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Viewing 31 to 60 of 43385
2016-09-19
WIP Standard
J584
This SAE Standard provides design parameter and general requirements for motorcycle headlamps.
2016-09-19
WIP Standard
AMS6308F
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
2016-09-19
WIP Standard
AMS6481D
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2016-09-19
WIP Standard
AMS6529D
This specification covers a special aircraft-quality, low-alloy steel in the form of bars.
2016-09-19
WIP Standard
AMS6528D
This specification covers a special aircraft-quality, low-alloy steel in the form of bars.
2016-09-18
WIP Standard
AS20218B
Scope unavailable.
2016-09-18
WIP Standard
AS6038B
This specification covers antifriction bellcrank ball bearings intended primarily for airframe use.
2016-09-16
WIP Standard
J2806
Subject document is specifically intended for service brakes and service brakes when used for parking and/or emergency brakes (only) that are commonly used for automotive-type, ground wheeled vehicles exceeding 4536 kg (10 000 US lb) Gross Vehicle Weight Rating (GVWR). Subject specification provides the off-vehicle procedures, methods, and processes used to objectively determine suitability of tactical and combat ground wheeled vehicle brake systems and selected secondary-item brake components (a.k.a. aftermarket or spare parts), including brake “block” for commercial applications only, specifically identified within subject document. Subject specification is primarily based on known industry and military test standards utilizing brake inertia dynamometers. Targeted vehicles and components include, but may not be limited to the following: a.
2016-09-16
Standard
AIR6114
This document was prepared by the SAE AS-1B1 IMM Task Group to explain and document background information and design decisions made during the development of AS5726. This handbook is published separately to preserve information that is not required or provided in the AS5726 but may be important to system designers to ensure interoperability between the Micro Munition Host and Micro Munition. As a handbook, it cannot be invoked as a requirement in a contract. The structure and numbering of this document mirrors that of AS5726 for the convenience of readers. Headings such as “Requirements” in this handbook should not be interpreted as invoking requirements.
2016-09-16
Standard
J1752/2_201609
This SAE Recommended Practice defines a method for evaluating the near field electric or magnetic component of the electromagnetic field at the surface of an integrated circuit (IC). This technique is capable of providing a detailed pattern of the RF sources internal to the IC. The resolution of the pattern is determined by the characteristics of the probes used and the precision of the mechanical probe positioner. The method is usable over the 10 MHz to 3 GHz frequency range with existing probe technology. The probe is mechanically scanned according to a programmed pattern in a plane parallel or perpendicular to the IC surface and the data is computer processed to provide a color-enhanced representation of field strength at the scan frequency. This procedure is applicable to measurements from an IC mounted on any circuit board that is accessible to the scan probe. For comparisons, the standardized test board shall be used.
2016-09-16
Standard
AS1241D
This document establishes the requirements for physical and chemical properties and the minimum tests to evaluate suitability of phosphate ester hydraulic fluids for use in aircraft systems where fire resistance is required. Additional tests may be specified by the qualifying agency to demonstrate compliance with their specific requirements. The "qualifying agency" will be defined herein to be the airframe manufacturer submitting certification approval for use of the fluid in a specific model airplane. Fluids meeting the requirements of this specification may be approved by a qualifying agency for use on specific airplane models. Data used to show compliance to this specification can be used by the qualifying agency to show compliance to the applicable regulations for the appropriate certifying authority; e.g., FAA, EASA, etc.
2016-09-16
WIP Standard
ARP5483B
This SAE Aerospace Recommended Practice establishes methods for testing airframe Rolling Element bearings. The purpose of ARP5483 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in standards, purchase orders, etc. when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests for the application.
2016-09-16
Standard
J1981_201609
The test is designed to evaluate the frontal impact resistance of wheel and tire assemblies used with passenger cars, light trucks and multi-purpose vehicles. The test is specifically related to vehicle pothole tests that are undertaken by most vehicle manufacturers. The scope has been expanded to allow the use of a striker that can be angled to preferentially impact the inboard and outboard wheel flange. For side impact of the outboard rim flange only, please refer to SAE J175. This SAE Recommended Practice provides a procedure to test a wheel or a tire and the test failure critiera. The specific test for a vehicle requires input from a pothole test on that vehicle to establish the drop height of the striker used in this test.
2016-09-16
Standard
J1654_201609
This SAE Standard covers unshielded cable intended for use at a nominal system voltage up to 600 V or 1000 V (AC rms or DC). It is intended for use in surface vehicle electrical systems.
2016-09-15
WIP Standard
AS6858
This document defines the technical requirements for the safe integration of Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) in large aircraft aircraft. Most of the technical concepts and approaches covered by this document represent current industry "best practice". Others require specific approval from the procuring activity before use. This requirement for approval is not intended to prohibit their use; but rather to ensure that the prime contractor has fully investigated their capability to perform reliably and to be sufficiently durable under the required conditions and that the prime contractor can present substantiating evidence for approval before the design is committed to.
2016-09-15
WIP Standard
AS5756/7A
SCOPE IS UNAVAILABLE.
2016-09-15
WIP Standard
AIR5575A
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.

Although prominent members of the aerospace community are taking aggressive measures to phase out the hot stamping of interconnecting wire, the process lingers on, particularly within the operations of smaller manufacturers, modification shops, and operator maintenance facilities. In recent years, non-impact marking processes have been developed that can mark virtually all of the common wire types used in aerospace interconnect applications. The purpose of this document is to encourage full conversion to non-impact marking processes in order to reduce the probability of causing damage to the wire insulation.

2016-09-15
WIP Standard
ARP5369B
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables. This document is not intended to encourage the use of hot stamp marking or to endorse the related process. This method of marking wire identification may be prohibited on any aerospace vehicle wiring that is required to conform to the provisions of MIL-W-5088L or AS 50881. Methods which do not deform wire or cable insulation, such as Ink Jet, Dot Matrix or UV Laser marking are encouraged as a means of minimizing the possibility of insulation damage, particularly on insulation constructions of less than 0.010 in wall thickness. In recognition that the present use of hot stamp wire marking is widespread and may continue for an extended period, the guidelines provided in this document are intended to provide process control information necessary to minimize the possibility of insulation damage.
2016-09-15
Standard
AMS2232H
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range. Tolerances for product sizes not listed herein shall be as agreed upon by purchaser and vendor.
2016-09-15
Standard
CPGM1_17LT4CAMA
This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.
2016-09-15
Standard
CPGM2_17LT4CAMA
This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.
2016-09-14
Standard
AMS3894/1C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/18A
This specification covers one type of toughened, high-impact epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/3C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/2C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/7C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/5C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
2016-09-14
Standard
AMS3894/9C
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
Viewing 31 to 60 of 43385