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Viewing 1 to 30 of 493
2017-11-13
WIP Standard
AS6522A
The UCS technical governance comprises a set of policies, processes, and standard definitions to establish consistency and quality in the development of architecture artifacts and documents. It provides guidance for the use of adopted industry standards and modeling conventions in the use of Unified Modeling Language (UML) and Service Oriented Architecture Modeling Language (SoaML), including where the UCS Architecture deviates from normal UML conventions. This document identifies the defining policies, guidelines, and standards of technical governance in the following subjects: - Industry standards adopted by the AS-4UCS Technical Committee: These are the industry standards and specifications adopted by AS-4UCS in the generation and documentation of the architecture. - UCS Architecture Development: UCS specific policies on the development of the UCS Architecture. The AS-4UCS Technical Committee governance policies are intentionally minimal.
CURRENT
2017-11-09
Standard
ARP9107A
Limited to the commercial aerospace industry where a request is made for a PO to have Direct Delivery Authorization (DDA), which includes an Appropriate Arrangement (AA) between the PO and the Design Organization (DO). In this process the DO is responsible for ensuring the continuous updating of design and airworthiness data to the PO, whilst the PO is responsible for assurance that the manufactured article conforms to approved design and airworthiness data. The PO is responsible to provide airworthiness release documentation.
2017-10-31
WIP Standard
SAE1002
Latitude and Longitude is not a reference system commonly used by land-based First Responders. Street names and associated addresses are, but following disasters such as floods, fires, etc., they are often obscured or destroyed. The USNG is a point and area location grid reference system that provides a reliable and available geoaddressing capability that is an easy to use alternative to latitude and longitude.
CURRENT
2017-10-18
Standard
AS4877G
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.
CURRENT
2017-10-11
Standard
AS6089
This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that this verification document only verifies the specific requirements from AS5653 and does not verify all of the requirements invoked by documents that are referenced by AS5653. The procuring authority may require further testing to verify the requirements not explicitly defined in AS5653 and in this verification document.
2017-09-30
WIP Standard
AS9104B
These requirements are applicable to IAQG sector schemes when making use of ABs, CRBs and their auditors, for the assessment and certification/registration of supplier quality systems in accordance with the requirements of this document. The quality management system standard used by the CRB shall be 9100/9110/9120, as appropriate to the supplier's activities. It shall be applied to the supplier's complete Quality System that covers aerospace products. Sectors may use these requirements for other standards. IAQG members have committed to recognize the equivalence of certification/registration of a suppliers quality management system to either of the AS, EN or JISQ/SJAC standards.
2017-09-22
WIP Standard
AS6171/23
The intent of this test method is to describe high level processes to detect suspect/counterfeit (SC) Electrical, Electronic, and Electromechanical (EEE) Assemblies, covering both custom and military/commercial off-the-shelf (COTS) assemblies. This standard includes requirements for accreditation and certification of Laboratory and Laboratory personnel, and also, data collection, interpretation, and reporting as applicable to this test method. This standard covers EEE assemblies and includes electronic circuit card assemblies as defined under the definition for EEE Assembly and Electronic Circuit Card Assembly.
2017-09-21
WIP Standard
SAE9990/1
This eLoran transmitted signal standard provides technical descriptions of a data channel based on the tri-state pulse position modulation technique.
2017-09-21
WIP Standard
SAE9990/2
This eLoran transmitted signal standard provides technical descriptions of the data channel using 9th pulse modulation technique.
2017-09-11
WIP Standard
AS6171/6A
Through the use of ultra-high frequency ultrasound, typically above 10 MHz, Acoustic Microscopy (AM) non-destructively finds and characterizes physical features and latent defects (visualization of interior features in a layer by layer process) - such as material continuity and discontinuities, sub-surface flaws, cracks, voids, delaminations and porosity. AM observed features and defects can be indicators that the components were improperly handled, stored, altered or previously used. If AS6171/6 is invoked in the contract, the base document, AS6171 General Requirements shall also apply.
CURRENT
2017-09-05
Standard
AS13001A
This standard establishes the common requirements for training of DPRV personnel for use at all levels of the aerospace engine supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to its suppliers (reference 9100 and 9110 standards) and to perform product acceptance on its behalf. It is intended that organizations specify their DPRV requirements through the application of AS9117. While the delegating organization will use the AS13001 standard as the baseline for establishing DPRV process and product training, it may include additional contractual training requirements to meet its specific needs. The DPRV training material was primarily developed for aerospace engine supply chain requirements. However, this standard may also be used in other aerospace industry sectors where a DPRV process requiring specific training can be of benefit.
CURRENT
2017-08-28
Standard
AS13004
This standard defines requirements for the identification, assessment, mitigation, and prevention of risk in the manufacturing process through the application of Process Flow Diagrams (PFDs), Process Failure Mode and Effects Analysis (PFMEA) and Control Plans throughout the life cycle of a product. This standard aligns and collaborates with the requirements of AS9100, AS9102, AS9103, and AS9145. The requirements specified in this standard apply in conjunction with and are not alternative to contractual and applicable statutory and regulatory requirements. In case of conflict between the requirements of this standard and applicable statutory or regulatory requirements, the latter shall take precedence.
CURRENT
2017-08-24
Standard
TS201AR-6
No Scope available.
CURRENT
2017-08-24
Standard
TS202AR-13
No Scope available.
CURRENT
2017-08-24
Standard
TS201-6
No Scope available.
CURRENT
2017-08-24
Standard
TS202-13
No Scope available.
2017-08-17
WIP Standard
AS6810
The criteria defined in the standard shall be utilized by an Accreditation Body (AB) to establish compliance to AS6171 Test Methods Standard; General Requirements, Suspect/Counterfeit, Electrical, Electronic, and Electromechanical Parts, and associated AS6171 Test Methods.
CURRENT
2017-08-15
Standard
AS4115A
This test plan consists of two major sections for testing of MIL-STD-1553B data bus systems: Bus Network and System Integration Tests.
CURRENT
2017-08-14
Standard
AS4116A
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
CURRENT
2017-08-14
Standard
AS4114A
This test plan consists of two major sections for the production testing of bus controllers: Electrical tests and Protocol tests.
CURRENT
2017-08-10
Standard
AS4117A
This test plan defines the requirements of data bus components which comply with the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
CURRENT
2017-08-10
Standard
AS4112A
This test plan is broken into two major sections for the production testing of remote terminals: Electrical and Protocol.
CURRENT
2017-08-10
Standard
AS4111A
This SAE Aerospace Standard (AS) contains a sample test plan for AS15531 or MIL-STD-1553B Remote Terminals (RT) that may serve several different purposes. This document is intended to be contractually binding when specifically called out in a specification, Statement of Work (SOW), or when required by a Data Item Description (DID). Any and all contractor changes, alterations, or testing deviations to this section shall be separately listed for easy review.
2017-08-09
WIP Standard
AS42702
This document establishes techniques for verifying that a Mission Store Interface (MSI) complies with the interface requirements delineated in MIL-STD-1760 Revision E.
2017-08-08
WIP Standard
GEIASTD0005_1B

