EUROCAE ED-233 PDF

EUROCAE ED-233 PDF

Name:
EUROCAE ED-233 PDF

Published Date:
06/01/2014

Status:
[ Active ]

Description:

SAFETY AND PERFORMANCE REQUIREMENTS DOCUMENT FOR CDTI ASSISTED VISUAL SEPARATION (CAVS)

Publisher:
European Organization for Civil Aviation Equipment

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

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$64.8
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This document includes the definition of the services and the Environmental Conditions relevant to the implementation of the CAVS application and the operational, safety and performance requirements for using the application.

NOTE: Requirements that provide protection against intentional behaviour causing harm or sabotage are beyond the scope of this document.

NOTE: Requirements related to the recording of ADS-B data for accident or incident investigation purposes are beyond the scope of this document.

PURPOSE OF THE DOCUMENT

This document defines and allocates the set of minimum requirements for the end-toend operational, safety and performance aspects for implementations of the CAVS application. This SPR allocates these requirements to the necessary domains of the CNS/ATM system (i.e. at aircraft and ground domain levels).

These requirements can be used as a component for approval processes including aircraft type design approval, aircraft operator operational approval, and Air Traffic Services (ATS) provider operational approval. This SPR document is also written to support system-specific standards (e.g. MOPS, TSOs, etc.) which will be required for many airspace regulators.

In addition, this document also provides guidance to determine the levels of design assurance and performance that are needed for each element (aircraft, operator, and Air Navigation Service Provider – ANSP) to support the CAVS application.

The CAVS SPR is also envisaged to be used along with those from other surveillance applications based on Automatic Dependent Surveillance-Broadcast (ADS-B) to develop minimum standards for avionic systems to assure that all subsystems perform their intended functions adequately for these applications


Edition : 14
File Size : 1 file , 2.6 MB
Number of Pages : 170
Published : 06/01/2014

History


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