Search Results

Standard

MARK 3 AVIATION SATELLITE COMMUNICATION SYSTEMS

2017-08-09

CURRENT

ARINC781-7

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. The intent of this document is to provide 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 is specified in ARINC Characteristic 791.

Standard

CABIN CONNECTORS AND CABLES, PART 2, SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS

2014-10-07

CURRENT

ARINC800P2

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.

Standard

MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM PART 2 ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION

2014-07-28

CURRENT

ARINC791P2-1

This document provides the 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 ARINC 791 Satcom system, and in particular, between the Modman and the Antenna Subsystem, are described to permit interchangeability between any Modman and any Antenna Subsystem.

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.

Standard

ELECTRONIC FLIGHT INSTRUMENTS (EFI)

2013-06-01

CURRENT

ARINC725-2

This standard sets forth the features of a color EFI system for installation in commercial transport aircraft. The EFI provides display functions that include Attitude Director Indicator (ADI), Horizontal Situation Indicator (HSI), Air Data, Map display, Weather display, Radio Altitude data, Flight Control Mode annunciation, Flight Path information, and Flight Warning display.

Standard

FIBER OPTIC CONNECTORS

2013-06-06

CURRENT

ARINC801-3

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

FLIGHT WARNING COMPUTER SYSTEM

1981-09-10

CURRENT

ARINC726-1

This standard sets forth the characteristics of a FWCS intended for use in commercial transport aircraft. It is intended to process caution and warning inputs for visual and/or audible presentation to the flight crew.

Standard

AVIONICS REFRIGERATION COOLING SYSTEM

2017-10-27

CURRENT

ARINC728

This standard provides standards for the in accordance with which aircraft operators and manufacturers can order avionics refrigeration units and can design installations for an ARCS.

Standard

AIRBORNE MICROWAVE LANDING SYSTEM

1987-08-27

CURRENT

ARINC727-1

This standard sets forth the characteristics of MLS receiver processors intended for installation in all types of commercial transport aircraft. The function of the airborne MLS receiver processor is the reception and processing of the MLS azimuth signals, the elevation signals, and the data transmitted from the MLS ground stations.

Standard

ELECTRONIC CHRONOMETER

1998-11-30

CURRENT

ARINC731-3

This standard sets forth the characteristics for a self-contained Electronic Chronometer for installation in all types of commercial transport aircraft. It provides the following indications to the flight crew, Time of Day, Day and Month, Elapsed Time and Chronograph.

Standard

ANALOG AND DISCRETE DATA CONVERTER SYSTEM

1981-09-10

CURRENT

ARINC729-1

This standard sets forth the characteristics of an ADDCS designed for installation in commercial transport aircraft. The ADDCS is intended to process, convert and multiplex analog and discrete signals in order to provide them in digital format described in ARINC 429.

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

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

MULTI-PURPOSE CONTROL AND DISPLAY UNIT

1990-06-20

CURRENT

ARINC739-1

MCDU consists of an alphanumeric keyboard and display unit capable of interfacing with a number of aircraft systems. Dedicated keys on the MCDU provide the means for system selection with programmable soft keys. ARINC 429 interfaces are used to communicate with participating systems.

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

AIR DATA AND INERTIAL REFERENCE SYSTEM (ADIRS)

2001-07-31

CURRENT

ARINC738A-1

This standard sets forth characteristics for a 4 MCU integrated digital ADIRS intended for installation in subsonic commercial transport aircraft. It is envisioned that the ADIRS will incorporate the capabilities of both an air data system and an inertial reference system.

Standard

MULTIPLE-INPUT COCKPIT PRINTER

1998-06-01

CURRENT

ARINC740-1

This standard describes the form, fit, function and interfaces of an airborne printer capable of communicating with multiple systems one at a time. The printer contains the circuitry for acquisition, buffering and processing of coded alphanumeric messages for print-out on half-width paper.

Standard

AIRBORNE GLOBAL POSITIONING SYSTEM RECEIVER

1990-03-01

CURRENT

ARINC743

This standard provides design guidance for the development of GPS sensors for airline use. It describes the operational capability of the GPS receiver and the standards necessary to ensure interchangeability. GPS provides navigation data to pilots and provides data for use by other aircraft systems.

Standard

AVIATION SATELLITE COMMUNICATION SYSTEM PART 2 SYSTEM DESIGN AND EQUIPMENT FUNCTIONAL DESCRIPTION

2012-06-27

CURRENT

ARINC741P2-11

This document describes the desired operational capability of the equipment as configured with the first generation Satellite Data Unit (SDU) to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. Supplement 11 adds commentary on the commonality of physical interfaces between ARINC 741 systems defined for SwiftBroadband safety services and ARINC 741 systems defined only for the Inmarsat Classic Aero safety services. It adds the SwiftBroadband safety services to the SDU functional definition.

Standard

WINDSHEAR WARNING AND GUIDANCE SYSTEM

1988-01-27

CURRENT

ARINC742

This standard describes stand-alone windshear warning system comprised of a windshear warning computer and associated cockpit displays. The system uses data pertaining to aircraft movement with respect to air movement to detect and annunciate a windshear condition. As an option, it may also provide instrument guidance to the crew indicating optimum pitch to endure the windshear encounter.