Advanced Search

Results

Items (212,784)

Guidance for Assessing the Damage Detection Capability of Structural Health Monitoring Systems

ARP6821 (Current)

02/07/2025

This document contains information and guidance necessary for the development of a representative, repeatable validation program that may be utilized to assess the capability of SHM systems. The nature of SHM data differs from that seen in traditional nondestructive evaluation (NDE) applications in that the position of SHM sensors is fixed and SHM data can be available much more frequently (if not continuously) over time. This document presents methodologies that can be used to arrive at SHM capability while considering the unique nature of SHM deployment. Each SHM system must be considered independently to determine the applicability and limitations of the guidance contained here for each SHM system being assessed.

Aerospace Industry Steering Committee on Structural Health

ACCESSORY, DUMMY STOWAGE RECEPTACLE, CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING (FOR SERIES 2 CONNECTORS)

AS81511/19A (Current)02/07/2025

AE-8C1 Connectors Committee

Assigned Identification Number Structure and Usage for North American Vehicles/Watercraft Other than Certified to Federal Regulations

J2750_202502 (Current)

02/07/2025

This SAE Recommended Practice establishes recommended procedures for the issuance, assignment, and structure of Identification Numbers on a uniform basis by states or provinces for use in an Assigned Identification Number (AIN).

VIN - WMI Technical Committee

ACCESSORY, COVER, PROTECTIVE, PLUG CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING (SERIES 2)

AS81511/17A (Current)02/07/2025

AE-8C1 Connectors Committee

REPAIR SLEEVE, PRIMARY WIRE INSULATION DAMAGE, ELECTRIC, PERMANENT, ENVIRONMENT RESISTANT, 150 °C MAXIMUM OPERATING TEMPERATURE

AS6224/1A (Current)02/07/2025

AE-8C2 Terminating Devices and Tooling Committee

661P1-9 Cockpit Display System Interfaces to User Systems, Part 1, Avionics Interfaces, Basic Symbology, and Behavior

ARINC661P1-9 (Current)02/09/2024

ARINC 661 defines logical interfaces to Cockpit Display Systems (CDS) used in all types of aircraft installations. The CDS provides graphical and interactive services to user applications within the flight deck environment. When combined with data from user applications, it displays graphical images to the flight deck crew. The document emphasizes the need for independence between aircraft systems and the CDS. This document defines the interface between the avionics equipment and display system graphics generators. This document does not specify the "look and feel" of any graphical information, and as such does not address human factors issues. These are defined by the airline flight operations community. Supplement 9 adds numerous changes and additions: Restructuring of the document for ease of use Addition of GpVertexBuffer and GpVertexRender Widgets Formalization of the Super Layer concept Generalization of input device text Timeout values for things like popups Extended Block

Airlines Electronic Engineering Committee

682 Guidance for Air Transport Service Bulletins

ARINC682 (Current)09/21/2022

This document provides industry guidance to supplement ATA standards and airframe requirements, addressing gaps and vague areas to move suppliers/vendors and airframers toward a common standard for format and wording in Vendor Service Bulletins (VSB) for Air Transport components. This document supplements the VSB guidance of iSpec 2200, providing clarity of requirements and resulting in a common standard wording and format of VSBs from all suppliers on all aircraft types. The guidance in this document is intended to be applied to VSBs created and released subsequent to the release of the guidance document and will not require the retroactive update of VSBs released prior to the creation and release of the guidance.

Avionics Maintenance Committee

781-9 Mark 3 Aviation Satellite Communication Systems

ARINC781-9 (Current)07/31/2024

This document sets forth the desired characteristics of an aviation satellite communication (satcom) system intended for installation in all types of commercial transport and business aircraft. This document provides general and specific guidance on the form factor and pin assignments for the installation of the avionics primarily for airline use. It also describes the desired operational capability of the equipment to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. This Characteristic specifies equipment using Inmarsat satellites operating in L-band. Ku-band and Ka-band equipment are specified in ARINC Characteristic 791, ARINC Characteristic 792, and ARINC Characteristic 793. Supplement 8 added Diplexer Low Noise Amplifiers (DLNA) to protect Inmarsat's Classic Aero and SwiftBroadband satcom equipment from possible ground-based LTE and ATCt (Ligado) interference. Supplement 9 expands the Dual Satcom Operation description

