Refine Your Search

Search Results

Standard

Gaseous Nitrocarburizing

2018-04-16
WIP
AMS2759/13
This specification covers the engineering requirements for producing a continuous thin epsiloniron- carbonitride compound layer on parts by means of a gaseous, low temperature process, and properties of the case.
Standard

Ice Crystal and Mixed Phase Icing Tunnel Testing of Air Data Probes

2018-04-16
WIP
AIR6974
This document provides information on current practices for testing air data probes to 14 CFR Part 33 Appendix D ice crystal and mixed phase icing conditions. This AIR is primarily concerned with techniques for measuring the flow and icing environment in the test facility. While the focus of this report is the testing of air data probes, techniques described may be applicable to Appendix D tests of other aerospace equipment as well.
Standard

AM Polymer Data Submission Guidelines

2018-04-16
WIP
AIR7300
To summarize data submission guidelines to establish statistically determined minimum values for the mechanical properties (i.e., static mechanical property) for additive manufactured (AM) polymers published in SAE AMS specifications.
Standard

Butadiene - Acrylonitrile (Nbr) Rubber for Fuel-Resistant Seals, 60 to 70

2018-04-15
WIP
AMSP5315C
This specification covers a butadiene - acrylonitrile (NBR) rubber in the manufacturer of molded seals.

These products have been used typically at temperatures from -65 degrees F (-54 degrees C) to +180 degrees F (+182 degrees C) where resistance to fuel is required, but usage is not limited to such applications. Each application should be considered individually.

Standard

Sheet and Strip Surface Finish Nomenclature

2018-04-12
WIP
AS4194B
This SAE Aerospace Standard (AS) defines the nomenclature for surface finishes commonly used for sheet and strip in aerospace material specifications. It is applicable to steel and to iron, nickel, cobalt, and titanium base alloys.
Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

2018-04-12
WIP
AS1650F
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
X