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This specification covers one type of copper alloy (brass) in the form of bars and rods up to 4.000 inches (101.60 mm) in nominal diameter, thickness between parallel sides, or width as defined in Tables 3 through 6 (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of rolled or cold finished bars and rods of the sizes specified in 3.3.1.1 (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a polysulfide sealing compound with low adhesive strength, supplied as a two-component system that cures at room temperature
AMS G9 Aerospace Sealing Committee
This recommended practice establishes the requirements and procedures for Barkhausen Noise (BN) inspection of ferromagnetic steel components. See Appendix B for a list of common materials for BN inspection. Applications of the method are listed in 1.2 through 1.5
AMS K Non Destructive Methods and Processes Committee
This SAE Recommended Practice provides test methods and criteria for evaluating the internal cleanliness and air leakage for engine charge air coolers. This SAE Recommended Practice also provides nomenclature and terminology in common use for engine charge air coolers, related charge air cooling system components, and charge air cooling system operational performance parameters
Cooling Systems Standards Committee
This specification covers procedures for identifying wrought products of titanium and titanium alloys
AMS G Titanium and Refractory Metals Committee
This practice presents methods for establishing the driver workspace. Methods are presented for: Establishing accelerator reference points, including the equation for calculating the shoe plane angle. Locating the SgRP as a function of seat height (H30). Establishing seat track dimensions using the seating accommodation model. Establishing a steering wheel position. Application of this document is limited to Class-A Vehicles (Passenger Cars, Multipurpose Passenger Vehicles, and Light Trucks) as defined in SAE J1100
Human Accom and Design Devices Stds Comm
This SAE Standard provides test procedures, requirements, and guidelines for stop lamps intended for use on vehicles of less than, equal to, or greater than 2032 mm in overall width
Signaling and Marking Devices Stds Comm
The purpose of this document is to provide detailed requirements to preclude the acquisition and use of suspect counterfeit or counterfeit bearings and/or bearing components/materiel. The term bearings referenced throughout this document includes bearings and/or bearing components/materiel (e.g., balls, races, lubricant, cage, seal). The requirements of this document supplement the requirements of a higher-level quality standard (e.g., AS/EN/JISQ9100, ISO 9001, ANSI/ASQ E4, ASME NQA-1, AS9120, AS9003, and IATF 16949 or equivalent) and other quality management system documents. All appendices are provided for guidance and are not mandatory
G-21 Counterfeit Materiel Committee
Test procedures are described for measuring noise at specific receiver locations (passenger and cargo doors, and servicing positions) and for conducting general noise surveys around aircraft. Procedures are also described for measuring noise level at source locations to facilitate the understanding and interpretation of the data. Requirements are identified with respect to instrumentation; acoustic and atmospheric environment; data acquisition, reduction and presentation, and such other information as is needed for reporting the results. This document makes no provision for predicting APU or component noise from basic engine characteristics or design parameters, nor for measuring noise of more than one aircraft operating at the same time. No attempt is made to suggest acceptable levels of noise or suitable subjective criteria for judging acceptability. ICAO Annex 16 Volume I Attachment C provides guidance on recommended maximum noise levels
A-21 Aircraft Noise Measurement Aviation Emission Modeling
This SAE Aerospace Information Report (AIR) is intended to be used as a process verification guide for evaluating implementation of key factors in repair of metal bond parts or assemblies in a repair shop environment. This guide is to be used in conjunction with a regulatory approved and substantiated repair and is intended to promote consistency and reliability
AMS CACRC Commercial Aircraft Composite Repair Committee
This SAE Recommended Practice specifies graphic symbols for operator controls, gauges, tell-tales, indicators, instructions, and warning against risks in small craft and for engines and other equipment intended to be used in small craft
Marine Technical Steering Committee
This specification covers an acrylonitrile-butadiene (NBR) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS-P-83461 specification or the MIL-PRF-25732 specification
AMS CE Elastomers Committee
This document derives from the Federal Motor Vehicle Safety Standards (FMVSS) 105 and 135 vehicle test protocols as single-ended inertia-dynamometer test procedures. The test sequences enable brake output measurement, friction material effectiveness, and corner performance in a controlled and repeatable environment. This SAE Document also includes optional sections for parking brake output performance for rear brakes with hydraulic or Electric Park Brakes (EPB). It applies to brake corners from vehicles covered by the FMVSS 105 and 135 when using the appropriate brake hardware and test parameters. The FMVSS 135 applies to all passenger cars and light trucks up to 3500 kg of gross vehicle weight (GVWR). The FMVSS 105 applies to all passenger cars, multi-purpose vehicles, buses, and trucks above 3500 kg of GVWR. This document does not include testing for school bus applications or vehicles equipped with hydraulic brakes with a GVWR above 4540 kg. This document does not evaluate or
Brake Dynamometer Standards Committee
