Search
Advanced Search
of the following are true
(
)

Results

Items (219,718)
Aluminum Alloy, Forgings 4.5Cu 0.85Si 0.8Mn 0.5MgAMS4135M (Current)4/1/1986
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and stock for forgings on rolled rings. Primarily for applications, such as aircraft structural members, requiring material with moderately high strength. Certain design and processing procedures may cause these forgings to become susceptible to stress corrosion cracking; ARP 823 recommends practices to minimize such conditions.
AMS D Nonferrous Alloys Committee
595 Barometric Altitude Rate Computer (BARC)ARINC595 (Current)2/1/1975
This standard provides general guidance for the design and installation of a BARC for use with a GPWS. The BARC generates an electrical rate signal from pneumatic pressure supplied by the aircraft static pressure system. The BARC unit is intended primarily for use with ground proximity warning equipment in aircraft that do not have a suitable electrical signal for altitude rate.
Airlines Electronic Engineering Committee
800P3-2 Cabin Connectors and Cables, Part 3, Specification of CablesARINC800P3-2 (Current)7/7/2025
This specification describes the general cable and wire characteristics recommended for use in cabin systems for commercial aircraft. Supplement 1 adds new definitions of 26 AWG 2-pair (Quad), 4-pair (Oct) data cables, and copper-fiber optic hybrid composite cables. Supplement 2 includes definitions of shielded twisted pair ethernet over single pair for data rates up to 1000Base-T1.
Airlines Electronic Engineering Committee
850 System Level Guidance for Data Loading LRU Target SystemsARINC850 (Current)1/12/2024
This document provides LRU Target System manufacturers, airframe manufacturers, and others with principles, concepts, and guidance for the design of data loading targets and complex data loading target systems. The mechanisms described in this paper apply to federated LRUs and complex platforms, such as airborne servers and data loading of IMA systems. The document guides data loading system design for Target Systems: How to avoid common pitfalls during the system/software design architectural design phase Specific considerations to actively decide on in early conceptual design phases Increase of useability and robustness for the end-user and maintainer of data loading targets This document focuses on reaching common design objectives for Target System data loading systems and circumventing repeatedly occurring issues rooted in system design. Commonly desired design objectives include: Architectural choices – Simplify the upload process of LRU Target Systems of the same type Reducing
Airlines Electronic Engineering Committee
Aluminum Alloy, Forgings 4cu 2ni 1.5mg 0.7si as FabricatedAMS4142C (Current)1/1/1991
AMS D Nonferrous Alloys Committee
722 Projection Video System (PVS)ARINC722 (Current)11/5/1980
This standard sets forth design guidance and airplane interfaces for the development and installation of a PVS in commercial transport aircraft. Basic function of the PVS is to display projected television images to each passenger.
Airlines Electronic Engineering Committee
438 Guidance For Acceptance of Flight Simulation Training DevicesARINC438 (Current)9/1/2013
This document provides guidance to the flight simulation industry for the acceptance of a Flight Simulation Training Device (FSTD). It may also be used during Request for Proposal (RFP) and contract discussions for an FSTD purchase to define the requirements for acceptance of the device. It is intended to be usable for all FSTD devices - types, repeat, prototype, updated, new, and used - and for different levels of qualification being sought.
Flight Simulator Engineering and Maintenance Committee
607-3 Design Guidance for Avionics EquipmentARINC607-3 (Current)8/1/1998
This standard provides general guidelines for the design of avionics equipment. It represents the desires of the airline industry resulting from extensive airline experience. Manufacturers are urged to use this standard when initially starting the design of new equipment. Airplane Personality Module (APM) specifications are included.
Airlines Electronic Engineering Committee
613 Guidance for Using the Ada Programming Language in Avionics SystemsARINC613 (Current)1/1/1988
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
Airlines Electronic Engineering Committee
439B Simulated Air Traffic Control Environments in Flight Simulation Training DevicesARINC439B (Current)8/31/2020
This document provides guidance on provision of SATCE systems in Flight Simulation Training Devices (FSTDs) for the benefit of flight crew training. This work builds upon that originally undertaken by International Air Transport Association (IATA) Flight Simulator Working Group in 2002, and further developed in the International Civil Aviation Organization (ICAO) Doc. 9625 Vol 1, Part 2, Editions 3 and 4. This document is intended to be a practical starting point that can serve as the basis for future developments of SATCE.
Flight Simulator Engineering and Maintenance Committee
Heat Treatment, Carbon, Low-Alloy and Specialty SteelsAMS2760A (Current)1/1/1987
This specification covers the procedure for through-hardening and related heat treatments of carbon, low-alloy, and specialty steel parts to produce specified mechanical properties within the capability of each respective steel. Heat treating processes such as induction hardening, flame hardening, carburizing, nitriding, austempering, and martempering are recognized processes but are not covered by this specification.
