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Standard

Inertia Dynamometer Rotor Crack Test Procedure for Air Disc Brakes

2018-04-27
WIP
J3080

This Recommended Practice applies to commercial vehicles equipped with air disc brakes and above 4536 kg of Gross Vehicle Weight Rating. Other assessments on the friction material or rotor related to wear, durability, correlation to product life, noise, judder, compliance to specific regulations, etc., are not part of this RP (Recommended practice).

Standard

Webbing, Tubular, Low Modulus Aramid, 3/4 (19) Wide, 2300 (10 231) Breaking Strength

2018-04-26
WIP
AMS3799/2D
This specification covers one width and one strength of low modulus aramid tubular webbing. This product has been used typically in construction of parachutes, but usage is not limited to such applications. 3/4 inch (19 mm) wide low modulus aramid tubular webbing having 2,300 pounds force (10,231 N) breaking strength.
Standard

Webbing, Tubular, Low Modulus Aramid 1 (25) Wide, 4000 (17,793) Breaking Strength

2018-04-26
WIP
AMS3799/3D
This specification covers one width and one strength of low modulus aramid tubular webbing. This product has been used typically in construction of parachutes, but usage is not limited to such applications. 1 inch (25.4 mm) wide low modulus aramid tubular webbing having 4000 pounds force (17,793 N) breaking strength.
Standard

Webbing, Tubular, Low Modulus Aramid, 3-3/16 (81) Wide, 2250 (10 008) Breaking Strength

2018-04-26
WIP
AMS3799/4D
This specification covers one width and one strength of low modulus aramid tubular webbing. This product has been used typically in construction of parachutes, but usage is not limited to such applications. 3-3/16 inches (81 mm) wide low modulus aramid tubular webbing having 2250 pounds force (10,008 N) breaking strength.
Standard

Cloth, Airplane, Mercerized Cotton, 80 Pounds Force (356 N) Breaking Strength

2018-04-26
WIP
AMS3806G
This specification covers one strength and one weave of mercerized cotton cloth known as "airplane cloth." This cloth has been used typically for covering aircraft surfaces, such as wings, fuselage, ailerons, elevators, and other airfoil surfaces, but usage is not limited to such applications.
Standard

SAFE-LIFE LIMITS FOR LANDING GEAR STRUCTURES

2018-04-26
WIP
AIR6949
This document describes the approaches taken to define safe-life limits for the management of fatigue in landing gear structures, and the substantiation of those limits through full-scale fatigue testing. The safe-life scatter factors considered in a range of military and civil regulatory standards are also reviewed.
Standard

Motorcycle Auxiliary Front Lamps

2018-04-26
WIP
J1306
This engineering design specification provides parameters and general requirements for auxiliary front lamps to be used on motorcycles.
Standard

SAE AMS AM Metals Data Submission Guidelines (for Additive Manufactured Metals)

2018-04-25
WIP
AIR7301
This document summarizes data guidelines to establish statistically determined minimum values for the mechanical properties (i.e., static mechanical property) for additive manufactured (AM) metals published in SAE AMS specifications. Such values are not intended to be used in designing actual parts.
Standard

Icing Wind Tunnel Interfacility Comparison Tests

2018-04-25
WIP
AIR5666A
This SAE Aerospace Information Report (AIR) presents and discusses the results of tests of three models in six icing wind tunnels in North America and Europe. This testing activity was initiated by the Facility Standardization Panel of the SAE AC-9C Aircraft Icing Technology Subcommittee. The objective of the testing activity was to establish a benchmark that compared ice shapes produced by icing wind tunnels available for use by the aviation industry and to use that benchmark as a basis for dialogue between facility owners to improve the state-of-the-art of icing wind tunnel technology.
Standard

Electric Vehicle Power Transfer System Using a Three-Phase Capable Coupler

2018-04-25
CURRENT
J3068_201804
This document covers the general physical, electrical, functional, testing, and performance requirements for conductive power transfer to an Electric Vehicle using a Coupler capable of, but not limited to, transferring three-phase AC power. It defines a conductive power transfer method including the digital communication system. It also covers the functional and dimensional requirements for the Electric Vehicle Inlet, Supply Equipment Connector, and mating housings and contacts. Moveable charging equipment such as a service truck with charging facilities are within scope. Charging while moving (or in-route-charging) is not in scope.
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