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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

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

Commercial Space Flight Seat Restraints

2018-04-24
WIP
AS6818
This standard shall apply to all commercial human suborbital spaceflights governed by the Commercial Space Launch Amendments Act of 2004.
Standard

Aerospace Military Aircraft Hydraulic System Characteristics

2018-04-24
WIP
AIR1899B
This SAE Aerospace Information Report (AIR) has been compiled to provide information on hydraulic systems fitted to the following categories of military vehicles: attack airplanes, fighter airplanes; bombers; anti-sub, fixed wing airplanes; transport airplanes; helicopters; and boats.

The purpose of this document is to provide hydraulic system information to military vehicle system and component designers in order to assist them in future aircraft fluid power system designs.

Standard

Methodology for Investigation of Flight Control System Anomalies

2018-04-24
WIP
AIR5875A
This SAE Aerospace Information Report (AIR) outlines comprehensive aircraft flight control system fault isolation methodology that has proven to be effective. The methodology presented in this Information Report has been used in several successful fault isolation efforts on military aircraft.
Standard

Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, Up to 1500 psi and 450 °F, Hydraulic and Pneumatic

2018-04-24
WIP
AS1946F
This SAE Aerospace Standard (AS) defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in aerospace hydraulic, fuel and lubricating oil systems at temperatures between -67 °F and 450 °F for Class I assemblies, -67 °F and 275 °F for Class II assemblies, and at nominal pressures up to 1500 psi. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated. 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, for example oxygen, shall be subject to the approval of the procuring activity.
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