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This SAE Recommended Practice covers passive torque biasing axle and center differentials used in passenger car and light truck applications. Differentials are of the bevel gear, helical gear, and planetary types, although other configurations are possible.
Drivetrain Standards Committee
This SAE Recommended Practice covers the design and application of a 120 VAC single phase engine based auxiliary power unit or GENSET. This document is intended to provide design direction for the single phase nominal 120 VAC as it interfaces within the truck 12 VDC battery and electrical architecture providing power to truck sleeper cab hotel loads so that they may operate with the main propulsion engine turned off.
Truck and Bus Electrical Systems Committee
This material type has resistance to hot air, but generally has poor resistance to fuels and lubricants, but usage is not limited to such applications. Each application should be considered separately. This material type has a typical service temperature range of -85 to 500 °F (-65 to 260 °C). The operating temperature range of the material is a general temperature range, but the presence of particular fluids and design parameters may modify this range. Recommendations on the material selection are based on available technical data and are offered as suggestions only. Each user should make his own tests to determine the suitability for his own particular use.
A-6C2 Seals Committee
This specification provides dimensional standards for crimp type contact wire barrel design and is a replacement for MS3190. Some wire barrel designs may exist in AS39029 but are not considered approved for future use, therefore, will not appear in this specification. The crimp barrel sizes listed in this document have been standardized in AS39029 and AS22520 specifications, tools and contacts are available to support these listed sizes. These crimp barrel requirements shall be used for any contact, regardless of whether it is a standard or non-standard contact configuration. The specification lists details for three types of wire barrels: A, B, and C. Wire barrel type A is not recommended for new design. Table 4 lists each AS39029 detail sheet wire barrel type.
AE-8C1 Connectors Committee
This SAE Recommended Practice establishes a uniform, powered vehicle test procedure and minimum performance requirement for lane departure warning systems used in highway trucks and buses greater than 4546 kg (10000 pounds) gross vehicle weight (GVW). Systems similar in function but different in scope and complexity, including lane keeping/lane assist and merge assist, are not included in this document. This document does not apply to trailers, dollies, etc. This document does not intend to exclude any particular system or sensor technology. This document will test the functionality of the lane departure warning system (LDWS) (e.g., ability to detect lane presence and ability to detect an unintended lane departure), its ability to indicate LDWS engagement, its ability to indicate LDWS disengagement, and its ability to determine the point at which the LDWS notifies the human machine interface (HMI) or vehicle control system that a lane departure event is detected. Moreover, this
Truck and Bus Automation Safety Committee
This document contains information and guidance necessary for the development of a representative, repeatable validation program that may be utilized to assess the capability of SHM systems. The nature of SHM data differs from that seen in traditional nondestructive evaluation (NDE) applications in that the position of SHM sensors is fixed and SHM data can be available much more frequently (if not continuously) over time. This document presents methodologies that can be used to arrive at SHM capability while considering the unique nature of SHM deployment. Each SHM system must be considered independently to determine the applicability and limitations of the guidance contained here for each SHM system being assessed.
Aerospace Industry Steering Committee on Structural Health
This SAE Recommended Practice establishes recommended procedures for the issuance, assignment, and structure of Identification Numbers on a uniform basis by states or provinces for use in an Assigned Identification Number (AIN).
VIN - WMI Technical Committee
This drawing specifies parts AS20905, AS20906, AS20907, AS20908, AS20909, AS20910, AS20911, AS20912, AS20913, AS20914, AS20915, AS20916, AS20917, AS20918, AS20919, AS20920, AS20921, AS20922, AS20923, AS20924, AS20925, AS20926, AS20927, AS20928, AS20929, AS20930, AS20931, AS20932, AS20934, AS20936, AS20938, AS20940, AS20942, AS20944, AS20946, AS20948, AS20950, AS20952, AS20954, AS20956, AS20958, AS20960, and AS20962. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
This document is applicable to civil aerospace airframe structural applications where stakeholders are seeking guidance on the definition, development, and certification of structural health monitoring (SHM) technologies for aircraft health management applications. Inputs to the structural health management are obtained from SHM equipment and/or from onboard sensors, delivering the detection and characterization of damage, load, or environmental parameters for operational and damage monitoring. For the purpose of this document, SHM is defined as “the process of acquiring and analyzing data from on-board sensors to characterize the health of a structure.” The suite of on-board sensors could include any presently installed aircraft sensors, as well as new sensors to be defined in the future.
