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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 defines the requirements for a PTFE lined, non-metallic, aramid reinforced assembly suitable for use to 135°C and 28 000 kPa aircraft and missile hydraulic and pneumatic systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
The Environmental Control Analysis SYstem (EASY) computer program is summarized in this report. Development of this computer program initially was sponsored by the U.S. Air Force Flight Dynamics Laboratory. (See References 1, 2, 3, and 4.) It provides techniques for determination of steady state and dynamic (transient) ECS performance, and of control system stability; and for synthesis of optimal ECS control systems. The program is available from the U.S. Air Force, or as a proprietary commercial version. General uses of a transient analysis computer program for ECS design and development, and general features of EASY relative to these uses, are presented. This report summarizes the nine analysis options of EASY, EASY program organization for analyzing ECS, data input to the program and resulting data output, and a discussion of EASY limitations. Appendices provide general definitions for dynamic analysis, and samples of input and output for EASY
AC-9 Aircraft Environmental Systems 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 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 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 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
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 a corrosion and heat-resistant nickel-iron alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials 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 has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: Alclad 6061-T4 (Sheet)/6061-T451 (Plate) UNS Number: A86061
AMS D Nonferrous Alloys 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
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4029, ALUMINUM ALLOY SHEET AND PLATE (2014; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4029 shall be fulfilled whenever reference is made to this specification
AMS D Nonferrous Alloys 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
E-25 General Standards for Aerospace and Propulsion Systems
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4049, ALUMINUM ALLOY SHEET AND PLATE (Alclad 7075; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4049 shall be fulfilled whenever reference is made to this specification
AMS D Nonferrous Alloys Committee
This specification covers the engineering requirements for selective (brush) electrodeposition of nickel and the properties of the deposit. This process has been used typically to provide good wear resistance and dimensional build-up and restoration of parts which may operate in service up to 450 degrees F (232 degrees C), where low tensile stress in the deposit is required, but usage is not limited to such applications. Diffusion heat treatment of the deposit is not required
AMS B Finishes Processes and Fluids Committee
This specification covers the specific requirements for 7075 aluminum alloy alclad one side plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7075) core with a thin layer of an aluminum alloy (7072) anodic to the core bonded to one surface
AMS D Nonferrous Alloys Committee
This specification covers a free-machining carbon steel in the form of bars
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of foil
AMS D Nonferrous Alloys Committee
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