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AE-8C2 Terminating Devices and Tooling Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers four series of electrical connectors (plugs and receptacles) with removable crimp contacts and accessories (see 6.1). AS81511 connectors are not recommended for new design. All AS81511 detail sheets that specified class D and/or H have been cancelled without replacement, therefore all class D and H requirements have been deleted from this specification. Electrical, mechanical and environmental features of these connectors include: Environment resisting at sea level and high altitude. Quick disconnect. RFI/EMI (Radio Frequency Interference/Electromagnetic Interference) protection (includes shell to shell grounding spring members). High density insert arrangements. Low level circuit capabilities. Scoop-proof. Fluid resistant class provided. High temperature class provided. Several voltage service ratings available. Individual contact release from the rear of the connector (series 3 and 4 only).
AE-8C1 Connectors Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This report revises ARD50015 document to the AIR format. This report, as was the original, is intended to complement ARP1420C and AIR1419C documents issued by the SAE S-16 Committee on spatial total-pressure distortion. These previous documents addressed only total-pressure distortion and excluded total temperature distortion. The subject of inlet total temperature distortion is addressed in this report with some background and identification of the problem area. The status of past efforts is reviewed, and an attempt is made to define where we are today. Deficiencies, voids, and limitations in knowledge and test techniques for total temperature distortion are identified.
S-16 Turbine Engine Inlet Flow Distortion Committee
The purpose of this SAE Aerospace Information Report (AIR) is to present a sample of the range of tire chine designs approved for application on aircraft requiring non-standard water spray deflection.
A-5C Aircraft Tires Committee
This standard specifies the system requirements for an on-board vehicle-to-vehicle (V2V) safety communications system for light vehicles1, including standards profiles, functional requirements, and performance requirements. The system is capable of transmitting and receiving the SAE J2735-defined basic safety message (BSM) [1] over a dedicated short range communications (DSRC) wireless communications link as defined in the Institute of Electrical and Electronics Engineers (IEEE) 1609 suite and IEEE 802.11 standards [2] to [6].
V2X Core Technical Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers a low-alloy steel in the form of welding wire. Type 2 - copper coated wire was removed from this document (see 8.4).
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing.
AMS E Carbon and Low Alloy Steels Committee
This specification covers piston rings fabricated from cast iron.
AMS E Carbon and Low Alloy Steels Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies