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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 establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications
AMS AM Additive Manufacturing Metals
This technical report covers performance requirements, design requirements, and design guidelines for replaceable bulbs which may be used in headlamp applications
Road Illumination Devices Standards Committee
A technical committee shall be responsible for a field of endeavor, as defined by its scope. In cases where projects overlap areas of interest of another council’s committee, the originating committee shall submit the project(s) for review and approval to the other concerned committee and its council prior to issuance. A committee is established when a new major project area is to be undertaken and no existing committee is available. A committee is discharged when the assigned work is completed and there is no further need for its services. The councils retain responsibility for periodic review of technical reports developed by their disbanded committees
Executive Standards Committee
This SAE Standard covers the complete dimensional and general specifications, including physical properties and methods of testing, for those types of lock washers intended for use in automotive and general industrial applications
Fasteners Committee
This SAE Standard describes a method for measuring the weighted sound pressure levels at prescribed microphone positions in the proximity of a device or machine for outdoor use, in order to determine compliance with noise limits. The A-weighted sound power level of the source is calculated from the measured values
SLTC - Earth Moving Machinery Sound Level
This SAE Standard describes a method for determining the noise emitted by earthmoving machinery at the operator's position in terms of the equivalent continuous A-weighted sound pressure level while the machine is in a stationary test condition. This SAE Standard is a special test code for specific types of earthmoving machinery. It is an extension of ISO 6081 which contains the general requirements for many types of machinery and equipment. Specific requirements are provided in this special test code to enable the sound pressure level at the operator's position, with the machine in a stationary test condition, to be determined in a manner which is repeatable. Attachments (bucket, dozer, etc.) for the manufacturer's production version shall be fitted since this is the configuration most likely to exist when the machine is in actual use. This document will enable compliance with noise limits to be determined. It can also be used for evaluation purposes in noice reduction investigations
SLTC - Earth Moving Machinery Sound Level
This specification covers a potassium-acetate base deicing/anti-icing fluid in the form of a concentrated liquid
G-12RDP Runway Deicing Product 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
SAE J3072 establishes requirements for a grid support inverter system function that is integrated into a plug-in electric vehicle (PEV), which connects in parallel with an electric power system (EPS) by way of conductively coupled, electric vehicle supply equipment (EVSE). This standard also defines the communication between the PEV and the EVSE required for the PEV onboard inverter function to be configured and authorized by the EVSE for discharging at a site. The requirements herein are intended to be used in conjunction with IEEE 1547-2018 and IEEE 1547.1-2020 or later versions
Hybrid - EV 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 corrosion and heat resistant steel in the form of welded tubing
AMS F Corrosion and Heat Resistant Alloys 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 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
Included herein are complete general and dimensional data for the types of slotted and recessed head machine, tapping, and wood screws, and slotted capscrews recognized as SAE Standard. Also included are performance data for tapping screws and appendixes which provide instructions for protrusion gaging flat heads, penetration gaging of recessed heads, across corners gaging of hexagon heads, recommended hole sizes for tapping screws, and a cross reference of tapping screw type designations. The inclusion of dimensional data in this standard is not intended to imply that all of the products described are stock production sizes. Consumer interests are requested to consult with manufacturers concerning lists of stock production sizes
Fasteners Committee
This specification covers tungsten in the form of forgings produced from billets processed by isostatically cold pressing, utilizing hydrogen reduced tungsten powder, and high-temperature sintering
AMS G Titanium and Refractory Metals Committee
This method is recommended for establishing breakage allowances for parts fabricated from cut lengths or blanks, or from coils processed directly into a progressive-die pressline, and is equitable to both the sheet producer and the fabricator
Sheet and Strip Steel Committee
This specification covers tungsten carbide-cobalt in the form of powder
AMS B Finishes Processes and Fluids Committee
This specification covers two types of semi-processed silicon steel in the form of sheet and strip supplied in coils or cut lengths
AMS E Carbon and Low Alloy Steels Committee
This SAE Standard pertains to off-road, self-propelled work machines as defined in categories one through five of SAE J1116. It is intended to provide engineers and designers with information in order that access openings provided in equipment and machinery for purposes of inspection, adjustment, and maintenance are made large enough for the intended function by the person in the field or shop
Machine Technical Steering Committee
