700 Series ARINC Characteristics define digital systems and equipment installed on current-model production aircraft. They include definitions of form, fit, function, and interface for Line Replaceable Units (LRUs) in a federated architecture.
The Advanced FMCS provides expanded functions beyond that defined in ARINC 702 to support the ant...icipated requirements for operation in the CNS/ATM operating environment. GNSS and RNP based navigation, air-to-ground data link for communications and surveillance, and the associated crew interface control/display definitions are included.
This ARINC Standard defines the installation characteristics of first generation L-band satellite... communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included.
This document sets forth the characteristics of the integrated Global Positioning System (GPS)/Gl...obal Orbiting Navigation Satellite System (GLONASS) sensor unit (GNSSU) portion of a GNSS system intended for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GNSS sensors for airline use. It describes the desired operational capability of the GNSS system and the standards necessary to ensure interchangeability.
This document sets forth the characteristics of the GNSS Landing System Sensor Unit (GLSSU) inten...ded for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability.
This document sets forth the characteristics of the Global Navigation Satellite System (GNSS) Lan...ding System Sensor Unit (GLSSU) with a built-in VHF Data Broadcast (VDB) receiver. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability.
This ARINC Standard specifies the ARINC 758 Mark 2 Communications Management Unit (CMU) as an on-...board message router capable of managing various datalink networks and services available to the aircraft. Supplement 4 adds Ethernet interfaces, per ARINC Specification 664 Part 2. This will allow the CMU to communicate with IP based radio transceivers (e.g., L-Band Satellite Communication Systems (Inmarsat SwiftBroadband (SBB) and Iridium Certus), ACARS over IP, AeroMACS, etc.).
This ARINC Standard defines the installation characteristics of second generation L-band satellit...e communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included
This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Avia...tion Satellite Communication (Satcom) System avionics intended for installation in all types of aircraft including commercial transport, business, and general aviation aircraft. The intent of this document is to provide 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.
This document sets forth the desired characteristics of an aviation satellite communication (satc...om) 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.
This standard sets forth the desired characteristics of Aviation Ku-band Satellite Communication ...(Satcom) and Ka-band Satcom Systems intended for installation in all types of commercial air transport aircraft. The intent of this characteristic is to provide guidance on the interfaces, form, fit, and function of the systems. This document also describes the desired operational capability of the equipment needed to provide a broadband transport link that can be used for data, video, and voice communications typically used for passenger communications and/or entertainment. The systems described in this characteristic are not qualified, at this writing, for aviation safety functions.
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.
AEEC, AMC, and FSEMC are aviation industry activities organized by ARINC Industry Activities, an industry program of SAE Industry Technologies Consortia (SAE ITC)®, to establish consensus technical standards, known globally as ARINC Standards, and develop shared technical solutions that no one organization could accomplish independently.