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AS8049A currently requires adjustable features on aircraft seats to be designed so they can be returned to the positions required for taxi, takeoff and landing by the occupant without the release of the occupant restraints. This ARD will demonstrate Aviation Industry support for revisions to TSO-C39c and TSO-C127a to allow Technical Standard Order (TSO) approval of aircraft seat products designed with adjustable features that require the release of occupant restraints to return the feature to the taxi, takeoff and landing position.

• Define sub-roles within the primary J3016 roles • Define different human capabilities and list what those are (including definition of “capability”) • Frame issues • Document open questions

This SAE Recommended Practice applies to both Original Equipment Manufacturer (OEM) and aftermarket message-generating systems for light and heavy vehicles. The recommended practice covers both message prioritization and presentation (including simultaneous display of messages) for visual and auditory modalities. In addition, this recommended practice will consider temporal aspects of external events (e.g. merging into heavy traffic, time-to-collision) and their impact on temporal presentation and format (including multi-modal) of messages.

SAE Metallic Materials Testing Laboratories, is a technical Subcommittee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for Aerospace Metallic Materials Testing Requirements. The Subcommittee works in conjunction with related bodies such as the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA. The objectives of MTL are to: • Develop Aerospace Specifications (AS) for the control of materials testing specific to aerospace applications. • Provide a forum for the exchange of technical information related to aerospace materials testing. • Further the adaptation of industry sponsored material specifications through coordination with PRI and associated organizations. • Establish a system to ensure aerospace specifications are controlled.

This SAE Aerospace Recommended Practice (ARP) provides guidance to develop and assure validation and verification of IVHM systems used in autonomous aircraft, vehicles and driver assistance functions. IVHM covers a vehicle, monitoring and data processing functions inherent within its sub-systems, and the tools and processes used to manage and restore the vehicle’s health. The scope of this document is to address challenges and identify recommendations for the application of integrated vehicle health management (IVHM) specifically to intelligent systems performing tasks autonomously within the mobility sector. This document will focus on the core aspects of IVHM for autonomous vehicles that are common to both aerospace and automotive applications. It is anticipated that additional documents will be developed separately to cover aspects of this functionality that are unique to each application domain.

The documents listed in this ballot are being proposed for reaffirmation

This SAE Aerospace Information Report will be a compilation of system safety engineering and management terms and definitions covering concepts used across multiple products and disciplines

This recommended practice provides users with raw GNSS measurements to facilitate positioning, navigation, or timing solutions.

This standard provides recommended practices to significantly enhance the ability of PNT users to defend against a range of interference, jamming, and spoofing phenomena.

Provide a high level standard that resolves the gaps of SAE J1739 and other FMEA standards to support companies that currently use the cancelled MIL-Std-1629a FMECA Standard. The new standard will define: 1) the relationship and connection between FMEA/FMECA and maintainability and Supportability. 2) define the purpose of qualitative and quantitative criticality analysis and recommendations on usage of each within FMEA/FMECA. 3) how and when to incorporate Model-Based systems engineering to support FMEA/FMECA

This standard establishes the inertial and health monitoring data interface requirements for inertial measurement units used for military and aerospace vehicle applications.

This standard establishes the SAE2020 compliant inertial data interface requirements for simulator integration with inertial navigation systems used for military and aerospace vehicle applications.

This standard defines a test plan to verify an inertial measurement unit interface meets the requirements of SAE2020.

There are numerous GNSS user equipment interface standards in use that provide some form of timing and/or positioning information. This document incorporates their essential content into a uniform array that will enable seamless interoperation with eLoran.

The Design for Maintainer (DFM) standard identifies the recommended approach for conducting Design for Maintainability activities in support of system acquisition programs. The standard identifies general requirements and processes of a successful DFM program during concept and design development to ensure the lowest possible ownership costs. This standard provides specific detailed contractor requirements for DFM activities inclusive of the Human Engineering domain. The standard is consistent with MIL-STD-46855 and SAE 6906 Human Systems Integration. And DFM standard practices support performance of activities in coordination with other associated disciplines such as maintainability, supportability, and integrated logistics.

There are numerous GNSS user equipment interface standards in use that provide some form of timing and/or positioning information. This document incorporates their essential content into a uniform array that will enable seamless interoperation with eLoran.

This interface control document defines the (e)Loran based alternate PNT interface for the EGI. It provides technical descriptions of definitions, specifications, and explanations for general distribution to providers, manufacturers, and consumers.

This standard provides guidelines for resilient GNSS receivers.

This standard defines how a resilient GNSS receiver provides enough information for an alternative PNT source to be selected when the GNSS receiver does not meet the required levels of accuracy, availability, integrity, or continuity even when the GNSS signals are subject to interference

This recommended practice enables users to utilize raw GNSS measurements to improve positioning, navigation, and/or timing solutions.