This SAE Aerospace Standard (AS) establishes standard requirements for aerospace sealants and adhesion promoters, which may be incorporated as part of SAE Aerospace Material Specifications (AMS) for such products. This document provides for commonality of methods and procedures for responsibility for inspection, source inspection, classification of tests, establishment of/and qualification to qualified products lists, approval, reports, resampling and retesting, packaging, and marking
AMS G9 Aerospace Sealing Committee
This SAE Recommended Practice establishes an inertia dynamometer test procedure, using an exemplar caliper disc brake, to characterize the effectiveness of disc brake friction materials for passenger cars and light-duty trucks, up to and including 2700 kg (5954 lb) GVW. SAE J1652 provides a method of characterizing friction material effectiveness on a full disc brake, using test conditions that approximate those for U.S. mandated new vehicle brake tests
Brake Dynamometer Standards Committee
This specification covers procedures for identifying carbon and low-alloy steels, corrosion- and heat-resistant steels and alloys, maraging and other highly alloyed steels, and iron alloy sheet, strip, and plate, and aircraft tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This Recommended Practice provides a common method to measure wear of friction materials (brake pad assemblies and brake shoes) and their mating parts (brake disc or brake drum). These wear measurements apply to brakes fitted on passenger cars and light trucks up to 4536 kg of Gross Vehicle Weight Rating under the Federal Motor Vehicle Safety Standard (FMVSS), or vehicles category M1 (passenger cars up to nine occupants, including the driver) under the European Community’s ECE Regulations
Brake Dynamometer Standards Committee
This specification covers unalloyed copper in the form of sheet, strip, and plate at least 0.015 inch (0.38 mm) in nominal thickness
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 square inches (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 0.005 to 1.000 inches (0.13 to 25.40 mm) in nominal thickness in the solution heat-treated condition
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys
AMS B Finishes Processes and Fluids Committee
This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Recommended Practice establishes a uniform laboratory procedure for evaluating performance and wear of automotive brakes and brake drums by an inertial dynamometer simulation of vehicle test and operating conditions. The code is applicable to hydraulic, air, or electrically actuated brakes. For electric brakes, 'ampere' values are substituted for 'line pressure' where specified in the procedure or on data and curve sheets. The procedure includes the following tests: 1. Torque output and deceleration (various speeds and brake input). 2. Evaluation of lining life (wear tests). 3. Brake characteristics (fade and recovery tests, noise, chatter, grabbiness). 4. Drum evaluation (wear, heat checking, scoring
Brake Dynamometer Standards Committee
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and flash welded rings up through 4.000 in2 (25.81 cm2) cross-section and stock for flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers fuel-resistant polysulfide (T) sealing compounds supplied as a two-component system
AMS G9 Aerospace Sealing Committee
This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inches (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.017 to 2.000 inches (0.43 to 50.80 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars and rods 1.00 inch (25.4 mm) and under in nominal diameter
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars and forgings 14.000 inches (355.60 mm) and under in nominal diameter or least distance between parallel sides and stock for forging (see 8.6
AMS G Titanium and Refractory Metals 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 nominal diameter or least distance between parallel sides and of stock of any size for forging and flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars, wire, and forgings up through 4.000 inches (101.60 mm), inclusive, in diameter or least distance between parallel sides and forging stock of any size (see 8.8
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of extruded bars and shapes, flash welded rings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides, and stock for flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium alloy in the form of bars, rods, or wire
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium (niobium) alloy in the form of foil, sheet, strip, or plate
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of extruded bars, shapes, and flash-welded rings up through 3.000 inches (76.20 mm), inclusive, in nominal diameter or least distance between parallel sides, and stock for flash-welded rings of any size (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers one grade of commercially pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive
AMS G Titanium and Refractory Metals Committee
This specification provides a standard set of procedures for sampling and testing to meet the requirements of material specifications for wrought titanium and titanium alloy products, except forgings and forging stock. It is applicable to the extent specified in a material specification
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of seamless tubing
AMS G Titanium and Refractory Metals Committee
This specification covers titanium in the form of laminated sheet
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of round, hexagon and square bars and forgings up through 3.000 inches (76.20 mm), inclusive, rectangular bar and forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and forging stock of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
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