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Viewing 1 to 30 of 922
2016-05-02
Standard
AIR6007
The purpose of this document is to provide guidance on in-flight thrust determination of engines that are impacted by intentional or unintentional thrust vectoring. However, as indicated in the Foreword, the field of aircraft thrust vectoring is varied and complex. For simplicity and coherence of purpose, this document will be limited in scope to multi-axis thrust vectoring nozzles or vanes attached to the rear of the engine or airfame; single-axis thrust vectoring and unintentional thrust vectoring (fixed shelf or deck configuration) are special cases of this discussion. Specifically excluded from this scope are thrust vectoring created primarily by airframe components such as wing flaps, etc.; lift engines, propulsive fans and thrust augmenting ejectors; and powerplants that rotate or otherwise move with respect to the airframe.
2016-05-02
Standard
AS1975G
This SAE Aerospace Standard (AS) defines the requirements for a polytetrafluoroethylene (PTFE) lined, para-aramid fiber reinforced, hose assembly suitable for use up to 4000 psi, and up to 275 °F, aircraft and missile hydraulic and pneumatic systems.
2016-04-26
WIP Standard
AS6386
This document, the JAUS Automated Behaviors and Diagnostics Service Set, defines a message-passing interface for services commonly found in mobile unmanned systems. These services represent the platform-independent capabilities common across all domains. Additional capabilities are specified in the JAUS Core Service Set (AS5710) and are frequently referenced herein.
2016-04-25
WIP Standard
AS6146A
Scope unavailable.
2016-04-20
Standard
ARP6852A
This document describes methods that are known to have been used by aircraft manufacturers to evaluate aircraft aerodynamic performance and handling effects following application of aircraft ground deicing/anti-icing fluids (“fluids”), as well as methods under development. Guidance and insight based upon those experiences are provided, including: - Similarity Analyses - Icing Wind Tunnel Tests - Flight Tests - Computational Fluid Dynamics and other Numerical Analyses This document also describes: - The history of evaluation of the aerodynamic effects of fluids - The effects of fluids on aircraft aerodynamics - The testing for aerodynamic acceptability of fluids for SAE and regulatory qualification performed in accordance with AS5900 - Additionally, Appendices A to E present individual aircraft manufacturers’ histories and methodologies which substantially contributed to the improvement of knowledge and processes for the evaluation of fluid aerodynamic effects.
2016-04-05
WIP Standard
AS6453A

This SAE Aerospace Standard (AS), identical to ISO 14186, specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used either:

    a. in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or
    b. on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.