AMS E Carbon and Low Alloy Steels Committee
538B-1 Hand-Held MicrophoneARINC538B-1 (Current)2/1/1983
This standard describes a hand-held microphone for use with airborne radio installations.
Airlines Electronic Engineering Committee
446 Guidance for Flight Training Device Documentation Structure, Content, and MaintenanceARINC446 (Current)1/1/2016
The intent of this standard is to provide guidance so the documentation provided with the Flight Simulation Training Device (FSTD) reflects and describes the delivered FSTD, including the description and definition of third party equipment and content. In the context of documentation guidance found in this report, the term FSTD is meant to include all levels of flight simulation devices. The documentation described herein is required for the operator to independently support the FSTD in the maintenance, operation, and update of the device throughout the lifetime of the device. This report describes a superset of a possible range of documentation involved in the initial delivery or an update of a FSTD. The deliverable documentation set for a particular FSTD may vary depending on the level of device (e.g., flat panel trainer versus a full flight simulator) as well as issues related to intellectual property, export compliance, technical requirements, and/or contractual agreements.
Flight Simulator Engineering and Maintenance Committee
413A Guidance for Aircraft Electrical Power Utilization and Transient ProtectionARINC413A (Current)10/1/1989
This standard provides guidance to airframe manufacturers concerning the utilization of aircraft electrical power. This standard covers the description of basic power characteristics, and detailed guidance concerning transient protection, interference control, and equipment installation considerations.
Airlines Electronic Engineering Committee
677 Installation Standards for Low Frequency Underwater Locator Beacon (LF-ULB)ARINC677 (Current)7/1/2015
This document provides aircraft installation requirements for a Low Frequency Underwater Locator Beacon (LF-ULB) transmitting on a frequency of 8.8 kHz. ICAO Annex 6 Amendment 36, states that a LF-ULB shall be installed on all aircraft with a maximum certified take-off mass of over 27,000 kg, operating over water at particular distances to land suitable for making an emergency landing. ICAO Annex 6 Amendment 36 further states that an LF-ULB shall be installed by January 1, 2018.
Airlines Electronic Engineering Committee
436-1 Guidelines for Electronic Qualification Test GuideARINC436-1 (Current)9/20/2010
The purpose of ARINC Report 436 is to provide Flight Simulation Training Device (FSTD) users, suppliers and regulatory authorities a set of guidelines for Electronic Qualification Test Guide (eQTG) systems. This document is intended to be supplementary to existing regulatory authority requirements. This document is not designed to direct the use of certain technologies or platforms, but to outline the minimum requirements of an eQTG system. The choice of the technology used to meet these requirements is left to the system's designers and users.
Flight Simulator Engineering and Maintenance Committee
724B-6 Aircraft Communications Addressing and Reporting System (ACARS)ARINC724B-6 (Current)2/24/2012
This standard describes the 724B version of the airborne components of ACARS, and is intended for use in conjunction with VHF radio equipment existing on the plane. This ACARS enhancement improves the ability of the system to provide air-to-ground and ground-to-air data communications.
Airlines Electronic Engineering Committee
Concentrate, Corrosion Preventive Compound, Aircraft EngineAMS3071B (Current)1/1/1990
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of January 1990.
AMS B Finishes Processes and Fluids Committee
792-2 Second-Generation Ku-Band and Ka-Band Satellite Communication SystemARINC792-2 (Current)8/25/2023
This standard sets forth the desired characteristics of a second-generation aviation Ku-band and Ka-band satellite communication (satcom) system intended for installation in all types of aircraft.
Airlines Electronic Engineering Committee
848 Media Independent Secure Offboard NetworkARINC848 (Current)6/19/2020
ARINC Specification 848 is a functional standard based on a protocol specification profile for a secured network interface. The purpose is to define a common method of initiating a mutually authenticated tunnel between an aircraft service and its Enterprise service. ARINC Specification 848 defines a standard implementation for securing the communications between an onboard Local Area Network (LAN) and an Enterprise LAN on the ground. Various aircraft network architectures and various air to ground communication channels (aka media) are accommodated in this document. For example, L-band Satellite Communication (Satcom), Ku/Ka-band Satcom, Gatelink Cellular, and Gatelink are considered.
Airlines Electronic Engineering Committee
408A Air Transport Indicator Cases and MountingARINC408A (Current)12/15/1976
This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system.
Airlines Electronic Engineering Committee
440 Guidelines for the Provisioning and Support of Training Equipment DataARINC440 (Current)10/1/2005
This document provides guidelines for the aviation industry to ensure that data and solutions for training are adequately provided in content and schedule, are cost effective, and are completely supported throughout the life of the equipment. It should be used at all appropriate levels within a company (e.g., Purchasing, Operations, Training) when purchasing or developing new aircraft, major aircraft modifications or training systems.
