ARINC SPECIFICATION 828-4-2015 PDF
Name in English:
St ARINC SPECIFICATION 828-4-2015
Name in Russian:
Ст ARINC SPECIFICATION 828-4-2015
Original standard ARINC SPECIFICATION 828-4-2015 in PDF full version. Additional info + preview on request
Full title and description
St ARINC SPECIFICATION 828-4-2015 — ARINC 828-4:2015: "Electronic Flight Bag (EFB) Standard Interface". This specification defines a common aircraft-mounted interface, connector provisions and data/power/service definitions to support installation and operation of Electronic Flight Bags (EFBs) for both forward-fit and retrofit applications.
Abstract
ARINC 828-4:2015 specifies the electrical, mechanical and logical interface requirements for Electronic Flight Bag (EFB) installations. It standardizes connector types and pin assignments, aircraft data interface services and parameters, power and Ethernet provisions introduced in Supplement 4, and includes appendices covering example wiring, connector termination, use cases and environmental test guidance for EFB equipment.
General information
- Status: Current / Active.
- Publication date: December 11, 2015 (2015-12-11).
- Publisher: Aeronautical Radio, Inc. (ARINC) / AEEC / SAE-ITC distribution.
- ICS / categories: 49 — Aircraft and space vehicle engineering (avionics, aircraft interfaces).
- Edition / version: ARINC 828, Supplement 4 (designated ARINC 828-4), 2015 edition.
- Number of pages: 163 pages (full specification).
Scope
Defines a common EFB aircraft interface covering connector form/fit, power provisioning, standardized signaling and a reference plane for interfacing EFB hardware classes to aircraft systems. The document addresses aircraft data interface services and parameters, common EFB connector pin requirements and provides multiple appendices with example wiring, mounting provisions and environmental test examples. Supplement 4 specifically adds two new connectors to provide power and Ethernet to EFB installations to reduce footprint and weight.
Key topics and requirements
- Standardized EFB connector definitions, pin assignments and cross‑wiring guidance (including alternate connector options).
- Aircraft data interface services and parameter definitions to support common EFB applications (discretes, serial buses, Ethernet, USB, video interfaces, etc.).
- Power provisioning and power-supply signaling for EFBs (including provisions introduced in Supplement 4).
- Reference plane, signaling levels, connector termination and example wire types.
- Appendices with example use cases, mounting/space provisions, environmental test examples and connector termination methods.
Typical use and users
Used by aircraft manufacturers (airframers), airlines, EFB hardware and accessory manufacturers, installation/retrofit contractors, avionics systems engineers and certification authorities. It is referenced during design and installation of cockpit EFB provisions, electrical harness design, avionics integration and for ensuring interoperability of EFB applications with aircraft systems.
Related standards
Related ARINC and regulatory documents commonly used alongside ARINC 828-4 include ARINC 840 (EFB Application Control Interface), ARINC 821 (Aircraft Network Server System), ARINC 834 (Aircraft Data Interface Function / ADIF), ARINC 429 (avionics data bus), and FAA guidance such as FAA AC 120-76 on EFB authorization. The specification itself is cited by and cross-references multiple ARINC standards and FAA guidance.
Keywords
Electronic Flight Bag (EFB), EFB interface, ARINC 828-4, connectors, MIL‑DTL‑38999, power provisioning, Ethernet, aircraft data interface, pin assignments, avionics integration, EFB retrofit.
FAQ
Q: What is this standard?
A: ARINC 828-4:2015 is the ARINC specification that defines the standard aircraft interface and installation provisions for Electronic Flight Bags (EFBs), including connector definitions, power and data services, and related installation guidance.
Q: What does it cover?
A: It covers connector form/fit and pin assignments, standardized signaling, power supply requirements, aircraft data interface services and parameters, and appendices with wiring, termination, mounting and environmental test examples. Supplement 4 adds two connectors providing power and Ethernet to support smaller/lighter EFB installations.
Q: Who typically uses it?
A: Airframers, airlines, EFB and avionics OEMs, installation/retrofit teams, systems engineers and certification/regulatory personnel use it for design, integration and approval of EFB installations.
Q: Is it current or superseded?
A: As published on December 11, 2015, ARINC 828-4 is listed as the current/active edition in standards catalogues. Users should verify with the ARINC/AEEC (SAE/Industry channels) or the publisher before using it for critical certification work to confirm no later supplements or revisions have been released.
Q: Is it part of a series?
A: Yes — ARINC 828 is a family of documents addressing EFB interfaces; 828-4 represents the Supplement 4 / 2015 edition within that ARINC 828 series of specifications and updates.
Q: What are the key keywords?
A: Electronic Flight Bag (EFB), EFB interface, connectors, power, Ethernet, pin assignments, avionics interface, ARINC 828, MIL‑DTL‑38999, retrofit.