Airlines Electronic Engineering Committee

771-3 Low-Earth Orbiting Aviation Satellite Communication Systems

ARINC771-3 (Current)07/26/2024

This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Aviation Satellite Communication (Satcom) System avionics intended for installation in all types of aircraft including commercial transport, business, and general aviation aircraft. This document provides a description of the system components, aircraft interfaces, and satellite communication functions. It also describes the desired system performance and operational capability of the equipment. The equipment defined in these standards are capable of supporting Air Traffic Safety Serices. This characteristic specifies equipment using the next generation of Iridium satellites (referred to as Iridium NEXT) operating in L band. The services used on the NEXT network are referred to as Iridium Certus®. Based on maximum baud rates and antenna configuration different Certus Service Classes are offered. The Iridium NEXT/Certus satellite network replaces the Iridium legacy satellite network known as

Airlines Electronic Engineering Committee

850 System Level Guidance for Data Loading LRU Target Systems

ARINC850 (Current)01/12/2024

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

829 Guidance for Wireless Use of COTS Crew Devices

ARINC829 (Current)07/24/2024

This standard provides guidance on the preferred methods for establishing wireless connectivity and security for EFB devices. The Wireless Access Point (WAP) may be connected to an Aircraft Interface Device (AID) and/or the Inflight Entertainment System (IFE). Passenger devices are out of scope for this standard.

Airlines Electronic Engineering Committee

791P2-2 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 2, Electrical Interfaces and Functional Equipment Description

ARINC791P2-2 (Current)01/29/2024

This document (ARINC Characteristic 791, Part 2) provides the non-networking interface definition of the Mark I (ARINC 791) and Mark II (ARINC 792) Ku-Band and Ka-Band Satellite Communication (satcom) system intended for passenger entertainment on commercial transport aircraft. ARINC Characteristic 791 Part 1 of this document provides an overview of Ku-band and Ka-band satcom systems. System provisions, including Line Replaceable Unit (LRU) form factors, attachments, cooling, and inter-system wiring, are defined. Signals between the Modem/Modem Manager (Modman) and the Antenna Subsystem are described to permit interchangeability between any Modman and any Antenna Subsystem. ARINC Characteristic 791 Part 2 of this document provides the non-networking interface definition of the satcom system. Any signal crossing into or out of the communication system is documented to ease aircraft integration. Signals within the satcom system, and in particular, between the Modman and the Antenna

Airlines Electronic Engineering Committee

858P2-1 Internet Protocol Suite (IPS) for Aeronautical Safety Services, Part 2, IPS Gateway Air-Ground Interoperability

ARINC858P2-1 (Current)07/12/2024

ARINC 858 Part 2 provides aviation ground system gateway considerations necessary to transition to the Internet Protocol Suite (IPS). ARINC 858 Part 2 describes the principles of operation for an IPS gateway that enables ACARS application messages to be exchanged between an IPS aircraft and a ground ACARS host. ARINC 858 Part 2 also describes the principles of operation for an IPS gateway that enables OSI-based application messages to be exchanged between an IPS host and an OSI end system. This product was developed in coordination with ICAO WG-I, RTCA SC-223, and EUROCAE WG-108.

Airlines Electronic Engineering Committee

858P3-1 Internet Protocol Suite (IPS) for Aeronautical Safety Services, Part 3, Common IPS Radio Interface Protocol

ARINC858P3-1 (Current)07/12/2024

ARINC 858 Part 3 defines a Common IPS Radio Interface (CIRI) protocol for conveying radio status information and transferring digital data between the Airborne IPS System and Airborne Radios. This standard includes the functional description of the protocol, including applicable use cases, protocol message formats, and protocol operation for both control plane and data plane exchanges. The protocol is intended to operate over a variety of on-aircraft communication means, including, but not limited to, ethernet-based and ARINC 664-based aircraft networks. The reader should also reference ARINC 858 Part 1 and Part 2. This product was developed in coordination with ICAO WG-I, RTCA SC-223, and EUROCAE WG-108.

Airlines Electronic Engineering Committee

424-23 Navigation System Database

ARINC424-23 (Current)03/30/2022

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

812AP1-3 Standard Data Interferes for Galley Insert (GAIN) Equipment, Part 1, CAN Communications

ARINC812AP1-3 (Current)06/19/2023

The purpose of this specification is to define the general Galley Insert (GAIN) standardization philosophy, provide comprehensive equipment interfaces, and disseminate the most current industry guidance. Part 1 covers the Controller Area Network (CAN) data interface attachments, envelopes, and data content to be considered between all galley equipment using a Galley Data Bus as described within this specification. This document is intended as the successor and replacement for ARINC Specification 812. This document contains significant improvements to CAN data interfaces.

Airlines Electronic Engineering Committee

ARINC 834A Internet Protocol Based Aircraft Data Interface Function (ADIF)

ARINC834A (Current)02/27/2023

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

792-2 Second-Generation Ku-Band and Ka-Band Satellite Communication System

ARINC792-2 (Current)08/25/2023

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

810-7 Definition of Standard Interfaces for Galley Insert (GAIN) Equipment, Physical Interfaces

ARINC810-7 (Current)06/29/2023

ARINC 810 specifies physical attachments, envelopes, system connections, system performance attributes, design guidance, and qualification guidelines for the interchangeability of galley equipment.