Flight Simulator Engineering and Maintenance Committee
485P1-4 Cabin Equipment Interfaces, Part 1, Head End Equipment ProtocolARINC485P1-4 (Current)6/30/2020
This standard defines the electrical characteristics, protocol and data content for a modified version of the EIA RS-485 data bus adapted for use with cabin electronics equipment. Specific cabin equipment interfaces are defined by ARINC 628.
Airlines Electronic Engineering Committee
591 Quick Access Recorder for AIDS System (QAR)ARINC591 (Current)7/1/1972
This standard provides design guidance for development and installation of a QAR, whose basic functions are to store digital data supplied at the output of an ARINC 573 FDAU or other similar acquisition unit and provide an easy access to this stored data for systematic ground processing for performance monitoring, maintenance monitoring or other purposes.
Airlines Electronic Engineering Committee
625-4 Industry Guide for Component Test Development and ManagementARINC625-4 (Current)7/27/2020
This standard provides guidance to those who develop avionics test programs and the source documentation on which they are based. This includes guidelines for all steps and phases within the TPS life cycle.
Avionics Maintenance Committee
814 -1 Extensible Markup Language (XML) Encoding and Compression StandardARINC814-1 (Current)1/18/2019
ARINC 814 defines an XML encoding and compression standard for aviation. It is based on the Open Geospatial Consortium (OGC) Binary XML document. Binary XML encoding is extended in a way that is both flexible and robust. Compression is added on top of the binary encoding. ARINC 814 is expected to be used with Aeronautical Databases, in particular, ARINC Specification 813: Embedded Interchange Format for Terrain Databases, ARINC Specification 815: Embedded Interchange Format for Obstacle Databases, and ARINC Specification 816: Embedded Interchange Format for Airport Mapping Database.
Airlines Electronic Engineering Committee
718A-5 Mark 4 Air Traffic Control Transponder (ATCRBS/Mode S)ARINC718A-5 (Current)10/5/2022
Mark 4 Air Traffic Control Transponder (ATCRBS/MODE S) describes an Air Traffic Control Radar Beacon System/Mode Select (ATCRBS/Mode S) airborne transponder with Extended Interface Functions (EIF). The ATC surveillance system is made up of airborne transponders and ground interrogator-receivers, processing equipment, and antenna systems. Mode S is a cooperative surveillance system for air traffic control with ancillary communications capabilities. ARINC 718A supports elementary surveillance. Provisional enhanced surveillance functionality is also defined as a customer option. The Mark 4 transponder, like its predecessor, will support Collision Avoidance System which includes TCAS and ACAS X functions.
Airlines Electronic Engineering Committee
614 Standard Firmware Loader for Avionics ShopsARINC614 (Current)9/1/1989
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
428 Considerations for Avionics Network DesignARINC428 (Current)10/1/1995
This standard provides the framework for developing a set of requirements for an avionics data bus network. This standard is intended to provide system-level considerations for the development of such a network, which may include a mix of standard data buses and private data buses.
Airlines Electronic Engineering Committee
Insulating Components, Molded, Electrical, Heat Shrinkable, Boot, Strain Relief and Sealing, StraightAS5258/1A (Current)2/8/2011
The complete requirements for acquiring the molded components described herein shall consist of this document and the latest issue of AS 5258.
AE-8C1 Connectors Committee
RIVET, SOLID, 100° FLUSH HEAD, NICKEL ALLOY UNS N06600AS123601C (Current)4/28/2018
E-25 General Standards for Aerospace and Propulsion Systems
Aircraft Flight Control Actuation System Failure-Detection MethodsAIR5273A (Current)12/16/2022
This SAE Aerospace Information Report (AIR) provides descriptions of aircraft flight control actuation system failure-detection methods. The fault-detection methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight controls.
A-6A3 Flight Control and Vehicle Management Systems Cmt
Type F-1 Fiber Optic Media Interface CharacteristicsAS4074/1B (Current)10/21/2016
This slash sheet specifies the operational parameters and characteristics of a particular implementation of the SAE Linear, Token Passing Bus (LTPB) Interface Unit. This slash sheet defines the following: a The physical media interface: This slash sheet specifies the characteristics of the optical interface to the physical bus media. b The minimum and maximum timing requirements for operation of this implementation of the LTPB. c The data coding used to encode and decode the data for transmission. d The default values to be loaded into the timers of the LTPB interface at power-up prior to intervention by the host processor.
