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Airlines Electronic Engineering Committee Interiors, Cabins, and Cockpits Design Engineering and Styling

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Standard

CABIN ARCHITECTURE FOR WIRELESS DISTRIBUTION SYSTEM
2019-08-13
CURRENT
ARINC820
This document defines a secure Wi-Fi distribution network installed in the aircraft passenger cabin for passenger and crew use. Carry-on Portable Electronic Devices (PEDs) such as smart phones, tablets, and laptops may use this network to access public internet services provided on the aircraft.
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

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

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

CABIN COMMUNICATION SYSTEMS (CCS)
2010-11-19
CURRENT
ARINC746-6
This document provides general and specific design guidance for the development, installation, and desired operational capability of Cabin Communications Systems, including satellite communications, air-to-ground communications, and gatelink. Supplement 6 incorporates guidance for protection of personal information using methods consistent with the Payment Card Industry (PCI) Data Security Standard (DSS). The CCS characteristic provides encryption approaches for payment card information and suggestions for key management.
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

AIR TRANSPORT INDICATOR CASES AND MOUNTING
1976-12-15
CURRENT
ARINC408A
This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system. This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system.
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

CABIN STANDARD ENCLOSURES - MODULAR RACK PRINCIPLE (MRP)
2012-06-22
CURRENT
ARINC836
This document provides installation standards for cabin equipment and related mechanical enclosures. It provides provisions for equipment attachment on overhead racks and monuments. The document provides a series of standard volumes and associated masses. Standardized packaging of cabin systems components is expected to yield simpler installation and maintenance of cabin equipment. This is expected to reduce the time and cost related to installing and maintaining cabin systems.
Standard

MARK 5 AIRBORNE DISTANCE MEASURING EQUIPMENT
1988-10-31
CURRENT
ARINC709-8
This standard sets forth characteristics of a DME intended for installation in commercial transport aircraft. It provides slant range distance from an aircraft to a selected DME ground facility, which is presented to the flight crew on an indicator located in the instrument panel. Other applications include utilization of frequency scanning modes by navigation computers.
Standard

PRECISION AIRBORNE DISTANCE MEASURING EQUIPMENT (DME/P)
1994-08-17
CURRENT
ARINC709A-1
This standard provides general and specific design guidance for the development of a DME/P, which provides slant range distance from an aircraft to a selected DME ground facility. For landing purposes, the DME/P complements the angle MLS/ILS with precise range data.
Standard

AIRBORNE PASSENGER ADDRESS AMPLIFIER
1984-07-06
CURRENT
ARINC715-3
This standard describes the characteristics of a PA AMP designed for installation in commercial aircraft. Its function is to amplify control voice, music and internally generated chime audio signals to drive the aircraft cabin loudspeaker system.
Standard

CABIN EQUIPMENT INTERFACES PART 9 CABIN INTERFACE NETWORK (CIN)
2015-11-20
CURRENT
ARINC628P9-4
ARINC 628, Part 9 defines general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin information network related equipment. It specifies a generic on-board infrastructure with commercial server technology, high-speed data communication and exchange via wired and wireless LAN for a wide range of applications. Supplement 4 defines web-based interfaces for cabin control panels and recognizes current standards for commercial browsers and applications. It incorporates current network security practices, including reference to ARINC 842 Digital Certificates.
Standard

CABIN EQUIPMENT INTERFACES PART 4A CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM DAISY CHAIN
2005-02-28
CURRENT
ARINC628P4A-3
Cabin equipment interfaces use a standardized wiring topology defined in Part 4A. This standard defines a standard CDS using a daisy chain wiring topology. This standard defines standard wiring, connectors and installation requirements for a passenger seat network, overhead video network, and cabin management equipment network. Electrical and fiber optic networks are covered.
Standard

CABIN EQUIPMENT INTERFACES PART 2 CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - SEAT INTERFACES
2017-07-10
CURRENT
ARINC628P2-9
This document defines standard electrical and mechanical interfaces of the In-Flight Entertainment System (IFES) equipment associated with the seat (including the headphones, passenger control unit, seat video display, personal video player, telephone hand set, and seat electronics box). Supplement 9 updates applicable interfaces for USB 3.1 outlets in passenger seats.
Standard

CABIN EQUIPMENT INTERFACES PART 4C CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - CABIN DISTRIBUTION SYSTEM - 2ND GENERATION - DAISY CHAIN
2005-09-15
CURRENT
ARINC628P4C
ARINC Specification 628 Part 4 defines standards for the aircraft IFE Cabin Distribution System (CDS) wiring, connectors, power, identification codes, space envelopes and mounting principles. The equipment itself is not a subject of this specification because it may be unique to the system manufacturer or market place driven. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft. The CDS, in daisy chain architecture, is the content of both Parts 4A and 4C of ARINC Specification 628. Part 4C presents the second generation also known as 2GCN of the daisy chain topology, as an evolution based on the experience gained with the first version of the CDS. The main difference is that the system in Part 4C is divided into two separated networks, one for data, connected to the CEC, and the other one for power, connected to the Aircraft Power Supply.
Standard

CABIN EQUIPMENT INTERFACES PART 5 CABIN ELECTRICA EQUIPMENT AND WIRING INSTALLATION GUIDELINES
2013-06-14
CURRENT
ARINC628P5-3
ARINC Specification 628, Cabin Equipment Interfaces (CEI) Part 5 Parts Selection, Wire Design and Installation Guidelines, provides design and mounting guidelines for electrical installations, mainly for supplier of cabin furnishing equipment. Part 5 addresses several aspects of installation and is divided into five sections: Introduction, Parts Selection, Electrical Wire Design Guidelines, Wire Installation Guidelines, and Documentation Guidelines. Guidelines regarding design, safety, and other subjects relevant to acceptance of the end item are addressed. Notes explaining the reason for setting a guideline or suggesting methods for performing the task are provided in commentary. The content of the document is designed to make it usable for reference by industry, particularly manufacturers of seats and equipment.
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