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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
The purpose of this SAE Aerospace Information Report (AIR) is to provide guidance for aircraft engine and propeller systems (hereafter referred to as propulsion systems) certification for cybersecurity. Compliance for cybersecurity requires that the engine control, propeller control, monitoring system, and all auxiliary equipment systems and networks associated with the propulsion system (such as nacelle systems, overspeed governors, and thrust reversers) be protected from intentional unauthorized electronic interactions (IUEI) that may result in an adverse effect on the safety of the propulsion system or the airplane. This involves identification of security risks, their mitigation, verification of protections, and their maintenance in service. This document is intended to serve as suitable guidance for propulsion system manufacturers and applicants for propulsion system type certification. It is also intended to provide guidance for subsequent propulsion system integration into
E-36 Electronic Engine Controls Committee
OBJECT: Primarily to make porous magnesium alloy castings pressure tight
AMS D Nonferrous Alloys Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one type of nylon loop tape
AMS P Polymeric Materials Committee
This specification covers one width and strength of nylon tape
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers an aluminum alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet
AMS D Nonferrous Alloys Committee
This specification covers a two-component system composed of a non-polyester urethane resin and a hardener, supplied in kit form
AMS P Polymeric Materials Committee
This specification and its supplementary detail specifications cover an aromatic polyamide in the form of cord
AMS P Polymeric Materials Committee
This specification covers one type of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification covers one type of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification and its supplementary detail specifications cover two types of metallized nylon cloth
AMS P Polymeric Materials Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings
AMS E Carbon and Low Alloy Steels Committee
This specification covers established manufacturing tolerances applicable to aluminum alloy standard structural shapes ordered to inch/pound dimensions. Standard structural shapes are shapes in certain standard alloys, tempers, sizes, and sections such as angles, channels, Tees, Zees, I-Beams, and H-Beams commonly used for structural purposes. 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 two types of fire extinguishing foam concentrate in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a compound based on orthodichlorobenzene in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers vacuum-arc-cast molybdenum in the form of wrought round bars
AMS G Titanium and Refractory Metals Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of October, 1991
AMS B Finishes Processes and Fluids Committee
This specification covers one strength and weight of braided para-aramid cord
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers one weight and one type of finish of nylon cloth
AMS P Polymeric Materials Committee
This specification covers an aluminum-base alloy in the form of hand forgings and forging stock
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet
AMS D Nonferrous Alloys Committee
This specification covers a urea compound in the form of a solid
G-12 Aircraft Ground Deicing Steering Group
This specification covers a prepolymer in the form of a low molecular weight aromatic diglycidyl ester resin
AMS P Polymeric Materials Committee
AMS G Titanium and Refractory Metals 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 melt-processible, copolymer resin of ethylene and tetrafluoroethylene (ETFE) in the form of molded sheet
AMS P Polymeric Materials Committee
This document provides general and specific design guidance for the development of software data loading equipment for all types of aircraft. The primary purpose of data load is to upload loadable software parts to airborne computers. A secondary function of data load is downloading data from airborne computers. Software data load functionality generally falls into the following categories: Portable Data Loader (PDL) for loading equipment on the ground or carried onto aircraft to perform onboard loading. Airborne Data Loader (ADL) for installation on aircraft to perform onboard loading. Data Load Function (DLF) is software that performs the data loading. This document defines data loaders designed to load avionics equipment over a high-speed interface using an Ethernet network protocol. This document defines media interfaces and protocol requirements specific to all data load functions, whether portable or airborne. This document also describes the desired capabilities of data loading
Airlines Electronic Engineering CommitteeAvionics Maintenance CommitteeFlight Simulator Engineering and Maintenance Committee
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