Processes and Fluids Committee
This specification establishes requirements for aerosol packaging
AMS B Finishes Processes and Fluids Committee
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant, premium aircraft-quality alloy steel in the form of bars, forgings, and stock for forging
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate
AMS E Carbon and Low Alloy Steels 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 a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife
AMS G9 Aerospace Sealing 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 an aluminum alloy in the form of rolled or forged rings up to 6 inches (152 mm), inclusive, in thickness (see 3.3.1.2.1), and an OD to wall thickness ratio of 10 or greater (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of flash welded rings 0.062 to 4.499 inches, incl (1.57 to 114.27 mm incl) in radial thickness, with cross sectional areas up to 32 in2 (206 cm2) (see 8.5
AMS D Nonferrous Alloys Committee
AMS P Polymeric Materials Committee
This specification covers a two-component air-curing resin-baue material in the form of a paste or putty, suitable for application by spatula or putty knife
AMS G9 Aerospace Sealing Committee
This specification has been declared 'CANCELLED' by the Aerospace Materials Division, SAE, as of January 1996. Alloy: 2024-T6 UNS Number: A92024
AMS D Nonferrous Alloys 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 covers a corrosion and heat-resistant nickel-iron alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys 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
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
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
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