Airlines Electronic Engineering Committee

718A-5 Mark 4 Air Traffic Control Transponder (ATCRBS/Mode S)

ARINC718A-5 (Current)10/05/2022

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

735C Traffic Computer, ACAS-X, and ADS-B Functionality

ARINC735C (Current)11/02/2022

This document describes Airborne Collision Avoidance System X (ACAS X) functionality and provides the necessary interface definitions and protocols to accommodate the requirements of RTCA DO-385: Minimum Operational Performance Standards for Airborne Collision Avoidance System X (ACAS X) ACAS Xa and ACAS Xo) (latest version applies) and the requirements of RTCA DO-386: Minimum Operational Performance Standards for Airborne Collision Avoidance System X (ACAS X) ACAS Xu (latest version applies). Additionally, this document describes interfaces and protocols necessary to accommodate Cockpit Display of Traffic Information (CDTI) based on the reception of Automatic Dependent Surveillance-Broadcast (ADS-B) data and Traffic Information Services–Broadcast (TIS-B) data. The equipment becomes ACAS X with ADS-B IN applications added, as defined by RTCA DO-317C: Minimum Operational Performance Standards for (MOPS) for Aircraft Surveillance Applications (ASA) Systems (latest version applies). ACAS

Airlines Electronic Engineering Committee

AGS912 BOW, D-SHAPED (FOR CHAIN SHACKLE)

AGS912-8 (Current)09/03/2024

Scope is unavailable.

Engine and Airframe Technical Standards Committee (TSC)

687 Onboard Secure Wi-Fi Network Profile Standard

ARINC687 (Current)06/18/2021

This document defines a standard implementation for strong client authentication and encryption of Wi-Fi-based client connections to onboard Wireless LAN (WLAN) networks. WLAN networks may consist of multi-purpose inflight entertainment system networks operating in the Passenger Information and Entertainment System (PIES) domain, dedicated aircraft cabin wireless networks or localized Aircraft Integrated Data (AID) devices operating in the Aircraft Information Services (AIS) domain. The purpose of this document is to focus on the client devices requiring connections to these networks such as electronic flight bags, flight attendant mobile devices, onboard Internet of Things (IoT) devices, AID devices (acting as clients) and mobile maintenance devices. Passenger devices are not within the focus of this document.

Airlines Electronic Engineering Committee

806-6 Fiber Optic Installation and Maintenance

ARINC806-6 (Current)09/04/2019

This document defines recommended general practices for the maintenance and restoration of fiber optic systems. It is the intention of this document to outline proven practices and general standards of workmanship for technicians engaged in fiber optic maintenance and repair.

Airlines Electronic Engineering Committee

645-1 Common Terminology and Functions for Software Distribution and Loading

ARINC645-1 (Current)08/11/2021

This document provides airlines, airframe manufacturers, aircraft equipment suppliers, and others with information that is specific to data, software, and ground tools used in aviation configuration and data management. Which standard to use in specific situations The use of and how integrity checks should be applied Common terminology in airborne software management Since airplanes started using software controlled hardware, there has been a need to standardize processes and terminology. This document is the centroid to which other software standards are related.

Airlines Electronic Engineering Committee

615-4 Airborne Computer High Speed Data Loader

ARINC615-4-ER2 (Current)05/01/2002

This standard provides general and specific guidance for the development of a Portable Data Loader (PDL) for carry-on application and an Airborne Data Loader (ADL) for on-board the airplane. It specifies use of a 3.5 inch floppy disk to upload and download of data and operational programs using an ARINC 429 data bus connected to avionics computers.

Airlines Electronic Engineering Committee, Avionics Maintenance Committee, Flight Simulator Engineering and Maintenance Committee

RS678-AR Amendment Record for Reference Sheet No. RS678

RS678AR-7 (Current)11/23/2021

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

RS678 FASTENERS, ROLLED THREADS, CHAMFERS, LEAD THREADS & RUNOUTS

RS678-7 (Current)11/23/2021

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS2067 Chobert 100° Countersunk Rivet, Steel

AGS2067-7 (Current)06/13/2019

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

800P2-2 Cabin Connectors and Cables, Part 2, Specification of Connectors, Contacts, and Backshells

