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This specification covers a magnesium alloy in the form of sand castings.
AMS D Nonferrous Alloys Committee
This specification covers bonded honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered.
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
This document recommends standard gland dimensions for static radial O-ring seal applications specifically for engine and engine control systems and provides recommendations for modifying these glands in special applications.
A-6C2 Seals Committee
This specification covers a nickel-aluminum bronze alloy in the form of sand, centrifugal or continuous castings.
AMS D Nonferrous Alloys Committee
This SAE Aerospace Recommended Practice (ARP) establishes general criteria for the installation (e.g., type, location, accessibility, stowage) and crew member training needed for hand-held fire extinguishers.
S-9A Safety Equipment and Survival Systems Committee
This specification covers a leaded bronze in the form of sand and centrifugal castings.
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of round, non-welded tubing free from OD surface seams.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the engineering requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys by use of silver alloy filler metals, and the properties of such joints.
AMS B Finishes Processes and Fluids Committee
This specification covers two methods for determining the percentage of delta ferrite in steels and other iron alloys. When applicable, this specification will be invoked by the material specification.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Recommended Practice provides procedures for determining shot peening coverage and relating coverage to part exposure to the media stream. Effectiveness of shot peening is directly dependent on coverage. Inadequate or excessive coverage can be detrimental to fatigue strength and component life.
Surface Enhancement Committee
This procedure is applicable to brake pad modes between 500 Hz and 16 kHz. The parameters measured with this procedure are defined as the first three natural frequencies, fn (n = 1, 2, 3), and the corresponding loss factors, η.
Brake NVH Standards Committee
This standard establishes the design requirements for a fiber optic serial interconnect protocol, topology, and media. The application target for this standard is the interconnection of multiple aerospace sensors, processing resources, bulk storage resources and communications resources onboard aerospace platforms. The standard is for subsystem interconnection, as opposed to intra-backplane connection.
AS-1A Avionic Networks Committee
This SAE Aerospace Standard (AS) defines the requirements for a convoluted polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in aerospace fluid systems at temperatures between -65 °F and 400 °F for Class 1 assembly, -65 °F and 275 °F for Class 2 assembly, and at operating pressures per Table 1. The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, shall be subject to the approval of the procuring activity.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This document establishes test plans/procedures for the AS5643 Standard that by itself defines guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. This test specification defines procedures and criteria for testing device compliance with the AS5643 Standard.
AS-1A Avionic Networks Committee
This SAE Recommended Practice establishes consistent test procedures for determination of steady-state directional control properties for passenger cars and light trucks with two axles. These properties include the steering-wheel angle gradient, reference steer angle gradient, sideslip angle gradient, vehicle roll angle gradient, and steering-wheel torque gradient with respect to lateral acceleration. They also include the yaw velocity gain, lateral acceleration gain, and sideslip angle gain with respect to steering-wheel angle. Additionally, the characteristic or critical speed and the front and rear wheel steer compliances may be determined.
Vehicle Dynamics Standards Committee
This Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in 400 °F 5000 psi, aircraft and missile hydraulic fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This document describes a method for measuring transient force histories generated by the impact of a soft or frangible projectile on a thin slicer oriented in a plane parallel to the direction of the projectile motion. The slicer is intended to be representative of a typical turbofan engine fan blade. The document describes the hardware and instrumentation required as well as the processing and data reduction required to compute force. In this test, a projectile impacts a relatively thin, flat, blade-like device with a sharp leading edge (the “slicer”). The direction of motion of the projectile is parallel to the plane of the slicer. The test is designed to minimize lateral motion in the projectile as a result of the impact. The intended impact velocity range for this test is between approximately 50 and 300 m/sec. The slicer has a width greater than the largest diameter of the projectile and is supported on a fixture instrumented to measure force. The projectile material is expected
G-28 Simulants for Impact and Ingestion Testing Committee
This data dictionary provides definitions for quantities, measurement units, reference systems, measurands, measurements, and quantity modalities commonly used in the command and control of cyber-physical systems. A cyber-physical system is an engineered system that is built from, and depends upon, the seamless integration of computational algorithms and physical components. Cyber-physical systems are often interconnected via data links and networks. The term encompasses intelligent vehicles and devices that operate in any environment, including robotic and autonomous systems.
AS-4 Unmanned Systems Committee
This specification covers a silicone-rubber-remover compound in the form of a liquid supplied as a ready-to-use product.
AMS J Aircraft Maintenance Chemicals and Materials Committee
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