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This document recommends criteria for the layout and for the design, installation, and operation of flight deck facilities for transport aircraft.
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash-welded rings up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings.
AMS E Carbon and Low Alloy Steels Committee
AMS3970/6 Material Specification (MS) defines the requirements of carbon fiber plain weave fabric, 193 g/m2, reinforced epoxy structural prepreg for repair, curing under vacuum at 120 °C (250 °F), and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m2, used in repair of carbon fiber reinforced epoxy structures and qualified according to AMS3970/1 and AMS3970/2 for aerospace applications. The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests. If included, the requirements to be met by the adhesive are also defined in this document.
AMS CACRC Commercial Aircraft Composite Repair Committee
This SAE Standard covers equipment used to remove refrigerant from a Mobile Thermal Management System to be sent for reclamation rather than on-site recycling. The refrigerant could be contaminated and should not be mixed with recycled refrigerant. This could also be any refrigerant that the technician is not going to recycle and reuse. The refrigerant could also be a blend or a refrigerant for which Recovery/Recycling/Recharging equipment is not available.
ICTMS Service Committee
E-25 General Standards for Aerospace and Propulsion Systems
This SAE Recommended Practice describes a marking system to distinguish long-stroke from standard stroke for service, parking, and combination air-brake actuators and components. Said actuators are used for applying cam-type foundation brakes by slack adjuster means.
Truck and Bus Brake Actuator Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.008 to 4.000 inches (0.20 to 101.6 mm), inclusive, in thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion- and heat-resistant cobalt-chromium-molybdenum alloy in the form of bars 2.500 to 4.000 inches (63.50 to 101.60 mm) inclusive, diameter or least distance between parallel sides.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Recommended Practice establishes harmonized test methods for measuring volatile organic compound (VOC) emissions from polyurethane foam materials used in automotive interior applications. This recommended practice complements SAE J2989 by providing standardized emission collection methods, analytical procedures, and reporting formats to ensure consistent and comparable results across different testing laboratories and organizations. The methods discussed in this recommended practice include micro-scale chambers, small-scale chambers, bag methods, thermal extraction techniques, and bottle methods for aldehyde determination. This standard addresses the unique challenges presented by polyurethane foam materials, including their high surface area, absorption capacity, and sensitivity to environmental conditions. The selection of the appropriate test method shall be primarily determined by customer requirements or OEM specifications, as these requirements often dictate the specific test protocol needed for material approval or compliance. When customer requirements are not specified, the selected method should be based on available laboratory capabilities, sample size constraints, testing timeline requirements, and the intended use of the results. This recommended practice provides guidance on the appropriate conditions and limitations for each method to ensure consistent and comparable results across different testing approaches. The standardization of these testing methodologies is essential for reducing the variability currently observed across the automotive industry. By providing clear guidance on specimen preparation, test conditions, analytical procedures, and reporting formats, this standard aims to facilitate meaningful comparison of results, reduce testing costs, and improve product development and quality control efforts. This recommended practice applies to both molded polyurethane foam components such as seating cushions and backrests, and slab stock foam materials used in automotive interior applications. The guidance in this document is intended to reduce ambiguity, improve reproducibility, and provide comparable results across different testing facilities.
Volatile Organic Compounds
This SAE Recommended Practice is intended to establish a procedure to certify the low mu/winter driving skill levels of professional drivers. This certification can be used by the individual driver to qualify their skills when seeking employment or other professional activity. These certification levels may also be used by test facilities or other organizations when seeking test or professional drivers of various skills. This document provides directions for obtaining certification through Probitas Authentication®1 and the low mu/winter driving skill examination requirements. This document is a supplement to SAE J3300, providing information specific to the low mu/winter driving skill certification and clarifying the application of the rules set forth in SAE J3300 to the low mu/winter driving certification. While the references, definitions, rules, and guidelines presented in SAE J3300, Sections 1 through 5 apply to the low mu/winter driving certification, they are not repeated in this document.
Driving Skills Standards Committee
This test procedure provides a standard method for evaluating the side stand retraction performance of a side stand/motorcycle combination.
Motorcycle Technical Steering Committee
The processes addressed in this AIR apply to the acquisition and validation of dynamic total-pressure and distortion data from CFD models simulating turbulent flows in inlets. The results of these processes can be used in the formation of an inlet-flow-distortion methodology that addresses turbine-engine operability assessments.
S-16 Turbine Engine Inlet Flow Distortion Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This test method provides a guidance for determining the total free play between the ball and outer ring of a spherical bearing when measured in both the radial and axial directions. Bearings covered by this test method include all plain spherical-type bearings, both self-lubricated (lined) and metal-to-metal.
ACBG Plain Bearing Committee
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Standard (AS) establishes the requirements for externally swaged tube-fitting assemblies used in aircraft fluid systems in the following pressure classes: B (1500 psi or 10500 kPa), and D (3000 psi or 21000 kPa), and in temperature types I (-65 to 160 °F or -55 to 70 °C), and II (-65 to 275 °F or -55 to 135 °C) of AS2001. This specification covers a common Cres, titanium, and aluminum fittings that may be used for a range of operating pressures up to 3000 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5902. Table 11 shows applicable aerospace fitting part number standard and tubing materials and operating pressures.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This study compares the energy efficiency of a real battery pack and a simulated battery pack using a hardware-in-the-loop battery emulator, through experimental testing on a dedicated inertia dynamometer for light quadricycles. The investigated LiFePo4 battery pack has a nominal voltage of 48 V and a nominal capacity of 100 Ah. Initial characterization identified a reduced State of Health based on capacity (SOHC), with a measured usable capacity of 48 Ah (from the nominal 100 Ah) and a corresponding reduction in charge acceptance capability. The emulator was configured to replicate the degraded battery characteristics, including the open-circuit voltage (OCV)-SOC relationship, internal resistance, and current limitations, enabling a direct comparison between simulated and experimental dynamic behavior. The experimental setup was designed to overcome the limitations of conventional chassis dynamometers for low-mass, independent four-wheel-drive quadricycles operating without mechanical friction braking systems. Multiple driving cycles were reproduced using a PLC-based closed-loop control system, with data acquisition performed via CAN communication. The comparative analysis highlights significant differences during regenerative braking events. While the emulator accurately reproduces baseline electrical behavior under mild operating conditions, the aged battery exhibits strong limitations during both high-power acceleration and severe deceleration phases. In particular, increased internal resistance and transient electrochemical polarization lead to premature saturation of charge acceptance, resulting in rejection of high-frequency current transients. Consequently, the experimentally observed energy recovery is significantly lower than the theoretical values predicted by the emulator. In addition, due to the absence of mechanical braking, the reduced regenerative capability directly leads to speed tracking deviations, as the required braking torque cannot be fully achieved. These results identify battery degradation as a key physical constraint affecting both energy efficiency and dynamic braking performance, highlighting the importance of improved electro-thermal and aging-aware model calibration for realistic system-level simulations.
Sementa, PaoloVaglieco, Bianca MariaAltieri, Nunzio