ARINC800P2-2 (Current)09/09/2021

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

848 Media Independent Secure Offboard Network

ARINC848 (Current)06/19/2020

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

AGS4677AR Amendment Record for Drawing Standard No. AGS4677

AGS4677AR-4 (Current)03/02/2022

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

854 Cabin Equipment Network Bus

ARINC854 (Current)06/19/2020

This standard defines a new cabin network bus. While ARINC Specification 485: Cabin Equipment Interfaces, Part 2, Physical Layer - In-seat Protocol defined a low-speed serial communications interface between electronic equipment in the passenger seat, it is design-focused on obtaining status from in-seat electronic equipment. ARINC Specification 854 is a messaging protocol but does not preclude using the bus for video streaming or multicast. Cabin Equipment has evolved from the very simple to quite sophisticated systems. The resulting communications needs have surpassed the ability of ARINC 485 to provide the necessary data capacity and response times. The basic requirements for low latency, full duplex, elimination of ARINC 485 Master/Slave polling and lower weight drives the selection of 100BASE-T1 (per IEEE 802.3) as the preferred bus format. This document specifies the ARINC 854 Cabin Equipment Network Bus (CENBUS) utilizing a new, serial communications protocol based on IEEE 802.3

Airlines Electronic Engineering Committee

485P2-5 Cabin Equipment Interfaces, Part 2, Physical Layer - In-Seat Protocol

ARINC485P2-5 (Current)06/30/2020

ARINC Specification 485, Part 2 specifies the ARINC 485-control protocol used by the LRUs described in ARINC Specification 628 Part 2. This document defines a multi-drop bus. The point-to-point configuration is also supported. The point-to-point bus is treated simply as a multi-drop bus with only one drop. There is one master LRU and one or more slave LRUs present on the bus. However; multiple buses may be connected in parallel, where each parallel bus operates independently from each other.

Airlines Electronic Engineering Committee

ESC76-AR Amendment Record for Drawing Standard No.ESC76

ESC76AR-5 (Current)03/01/2011

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AS46730 Nut Union - Thrust Wire - Male (Steel)

AS46730-1 (Current)07/01/1980

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AS46732 Thrust Wire - Nut Union, Male (Steel)

AS46732-1 (Current)07/01/1980

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

ESC66 Backshell, Assembly, 90° RFI / EMI Cone Grounding, Anti Decoupling. (MS 3155 Connector Interface MOD)

ESC66-3 (Current)09/01/1991

This drawing specifies parts ESC66-08, ESC66-10, ESC66-12, ESC66-14, ESC66-16, ESC66-18, ESC66-20, ESC66-22, ESC66-24, and ESC66-28. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.

Engine and Airframe Technical Standards Committee (TSC)

ESC76 Backshell Assembly, 90°, RFI / EMI Cone Grounding, 100% Anti-Decoupling

ESC76-5 (Current)03/01/2011

This drawing specifies parts ESC76-08, ESC76-10, ESC76-12, ESC76-14, ESC76-16, ESC76-18, ESC76-20, ESC76-22, ESC76-24, and ESC76-28. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.

Engine and Airframe Technical Standards Committee (TSC)

ESC74 Backshell, Assembly, 45° RFI / EMI Cone Grounding, Anti - Decoupling. (MS 3155 Connector Interface MOD)

ESC74-1 (Current)11/01/1991

This drawing specifies parts ESC74-08, ESC74-10, ESC74-12, ESC74-14, ESC74-16, ESC74-18, ESC74-20, ESC74-22, ESC74-24, and ESC74-28. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.

Engine and Airframe Technical Standards Committee (TSC)

ESC61 Connector Accessory: Outlet Nut

ESC61-2 (Current)05/01/1994

This drawing specifies parts ESC61-10 and ESC61-12. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.

Engine and Airframe Technical Standards Committee (TSC)

AGS1583 BA Washers (Double Spring)

AGS1583-6 (Current)12/03/2015

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1601 Sleeves, Identification, Cable, L.T. Unisheath 4, Cable

AGS1601-4 (Current)12/03/2015

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1596 Ends Cable Claw Type - 0 B.A.

AGS1596-6 (Current)05/16/1958

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1594 Ends - Cable Claw Type - 4 BA

AGS1594-6 (Current)05/16/1958

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1522 Sleeves, Insulating, Cable, L.T. Black and Red

AGS1522-5 (Current)05/07/1963

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1523 Sleeves, Identification, Cable, L.T. Black and Red

AGS1523-8 (Current)05/07/1963

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1518 Thimble for H.T. Cables

AGS1518-7 (Current)01/14/1925

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1606 Tubes, Cable End

AGS1606-8 (Current)02/13/1962

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

AGS1616 Sleeves, Bonding, Metal Braided Cable, H.T. Inner, Straight, Short

AGS1616-7 (Current)02/13/1962

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

Items per page:

1 – 50 of 212784