Aerospace Industry Steering Committee on Structural Health
This drawing specifies parts AS21506, AS21507, AS21508, AS21509, AS21510, AS21511, AS21512, AS21513, AS21514, AS21515, AS21516, AS21517, AS21518, AS21519, AS21520, AS21521, AS21522, AS21523, AS21524, AS21525, AS21526, AS21527, AS21528, AS21529, AS21530, AS21531, AS21532, AS21534, AS21536, AS21538, AS21540, AS21542, AS21544, AS21546, AS21548, AS21550, AS21552, AS21554, AS21556, AS21558, AS21560, AS21562, AS21564, AS21566, AS21568, AS21570, AS21572, AS21574, AS21576, AS21578, AS21580, AS21582, AS21584, AS21586, AS21588, AS21590, AS21592, AS21594, and AS21596. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
This drawing specifies parts AS21405, AS21406, AS21407, AS21408, AS21409, AS21410, AS21411, AS21412, AS21413, AS21414, AS21415, AS21416, AS21417, AS21418, AS21419, AS21420, AS21421, AS21422, AS21423, AS21424, AS21425, AS21426, AS21427, AS21428, AS21429, AS21430, AS21431, AS21432, AS21434, AS21436, AS21438, AS21440, AS21442, AS21444, AS21446, AS21448, AS21450, AS21452, AS21454, AS21456, AS21458, AS21460, and AS21462. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
This drawing specifies parts AS21607, AS21608, AS21609, AS21610, AS21611, AS21612, AS21613, AS21614, AS21615, AS21616, AS21617, AS21618, AS21619, AS21620, AS21621, AS21622, AS21623, AS21624, AS21625, AS21626, AS21627, AS21628, AS21629, AS21630, AS21631, AS21632, AS21634, AS21636, AS21638, AS21640, AS21642, AS21644, AS21646, AS21648, AS21650, AS21652, AS21654, AS21656, AS21658, AS21660, AS21662, AS21664, AS21666, AS21668, AS21670, AS21672, AS21674, AS21676, AS21678, AS21680, AS21682, AS21684, AS21686, AS21688, AS21690, AS21692, AS21694, and AS21696. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
This SAE Aerospace Information Report (AIR) is prepared for stakeholders seeking information about the evolution, integration, and approval of SHM technologies for military aircraft systems. The report provides this information in the form of (a) two military organizations’ perspectives on requirements, and (b) general SHM challenges and industry perspectives. The report only provides information to generate awarness of prespectives for military aircraft and, hence, assists those who are involved in developing SHM systems understanding the broad range of regulations, requirements, and standards published by military organizations that are available in the public domain from the military organizations.
Aerospace Industry Steering Committee on Structural Health
This SAE Aerospace Information Report (AIR) provides guidance on the definition, development, integration, qualification/certification, and deployment of Structural Health Monitoring (SHM) technologies applied to commercial and military rotorcraft. Increased implementation of SHM is believed to have numerous potential benefits, including enhanced operational safety and reduced maintenance burden. The focus is on augmenting ARP6461 to address specific unique aspects of implementing SHM on rotorcraft without unnecessarily duplicating guidance already contained in the ARP that is generally applicable to both fixed-wing and rotary-wing aircraft. For the purpose of this document, SHM is defined as “the process of acquiring and analyzing data from on-board sensors in order to determine the health of a structure”. Note that this is irrespective of whether the on-board sensors are a permanent or temporary installation. On-board sensors could include any presently installed aircraft sensors as
Aerospace Industry Steering Committee on Structural Health
This drawing specifies parts AS21905, AS21906, AS21907, AS21908, AS21909, AS21910, AS21911, AS21912, AS21913, AS21914, AS21915, AS21916, AS21917, AS21918, AS21919, AS21920, AS21921, AS21922, AS21923, AS21924, AS21925, AS21926, AS21927, AS21928, AS21929, AS21930, AS21931, AS21932, AS21934, AS21936, AS21938, AS21940, AS21942, AS21944, AS21946, AS21948, AS21950, AS21952, AS21954, AS21956, AS21958, AS21960, and AS21962. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
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