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This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers a high temperature, compression set and fluid resistant fluorocarbon (FKM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes for aeronautical and aerospace applications.
AMS CE Elastomers Committee
The specifications contained in this SAE Standard pertain to high-tension ignition cable used in road vehicle engine ignition systems.
Ignition Standards Committee
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers an aluminum alloy in the form of plate.
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat resistant steel in the form of sand or centrifugal castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
AMS E Carbon and Low Alloy Steels Committee
This SAE Standard specifies the guidance and the requirements for the electrodeposition of zinc-nickel alloy coatings on a range of metallic substrates for the provision of corrosion resistance to steel components and galvanic compatibility between some bi-metallic contacting surfaces.
AMS B Finishes Processes and Fluids Committee
This specification and its supplementary slash specifications establish the requirements for electrodeposition of metals by brush plating.
AMS B Finishes Processes and Fluids Committee
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size.
AMS G Titanium and Refractory Metals Committee
This specification covers a synthetic rubber in the form of a soft wall, smooth bore, collapsing-type hose.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
The electrical cranking system components, which include the battery, cables, and cranking motor, must be carefully selected to provide the necessary speed to start an engine under the most severe climatic conditions for which the system is intended. Engine cranking loads increase with cold temperatures, therefore, the initial selection of these components needs to consider low-temperature engine torque requirements. To insure an adequate electrical cranking system is obtained, it is important that proper test procedures are used for obtaining the cranking load requirements of the engine.
Electrical Systems
This report is intended to provide the information to estimate the accessory load of a typical heavy truck or bus. The components covered include: air compressors, alternators, refrigerant compressors, engine cooling fans and power steering pumps. The values show an estimate of the average power requirements and duty cycles for these accessories. This report does not address loads required for engine operation. Required systems include those needed for engine performance such as fuel pumps and electronic control modules (ECM).
Truck and Bus Powertrain Committee
This specification covers a stable, nonvolatile, petroleum-base compound in a form suitable for application by dipping at 170 to 210 °F (77 to 99 °C).
AMS B Finishes Processes and Fluids Committee
E-30 Propulsion Ignition Systems Committee
This SAE Recommended Practice is intended to apply to lamps, batteries, heaters, radios, and similar equipment for operation with mobile or automotive diesel engines. Twenty-four V systems have long been used for heavy-duty services because 24 V permit operating 12 V systems in series-parallel. Thirty-two V systems have been used for marine, railroad-car lighting, and other uses. Generators, storage batteries, starting motors, lighting, and auxiliary electrical equipment shall be for nominal system ratings of 12, 24, or 32 V as determined by the power requirements of the application. It is recommended that no intermediate voltages be considered. The combination of a 24 V starting motor and two 12 V batteries connected in series for cranking is considered practical where it can be adapted to the installation. The batteries are reconnected in parallel for charging from a 12 V generator/alternator and for operating lights and other auxiliary equipment, or charged separately and used
Electrical Systems
Circuit Protection and Switch Device Committee
This SAE Aerospace Information Report (AIR) outlines a recommended procedure for evaluation of the vibration environment to which the gas turbine engine powerplant is subjected in the helicopter installation. This analysis of engine vibration is normally demonstrated on a one-time basis upon initial certification, or after a major modification, of an engine/helicopter configuration. This AIR deals with linear vibration as measured on the basic case structure of the engine and not, for example, torsional vibration in drive shafting or vibration of a component within the engine such as a compressor or turbine airfoil. In summary, this AIR discusses the engine manufacturer’s "Installation Test Code" aspects of engine vibration and proposes an appropriate measurement method.
S-12 Powered Lift Propulsion Committee
This specification covers a solvent-dispersed, corrosion-inhibiting compound packaged in aerosol cans.
AMS B Finishes Processes and Fluids Committee
This SAE Recommended Practice applies to mobile, construction type, crane and cable excavator hand and foot controls. It should not be construed to limit the use of, or to apply to combination controls, automatic controls, or any other special operating control requirements.
Cranes and Lifting Devices Committee
AE-1 Engine Accessory Installations Committee
The purpose of this SAE Standard is to provide a standardized test procedure for generating engine performance maps. An engine performance map is a listing of engine fuel flow rates versus torque or power obtained at specific engine speeds and loads. Engine performance maps as specified by this code can be used in fuel economy simulation programs. This document is applicable to both four-stroke spark ignition (SI) and compression ignition (CI) engines, naturally aspirated and pressure charged, with or without charge air cooling.
Engine Power Test Code Committee
E-30 Propulsion Ignition Systems Committee
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
A-4 Aircraft Instruments Committee
This specification establishes the performance, qualification, acceptance limits, and identification for aeronautical engine high tension spark igniters.
E-30 Propulsion Ignition Systems Committee
SAE data file format for exchanging controlled periodic overload data. The object of this SAE Standard is to provide a simple, common methodology for exchanging the data from periodic overload fatigue tests. These tests consist of a single large fatigue cycle followed by a larger number of smaller cycles. The overloads are fully reversed fatigue cycles while the smaller cycles share a common mean and amplitude.
Materials, Processes and Parts Council
This Information Report describes eddy current testing, flux leakage testing, ultrasonic testing, and magnetic particle testing of steel tubing. The purpose of these testing methods is to expose flaws in the tube material or weld zone, such as discontinuities, seams, cracks, holes, voids, and other imperfections characteristic to the specific construction of the tubing. When agreed upon between the producer and purchaser, nondestructive testing is used in lieu of destructive hydrostatic pressure proof testing. Aircraft and Aerospace applications were not considered during the preparation of this document.
Metallic Tubing Committee
This specification covers a heat-treatable, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and stock for forging or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, flash-welded rings, and extrusions up to 12 inches (305 mm) in nominal diameter or least distance between parallel sides (thickness) in the solution heat-treated condition (see 8.4) and stock of any size for forging, flash-welded rings, or extrusions.
AMS F Corrosion and Heat Resistant Alloys 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 standard defines five CM functions and their underlying principles. The functions are detailed in Section 5. The principles, highlighted in text boxes, are designed to individually identify the essence of the related CM function and can be used to collectively create a checklist of “best practice” criteria to evaluate a CM program. The CM principles defined in this standard apply equally to internally focused enterprise information, processes, and supporting systems (i.e., Enterprise CM - policy driven, supporting the internal goals needed to achieve an efficient, effective and lean enterprise), as well as to the working relationships supported by the enterprise (i.e., Acquirer/Supplier CM - contracted relationship to support external trusted interaction with suppliers). In an Enterprise CM context there are several methodologies for principle use by the enterprise: The principles of this standard provide direction for developing enterprise or functional CM plans focused on
G-33 Configuration Management
This specification covers a titanium alloy in the form of forgings 1.00 inch (25.4 mm) and under in nominal cross-sectional thickness and of forging stock of any size.
AMS G Titanium and Refractory Metals Committee
This specification establishes the requirements for anodic coatings on aluminum alloys.
AMS B Finishes Processes and Fluids Committee
This specification covers a high-expansion steel in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification and its supplementary detail specification cover various types of non-woven glass cloth in the form of tape and flat sheet impregnated with epoxy resin, the resin to be supplied in a “B” staged condition.
AMS P17 Polymer Matrix Composites Committee
This specification covers a low-carbon steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a low-alloy steel in the form of sheet, strip, and plate 4.00 inches (101.6 mm) and under in thickness.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the requirements for an aluminum brazing flux in granular form.
AMS B Finishes Processes and Fluids Committee
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