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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.
Standard

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS)
2000-09-15
CURRENT
ARINC762-1
This standard sets forth the characteristics of a terrain awareness and warning system intended for installation in aircraft with digital signal interfaces. Describes the desired operational capability of the equipment, the standards necessary to ensure interchangeability, form factor, and pin assignments.
Standard

TERRAIN AWARENESS AND WARNING SYSTEM ((TAWS) - ANALOG
2001-12-12
CURRENT
ARINC562
Terrain Awareness and Warning System (TAWS)ý Analog addresses the need for standard TAWS installations in older aircraft that have analog equipment interfaces. The analog unit is intended as a replacement for ARINC Characteristic 594: Ground Proximity Warning System (GPWS) equipment. The document is intended to compliment ARINC Characteristic 762: Terrain Awareness and Warning System (TAWS) for later model aircraft having digital equipment interfaces.
Standard

SPECIFICATION CONNECTORS, RACK AND PANEL, RECTANGULA REAR RELEASE CRIMP CONTACTS
2015-06-01
CURRENT
ARINC404B-2
This document defines standardized connectors intended for use on rack-mountable avionics equipment. It is aligned to the latest version of MIL-C-81659. Supplement 2 was updated to support cabin equipment applications. It corrects intermateability control dimensions that are provided for single shell plug connectors.
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

MULTI-PURPOSE CONTROL AND DISPLAY UNIT
1998-12-16
CURRENT
ARINC739A-1
This MCDU standard consists of the original ARINC 739 definition with enhancements to allow it to be logged on to up to two systems at one time. Alternate form factors are included to allow the MCDU to be introduced into a wide variety of airframes candidate for CNS/ATM upgrade.
Standard

INSTALLATION STANDARDS FOR LOW FREQUENCY UNDERWATER LOCATOR BEACON (LF-ULB)
2015-07-15
CURRENT
ARINC677
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.
Standard

HEAD-UP DISPLAY (HUD) SYSTEM
2005-07-08
CURRENT
ARINC764
This document defines a Head-Up Display (HUD) system intended for installation in all types of aircraft. It describes the physical form factors, fit dimensions, electrical interface definition and typical HUD functions, including the display of navigation and guidance information in the flight crew's forward field of view. The HUD accomplishes this by projecting images onto a combiner with symbology that conforms to the outside world view. Guidance for HUD architectures include single, twin, dual and HUD integrated with Primary Flight Display (PFD). This document is an practical guide for the design of federated equipment and integrated modular avionics.
Standard

GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS
1999-02-15
CURRENT
ARINC610A-1
This standard preserves all of the technical concepts of ARINC 610. ARINC 610A encompasses the lessons learned since ARINC 610 was issued, provides additional information defining each simulator function and the responses required by each type, and creates guidance information relevant to Integrated Modular Avionics (IMA).
Standard

GUIDANCE FOR DESIGN AND INTEGATION AND AIRCRAFT AVIONICS EQUIPMENT IN SIMULATORS
1992-02-01
CURRENT
ARINC610-1
This standard sets forth general philosophy and design guidance for using aircraft avionics equipment in simulators. Its goal is to improve simulator training by providing a better understanding among avionics designers, simulator designers, airframe manufacturers and airline simulator users in the use of aircraft avionic equipment in flight simulators. Full flight simulator, cockpit procedure trainer, cockpit system simulator or fixed base simulator, part task trainer (e.g., flight management system trainer), and maintenance training simulator guidance is included.
Standard

GROUND PROXIMITY WARNING SYSTEM
1988-01-11
CURRENT
ARINC723-3
This standard sets forth the characteristics of a GPWS designed for installation in commercial aircraft. It aids pilots by providing audible and visible warnings or alerts when an aircraft approaches terrain more closely than, or deviates downward from an ILS glide slope beyond the limits set into the system.
Standard

FIBER OPTIC TRAINING REQUIREMENTS
2019-01-10
CURRENT
ARINC807-4
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
Standard

FIBER OPTIC TRAINING REQUIREMENTS
2013-06-26
CURRENT
ARINC807-3
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807, addressing fiber optic training requirements, is a scaled back version of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
Standard

EMBEDDED INTERCHANGE FORMAT FOR TERRAIN DATABASES
2018-12-21
CURRENT
ARINC813
This document defines an open encoding format for terrain databases. This format, when designed and implemented, will enable a quick, economic, and efficient use of Terrain Databases (TerrDBs). However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Standard

DESIGN GUIDELINES FOR AIRCRAFT CABIN HUMAN MACHINE INTERFACES
2011-06-01
CURRENT
ARINC837
This document provides guidance for standard cabin systems control panel Graphical User Interfaces (GUI) intended to improve the human-machine interface. The document defines control and indication elements for various cabin functions, including cabin lighting, cabin temperature, door status, and the like. Standardization of cabin system interfaces will enable airlines to have consistent cabin operations across their fleets and reduce cabin crew training costs.
Standard

DEFINITION OF STANDARD INTERFACES FOR GALLEY INSERT (GAIN) EQUIPMENT PHYSICAL INTERFACES
2015-11-23
CURRENT
ARINC810-5
ARINC 810 defines galley equipment physical attachments, envelopes, connections, and qualification guidelines for interchangeable galley equipment. Supplement 5 defines a size 6 galley insert, intended for microwave oven installation and other equipment suited to this type of installation. Supplement 5 also clarifies reference dimensioning for all GAIN sizes defined by ARINC 810.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS PART 1 AVIONICS INTERFACES, BASIC SYMBOLOGY, AND BEHAVIOR
2019-06-17
CURRENT
ARINC661P1-7
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 7 adds the definition of: Selector Widget, Tree Widget, New FormatString options, Readouts available in MapItems, Provisions for Touch Screen Displays.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS PART 1 AVIONICS INTERFACES, BASIC SYMBOLOGY, AND BEHAVIOR
2020-09-18
CURRENT
ARINC661P1-8
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 8 adds numerous changes and additions. Eleven new widgets are added, all related to 3D Maps. Seven new widget extensions. Metadata definitions (XML) for all widgets, extensions, events, symbols, and associated data types.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS
2016-09-01
CURRENT
ARINC661-6
ARINC 661 defines necessary interfaces to Cockpit Display Systems (CDS) used in all types of aircraft installations starting with the Airbus A380 airplane. 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 interfaces between the CDS and the aircraft systems. This includes 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.
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