2016-04-04
Standard
AS5643B
IEEE-1394b, Interface Requirements for Military and Aerospace Vehicle Applications, establishes the requirements for the use of IEEE Std 1394™-2008 as a data bus network in military and aerospace vehicles. The portion of IEEE Std 1394™-2008 standard used by AS5643 is referred to as IEEE-1394 Beta (formerly referred to as IEEE-1394b.) It defines the concept of operations and information flow on the network. As discussed in 1.4, this specification contains extensions/restrictions to “off-the-shelf” IEEE-1394 standards and assumes the reader already has a working knowledge of IEEE-1394. This document is referred to as the “base” specification, containing the generic requirements that specify data bus characteristics, data formats, and node operation.
2016-03-22
WIP Standard
AMS2757C
This specification covers the engineering requirements for producing a continuous thin epsilon iron carbonitride compound layer on parts by means of a gaseous, low-temperature process, and properties of the case.
2016-02-24
Standard
ARP4740A
This ARP addresses the issue of passengers smoking in aircraft lavatories and the need to improve warnings about the danger of fire caused by smoking.
2016-02-17
WIP Standard
ARP6366
This ARP document defines a comprehensive and widely-accepted set of guidelines for use or design of fiber optic sensors on aerospace applications.
2016-02-10
WIP Standard
ARP4927A
This SAE Aerospace Recommended Practice (ARP) provides guidance to achieve the optimum integration of new aircraft systems which have an impact on the cockpit layout or crew operating procedures. This process may also be used for modification of existing cockpits.
2016-02-04
WIP Standard
AIR6523
This data dictionary provides a mathematically coherent set of definitions for quantity types used in data models for unmanned systems. In this data dictionary, a quantity is defined as a property of a phenomenon, substance, or body whose value has magnitude.
2016-02-03
WIP Standard
ARP5595B
This SAE Aerospace Recommended Practice (ARP) aims at providing general utilization guidelines and calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/lashing arrangements performed to restrain cargo on board civil transport aircraft during flight: a. cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems meeting the requirements of NAS 3610, or b. additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or CG, or c. non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck or main deck containerized cargo compartments of an aircraft, or d. individual pieces of load loaded in non-containerized (bulk loaded) baggage or cargo compartments.
2016-02-03
WIP Standard
AS36102B
This SAE Aerospace Standard (AS) provides requirements on how to test air cargo Unit Load Devices (ULD).
2016-01-25
WIP Standard
AIR6373
pilots, air traffic controllers, dispatchers, aviation meteorologists
2016-01-25
WIP Standard
AS81914/7A
Scope unavailable.
2016-01-18
WIP Standard
ARP4102/10B
This document presents criteria for flight deck controls and displays for airborne collision avoidance systems providing vertical-only guidance, and provides design guidance for operational, functional, and installation characteristics and requirements for airborne collision avoidance systems in existing and future aircraft.
2016-01-18
WIP Standard
ARP4101/8A
This document recommends criteria for standardization of flight deck interior doors and their operation which will provide optimum use under normal and emergency conditions.
2016-01-15
WIP Standard
AIR6521
This document provides an example Interface Control Document (ICD) based on the Object Management Group’s (OMG) Data Distribution Service (DDS) specifications. The platform-specific mapping is derived from the UCS Model and a series of non-normative platform implementation choices. The machine readable ICD and results of the implementation-specific mapping are provide in Interface Description Language (IDL) format.
2016-01-15
WIP Standard
AS6512
This Architecture Description (AD) applies to the Unmanned Aircraft System (UAS) Control Segment (UCS) Architecture. It identifies all the elements of the UCS Architecture. It describes the UCS system-of-interest and environment, its stakeholders and their system concerns. It provides the rationale for significant architectural decisions. It describes the contributing views and models of the UCS Architecture, together with its governing architecture framework.
2015-12-30
WIP Standard
AS6250/3
This standard defines the design, performance and interoperability requirements for a fiber optic expanded beam, pin and socket termini incorporating a C-LENS configuration terminated onto single mode or multimode optical fiber for installation in MIL-DTL-38999 Series III size 16 cavities.
2015-12-27
Standard
AIR5631A
The purpose of this document is to provide a listing for current commercial and military aircraft landing gear systems and their types and manufacturers. Data has been provided for the following commercial aircraft types; wide body jet airliners, narrow body jet airliners, and turboprop/commuter aircraft and the following military aircraft types; fighter, bomber, cargo, attack, surveillance, tanker and helicopter categories. The aircraft that have been included in this document are in operational service either with airlines, business, cargo or military operators. No information is presented for aircraft that are currently being developed or that are not in extensive usage. This document will provide an informational reference for landing gear engineers to access when evaluating other gear and aircraft systems. Future revisions of this document will add aircraft as they enter into service.
2015-12-20
Standard
ARP1839
This Aerospace Recommended Practice (ARP) is a general overview of typical airborne engine vibration monitoring (EVM) systems applicable to fixed or rotary wing aircraft applications, with an emphasis on system design considerations. It describes EVM systems currently in use and future trends in EVM development. The broader scope of Health and Usage Monitoring Systems, (HUMS) is covered in SAE documents AS5391, AS5392, AS5393, AS5394, AS5395, AIR4174. This ARP also contains the essential elements of AS8054 which remain relevant and which have not been incorporated into Original Equipment Manufacturers (OEM) specifications.
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