The guardREC® solution complies with the EUROCAE ED to assist the The Functional specifications for CNS/ATM Recording (ED) is a set of. Std EUROCAE ED Functional specifications for CNS/ATM Recording – Including Amendment N°1. Context. Related Elements. Std EUROCAE ED EUROCAE and RTCA documents should be listed in an EUROCAE ED Safety and Performance Standard for Baseline 2 ATS Data. Communications (Baseline 2 Page

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Crash safety specifications, e. This document can also be used to give guidance to manufacturers intending to develop or install lightweight flight recording systems which maybe used for or other purposes such as flight training, flight data monitoring.


Level 1 through Level 5 transponders are addressed, test procedures are provided as well as information for optional features. Existing safety processes have not had to consider intentional disruption. The requirements contained in this document provide assurance that a VDL Mode 4 system will perform the intended function in an acceptably safe manner for the operations defined in the OSEDs for the various applications.

The following parts provide an overview about the deliverables WG has produced as individual reports, and how they can be used for standardisation of future services. It discusses those aspects of airworthiness certification that pertain to the production of software, using formal methods for systems approved using EDC.

ED – Audio systems characteristics and MPS covering microphones except carbon and headsets and handsets and loudspeakers and audio selector panels and amplifiers Issued in July Issued in October Aircraft equipped with ACAS X have the ability to interrogate airborne transponders and receive ADS-B Messages to determine the location of other aircraft in the vicinity and assess the risk of collision. This document is intended to capture minimum interoperability, performance and safety requirements for a service based on data-link communications used for Departure Clearance.

In addition, this example shows the interrelationships with ARP This Technical Specification document specifies the minimum performance requirements for a Wide Area Multilateration WAM System that is part of a system providing airspace situational awareness to air traffic controllers and other users within the European Air Navigation Region.

Change 2 to ED A full service description encompasses a logical service design, which is technology agnostic and transfers the operational information requirements into a description of the SWIM service on a conceptual level and a description of the technical service design. The purpose and scope section concentrates on introducing the technology and describes the process for the AeroMACS profile development.


This document provides a specification for the minimum performance requirements of a system to provide the flight crew with a view of the area outside the flight deck door. Change 1 to EDA. It provides standards for Mode S airborne equipment Mode S. The document includes 26 Sections and three Appendices.

Radio – Volume 2: This document provides guidance to be used by aircraft manufacturers and suppliers of electronic hardware items used in aircraft systems. Abbreviations and Terminology for Unmanned Aircraft Systems. No longer maintained Issued in April Equivalence between this form of the CAS logic and the state charts has been demonstrated by testing implementations based on each specification against the CAS test suite.

It specifies system and equipment characteristics that should be used by designers, installers, manufacturers, service providers and users of systems intended for operational use at aerodromes.

It provides practices for showing compliance with the regulations and serves to assist a company in developing and meeting its durocae internal standards by considering the guidelines herein. Issued in August However, in the avionics industry, it brings specific challenges as systems are complex, hardware heterogeneous and coming from multiple suppliers with different infrastructures.

Network Design Guideline Issued in February This document discusses the role of airborne collision avoidance from other traffic. The report addresses coordination processes leading towards safety, performance and interoperability assessment, with an eventual aim to support also airworthiness certification and operational approval.

Guidance has to be developed for equipment EMC qualification, aircraft system level verification, wiring installation and aircraft level EMC verification. The Sections and Tables affected are provided. Airport CDM also addresses the need for operational decisions to be edd-111 collaboratively thus providing a ev-111 contribution to maximising capacity and efficiency.

Based on the availability of standardized current AMDBs, a variety of applications can be envisioned. In this section various glossary terms used in the document are described. It provides the interoperability requirements standard for the initial implementation of the Aeronautical Telecommunications network ATNwhich supports several Air Traffic Services.

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EDG is complemented by ED This document expands the previously defined DOA intended function of an SVS beyond that of supplemental view of the external scene to include enhanced aircraft attitude and energy state awareness. This feasibility study document details the context of the study and a description of the intended function situational display of regions ahead of the aircraft that present potential hazards to the aircraft due to ice crystals.


Second generation homing specifications sd-111. This document defines the minimum specification to be met for all aircraft required to carry flight recorders which may record flight data; cockpit audio; images and data link digital messages; in a crash survivable recording medium ehrocae the purposes of the investigation of an occurrence accident or incident. This includes validation of requirements and verification of the design implementation for certification and product assurance.

No longer maintained Issued in January European Legacy Telephone Interworking – Volume 4: This document provides to the aviation community a collection of disciplines necessary to assure that the aeronautical information used by the community meets the standards of quality and integrity appropriate for a safe flight. The purpose of this document is to identify the unique safety criteria for the ed1-11 of fuel cell systems into aircraft. Rather, it is an approach to using aeronautical data, based on sharing data between all Partners, ensuring a common view of the ATM and airport environment on all levels.

This document provides general information on aicraft surface p-static charging mechanisms and the impact p-static has euurocae aircraft systems. ACAS X is intended to improve air safety by acting as a last-resort method of preventing mid-air collisions or near mid-air collisions NMAC between aircraft. This minimum operational performance specification is for aircraft Air Data Modules ADM that measure static or total pressure.

ED consists of two Volumes plus supplementary material: This document specifies system and equipment characteristics that should be useful to designers, installers, manufacturers, service providers and users of systems intended for operational use at aerodromes.

Objectives, activities, explanatory text and software life cycle data that should be addressed when model-based development and verification are used as part of the software life cycle.

This documents complements EDA.