This standard defines the objectives of, and requirements for, documenting processes that assure customers and regulatory agencies that ADHP electronic systems containing Pb-free solder, piece parts, and PBs will satisfy the applicable requirements for performance, reliability, airworthiness, safety, and certifiability throughout the specified life of performance.

It is intended to communicate requirements for a Pb-free Control Plan (LFCP), hereinafter referred to as the Plan, and to assist the Plan Owners in the development of their own Plans. The Plan documents the Plan Owner’s processes that assure their customers, and all other stakeholders that the Plan Owner's products will continue to meet their requirements, given the risks stated in the Introduction.

2017-08-01
WIP Standard
ARP7208
This ARP establishes guidelines for the use of IEEE-802.3 as a data bus network in military and aerospace vehicles. It encompasses the data cable and its connections for a system utilizing 10Base-T, 100Base-T, 1000BASE-T and 10GBASE-T over copper medium dependent interfaces (MDI). This document contains extensions/restrictions to “off-the-shelf” IEEE-802.3 standards, and assumes that the reader already has a working knowledge of IEEE-802.3.
CURRENT
2017-07-18
Standard
ARP4386D
This SAE Aerospace Recommended Practice (ARP) provides the technical terms and nomenclature, together with their definitions and abbreviations/acronyms that are used in aerospace fluid power, actuation and control systems. NOTE: ARP490 and ARP4493 are sources for definitions specifically for electrohydraulic servovalves.
CURRENT
2017-07-12
Standard
AIR5451A
The landing gear system is a major and safety critical airframe system that needs to be integrated efficiently to meet the overall aircraft program goals of minimizing the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large-scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft. The document structure is divided into four sections: Landing Gear System Configuration Requirements (Section 3) Landing Gear System Functional Requirements (Section 4) Landing Gear System Integrity Requirements (Section 5) Landing Gear System Program Requirements (Section 6) The landing gear system encompasses all landing gear structural and subsystem elements.
CURRENT
2017-07-10
Standard
AIR5565
This aerospace information report (AIR) provides historical design information for various aircraft landing gear and actuation/control systems that may be useful in the design of future systems for similar applications. It presents the basic characteristics, hardware descriptions, functional schematics, and discussions of the actuation mechanisms, controls, and alternate release systems. The report is divided into two basic sections: Landing gear actuation system history from 1876 to the present. This section provides an overview and the defining examples that demonstrate the evolution of landing gear actuation systems to the present day. This section of the report provides an in depth review of various aircraft. A summary table of aircraft detail contained within this section is provided in paragraph 4.1. The intent is to add new and old aircraft retraction/extension systems to this AIR as the data becomes available.
2017-07-06
WIP Standard
SAE1001
The purpose of the "Integrated Project Processes for Engineering a System(IPPES)" Standard is to provide an integrated set of fundamental technical processes to aid a project in the engineering or reengineering of a system over the full life cycle. Covers systems that can be any combination of people (humans); product (hardware or software); or process (service). Applicable to any type of system: commercial or non-commercial; small or large, simple or complex, precedented or unprecedented; new or legacy or any combination of these characteristics.
Viewing 1 to 30 of 493