AS-1A Avionic Networks Committee
FITTING END, WELD RING, SHORT TAPERED, DESIGN STANDARDAS5449B (Current)8/21/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
SCREW – OVAL FILLISTER HEAD, .138-32AS116925B (Current)2/1/2012
E-25 General Standards for Aerospace and Propulsion Systems
ARINC 834A Internet Protocol Based Aircraft Data Interface Function (ADIF)ARINC834A (Current)2/27/2023
This standard will define the Secure Open Data and Avionics Services (SODAS), the transport layers, and the suggested security mechanisms to enable communication between aircraft systems and an Electronic Flight Bag (EFB). Herein is the definition of a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. The purpose is to define a common set of services to be used to access specific avionics data that will enhance EFB applications.
Airlines Electronic Engineering Committee
CABLE, FIBER OPTIC, SINGLE-MODE, 4.6/125/450 µm, HERMETIC COATED, TIGHT BUFFERAS5382/4B (Current)9/21/2021
AS-3 Fiber Optics and Applied Photonics Committee
Oxygen Cylinder Installation GuideARP5021B (Current)9/13/2024
This document provides guidance for oxygen cylinder installation on commerical aircraft based on airworthiness requirements, and methods practiced within aerospace industry. It covers considerations for oxygen systems from beginning of project phase up to production, maintenance, and servicing. The document is related to requirements of DOT-approved oxygen cylinders, as well to those designed and manufactured to standards of ISO 11119. However, its basic rules may also be applicable to new development pertaining to use of such equipment in an oxygen environment. For information regarding oxygen cylinders itself, also refer to AIR825/12.
A-10 Aircraft Oxygen Equipment Committee
STUD, LOCKED IN-RING LOCKED, SERRATEDAS51989C (Current)9/28/2018
E-25 General Standards for Aerospace and Propulsion Systems
SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .2500-20 UNC - 3AAS115851C (Current)5/9/2022
E-25 General Standards for Aerospace and Propulsion Systems
424-23 Navigation System DatabaseARINC424-23 (Current)3/30/2022
This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Airlines Electronic Engineering Committee
800P2-2 Cabin Connectors and Cables, Part 2, Specification of Connectors, Contacts, and BackshellsARINC800P2-2 (Current)9/9/2021
This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.
Airlines Electronic Engineering Committee
DRUMS, METAL - SHIPPING AND STORAGE 3 TO 12 GALLONSAS27684 (Current)11/6/2017
AGE-2 Air Cargo
DRUMS, METAL - SHIPPING AND STORAGE 16 TO 80 GALLONSAS27683 (Current)11/6/2017
AGE-2 Air Cargo
669 Guidance for Lead-Based Soldering, Repair and ReworkARINC669 (Current)11/1/2004
This document provides guidance for using industry standards for developing a soldering program tailored to meet the specific requirements of the user. Moreover, it provides uniform guidance for maintenance facilities based on industry standards and, therefore, should be accepted throughout the air transport industry. This document is not a stand-alone document - it is intended to be used with the referenced international industry standards.
Avionics Maintenance Committee
437-1 Guidelines For Training FacilitiesARINC437-1 (Current)11/7/2012
The purpose of ARINC Report 437 is to provide guidance when planning a new training facility, extending an existing training facility, or adding new equipment to an existing facility.
Flight Simulator Engineering and Maintenance Committee
Characterizations of Aircraft Icing ConditionsAIR5396A (Current)1/20/2023
This SAE Aerospace Information Report (AIR) provides various graphical displays of atmospheric variables related to aircraft icing conditions in natural clouds. It is intended as a review of recent developments on the subject, and for stimulating thought on novel ways to arrange and use the available data. Included in this Report is FAR 25 (JAR 25) Appendix C, the established Aircraft Icing Atmospheric Characterization used for engineering design, development, testing and certification of civilian aircraft to fly in aircraft icing conditions.
AC-9C Aircraft Icing Technology Committee
Type E-1 Electrical Media Interface CharacteristicsAS4074/3B (Current)10/21/2016
This slash sheet specifies the operational parameters and characteristics of a particular implementation of the SAE Linear, Token Passing Bus (LTPB) Interface Unit. This slash sheet defines the following: a The physical media interface: This slash sheet specifies the characteristics of the electrical interface to the physical bus media. b The minimum and maximum timing requirements for operation of this implementation of the LTPB. c The data coding used to encode and decode the data for transmission. d The default values to be loaded into the timers of the LTPB interface at power-up prior to intervention by the host processor.
AS-1A Avionic Networks Committee
WASHER - LOCK, SPRING, CADMIUM PLATEAS122026B (Current)7/8/2014
E-25 General Standards for Aerospace and Propulsion Systems
FITTING, CONNECTOR, MULTIPLE FLUID PRESSURE LINE, 45°AS5164B (Current)5/19/2021
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Items per page:
1 – 50 of 219718