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Standard

USERS GUIDE FOR ARINC 616 AVIONICS SUBSET OF ATLAS
2017-11-29
CURRENT
ARINC605
This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).
Standard

STANDARD ATLAS LANGUAGE FOR MODULAR TEST
1995-01-30
CURRENT
ARINC626-3
This standard defines an airline-recommended subset of the Abbreviated Test Language for All Systems (ATLAS)intended to be used in conjunction with test systems that are compliant with ARINC 608A. ATLAS is a standard abbreviated English language used in preparation and documentation of test procedures that can be implemented with automatic or semiautomatic test equipment.
Standard

PROGRAMMERS GUIDE FOR SMART SYSTEMS USING ARINC 626 ATLAS
2002-06-30
CURRENT
ARINC627-2
This standard provides guidance to ATLAS test programmers for developing, writing and documenting test programs in ARINC 626 ATLAS. This is a companion standard to ARINC 608A, Design Guidance for Avionics Test Equipment. It provides guidance to managers and system integrators for standardizing test programs and their documentation.
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
1996-03-01
CURRENT
ARINC732-1
This standard defines an airborne tape reproducer for passenger entertainment. The function of this equipment is to play pre-recorded tapes to the passengers through the airplane passenger entertainment system. Some channels may be used for boarding music through the public address system.
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
1993-01-01
CURRENT
ARINC735-2
This standard defines as TCAS system capable of calculating the range, altitude and bearing of other aircraft equipped with Mode S transponders. The system monitors the trajectory of these aircraft for the purpose of determining if any of them constitute a potential collision hazard.
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
1988-04-01
CURRENT
ARINC737-1
This standard defines a system of sensors and monitoring equipment to determine aircraft weight while it is on the ground. The system serves as an aid to the pilot for determining aircraft weight distribution and center of gravity (CG).
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
2001-07-01
CURRENT
ARINC738-3
This standard defines an integrated ADIRS that provides air data information and directional guidance information for cockpit display. The ADIRS consists of up to three Air Data/Inertial Reference Units (ADIRUs) located in the aircraft electronic rack, an associated Control and Display Unit (CDU) and remotely mounted Air Data Modules (ADMs).
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
2015-08-01
CURRENT
ARINC735B-2
This document defines a Traffic Surveillance capability for NextGen and SESAR airspace environments. Supplement 2 adds hybrid surveillance functionality. It satisfies recent updates to FAA Airworthiness Circular AC 20-151B - Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II), and Technical Standard Order TSO-119d requiring the annunciation of a hybrid surveillance failure. Supplement 2 also adds strobe program pinning, updates TCAS inputs status, improves aircraft troubleshooting, and supports recent central maintenance computer function block point updates.
Standard

GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS
1999-01-25
CURRENT
ARINC611-1
This standard defines accuracy and reliability targets for fuel quantity measuring systems installed on commercial aircraft. It describes fuel quantity system components and design techniques that will contribute to safe and reliable operation. System design goals and installation practices are described. A report of a worldwide fuel survey is included.
Standard

GUIDANCE FOR STANDARD SUBDIVISION OF ATA SPEC. 100 FOR NUMBERING SYSTEM FOR AVIONICS
1971-10-06
CURRENT
ARINC421
This guidance standard was prepared in response to a need stated by air transport operators for uniformity in further subdividing the ATA Spec. 100 number system to better accommodate avionics systems. The ATA numbers are widely used in the maintenance community for inventory control, instruction manuals and equipment modification Service Bulletins.
Standard

FIBER OPTIC TEST PROCEDURES
2019-01-28
CURRENT
ARINC805-5
This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft. This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft.
Standard

FIBER OPTIC TEST PROCEDURES
2014-01-06
CURRENT
ARINC805-4
This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft.
Standard

EMBEDDED INTERCHANGE FORMAT FOR AIRPORT MAPPING DATABASE
2007-11-19
CURRENT
ARINC816-1
This document defines an open encoding format for airport databases which are loaded in airborne systems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Standard

EMBEDDED INTERCHANGE FORMAT FOR AIRPORT MAPPING DATABASE
2016-08-31
CURRENT
ARINC816-3
This document defines an open encoding format for airport databases which are loaded in airborne systems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Standard

DESIGN GUIDANCE FOR AVIONICS TEST EQUIPMENT
1993-01-15
CURRENT
ARINC608A
This standard is a top-level guidance standard intended for the design of Automatic Test Equipment (ATE). It includes the definition of hardware and software needed for analog and digital signal testing using a Test Unit Adapter common interface. This standard describes the overall ATE system concept as well as the definition of the specific elements of those systems.
Standard

CABIN PASSENGER SEAT PRODUCTION TESTING
2019-12-18
CURRENT
ARINC648
This report defines the requirements and recommended practices for production testing of aircraft passenger seats and seat groups. Production testing is performed at the seat manufacturers' facilities prior to the shipment of the seats to the airframe manufacturers, Maintenance, Repair, and Overhaul (MRO), or airlines/operators for installation in the aircraft. Using this guidance, rework is minimized and schedules remain minimally affected.
Standard

CABIN CONNECTORS AND CABLES, PART 4, STANDARD TEST METHODOLOGY
2020-07-13
CURRENT
ARINC800P4-1
ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed (Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.
Standard

CABIN CONNECTORS AND CABLES PART 4 STANDARD TET METHODOLOGY
2015-12-01
CURRENT
ARINC800P4
ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed (Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.
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