It applies to reports of Surface Vehicles and Machinery Technical Committees only. Aerospace technical reports are covered by editorial practices of the Aerospace Council. Close adherence to this recommended practice by technical committees of SAE will help to assure uniform technical reports. Should questions on format, style, or other matters pertaining to the organization and editorial practices of technical reports be raised within technical committees of the Technical Board, they should be referred to the Chairman of the Publications Advisory Committee for interpretation or for discussion by the full Publications Advisory Committee
Executive Standards Committee
This SAE Recommended Practice establishes a dynamic test procedure for evaluating Type 1 lap belt assemblies for pelvic restraints and Type 2 assemblies for combination pelvic and upper torso restraints, as defined in SAE J4c. Uniform test requirements, test procedures, a seat belt assembly loading device, and data recording requirements are specified. The intent of the recommended practice is to provide an acceptance procedure employing a dynamic test method for determining the ability of seat belt assemblies to meet minimal requirements for restraining a seat belt assembly loading device. A simple dynamic test is described which will yield repeatable and comparable results while simulating the loading condition a seat belt assembly is subjected to in a frontal accident. The impact conditions generate belt loads representative of those obtained in a motor vehicle striking a rigid barrier head on at 30 mph as stated in SAE J850
Motor Vehicle Council
The purpose of this SAE Recommended Practice is to provide a laboratory drop test procedure whereby specimens of laminated safety glazing intended for use in automotive windshields can be evaluated on the basis of resistance to penetration
Glazing Materials Standards Committee
This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier use
Truck Bus Control and Communications Network 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
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus
AS-1A Avionic Networks Committee
Traditional methods of photometry rely on the use of a goniometer to rotate the test item around two axes at right angles. This method is satisfactory for most situations but has certain disadvantages: a Point-by-point measurements with a goniometer may be slow. With more advanced requirements, particularly for headlamps, where the entire beam pattern is of concern, isocandela measurements are becoming increasingly needed. Such testing can be very time consuming. b For production quality assurance, the speed of a goniometer may not allow testing to keep pace with the production line if a large quantity of lamps must be sampled. c High Intensity Discharge (HID) lamps are becoming commonly used. Such lamps are orientation sensitive, changing in both lumen output and intensity distribution when tilted. This can introduce significant inaccuracies in test results when testing is performed using a goniometer. There is a need for alternative test techniques which can achieve very high speed
Test Methods and Equipment Stds Committee
The scope of this SAE Recommended Practice includes practical applications, theory, process management, audit and control recommendations, limitations, additional considerations, and process documentation
EG-1A Balancing Committee
This specification and its supplementary detail specifications cover carbon fibers in the form of tape and sheet impregnated with heat-activated, formable, thermoplastic polysulfone resin
AMS P17 Polymer Matrix Composites Committee
This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to AS64350-362. To view suppliers qualified against this standard, visit
Engine and Airframe Technical Standards Committee (TSC)
This SAE Standard applies to Construction, General Purpose Industrial, Agricultural, Forestry, and Specialized Mining categories of off-road, self-propelled work machines, as defined in SAE J1116. Powered industrial trucks and agricultural equipment, other than the basic agricultural tractor, are excluded from the scope of this document. The document defines positions for convenient placement of hand- and foot-operated controls derived from the overlapping reach capability of large and small operators. The large operator approximates the 95th percentile male, and small operator approximates the 5th percentile female of the U.S. population. This document defines zones in which controls used by a seated operator would ordinarily be placed, and is intended as a guide for the design of the operator compartment controls. Constraints peculiar to individual machine or user applications may require modification to these defined zones. The established zones are based upon singular reach
HFTC1, Controls, Visibility, Anthropometrics, Accessibility
This drawing specifies parts AS55018, AS55019, AS55020, AS55021, AS55022, AS55023, AS55024, AS55025, AS55026, AS55027, AS55028, AS55029, AS55030, AS55031, AS55032, AS55034, AS55036, AS55038, AS55040, AS55042, AS55044, AS55046, AS55048, AS55050, AS55052, AS55054, AS55056, AS55058, AS55060, AS55062, AS55064, AS55066, AS55068, AS55070, AS55072, AS55074, AS55076, AS55078, AS55080, AS55082, AS55084, AS55086, AS55088, AS55090, AS55092, AS55094, and AS55096. To view suppliers qualified to manufacture this part, visit
Engine and Airframe Technical Standards Committee (TSC)
This SAE Standard describes a method for determining the noise emitted by earthmoving machinery at the operator’s position in terms of the equivalent continuous A-weighted sound pressure level while the machine is carrying out a simulated work cycle
SLTC - Earth Moving Machinery Sound Level
This SAE Standard describes a method for determining the noise emitted to the environment by earthmoving machinery in terms of the A-weighted sound power level while the machine is working under dynamic test conditions
SLTC - Earth Moving Machinery Sound Level
This specification covers a urea compound in the form of a solid
G-12 Aircraft Ground Deicing Steering Group
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