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Description / Abstract:
PURPOSE AND SCOPE
The fundamental airborne flight recorder regulatory framework
developed in the late 1950's and early 1960's addressed voice based
communications to and from aircraft, consistent with the technology
of the time. The Communications, Navigation, Surveillance (CNS) and
Air Traffic Management (ATM) concepts, endorsed by ICAO, rely
extensively on new technology which replaces many of these
communications with digital messages. CNS/ATM operations have
already become and will continue to be more dependent upon these
digital communications. The accident investigation community
believes that the fundamental recording requirements have not
substantially changed, but that the regulatory framework needs to
be revisited in light of new technology and concepts introduced
with CNS/ATM. In particular, the replacement of traditional voice
messages with digital messaging technology creates a need to
consider new systems to ensure that the information necessary for
incident and accident investigation continues to be recorded
on-board the aircraft.
The ICAO FLIREC PANEL which convened in 1993, recommended
that;
"All aeroplanes equipped to utilise digital ATS communications
and required to carry a cockpit voice recorder shall record the
digital communications messages on the cockpit voice recorder."
This document contains minimum aviation system performance
specifications for Communication, Navigation, Surveillance, Air
Traffic Management (CNS/ATM) Message Recording System. They specify
characteristics that should be useful as guidance material to
regulatory authorities, designers, installers, manufacturers,
service providers and users of systems intended for operational.
Where systems are global in nature, the system may have
international applications which are taken into consideration.
Compliance with these specifications is recommended as one means
of assuring that the system and each subsystem will perform its
intended function(s) satisfactorily under conditions normally
encountered in routine aeronautical operations for the environments
intended. The MASPS may be implemented by one or more regulatory
documents and/or advisory documents (for example certifications,
authorisations, approvals, commissioning, advisory circulars,
notices) and may be implemented in part or in total. Any regulatory
application of this document is the sole responsibility of
appropriate governmental authorities.
While this MASPS does not specify where the information is to be
recorded on board the aircraft, there may be advantages to adapting
Cockpit Voice Recorders to handle many of these requirements.
However, for some information, such as navigation parameters, it
may be better to use the Flight Data Recorder. This MASPS does not
preclude the development of new architecture recorders.
Chapter 1 of this document describes the CNS/ATM Message
Recording System and provides information helpful to understand the
rationale for the system characteristics and requirements. This
chapter describes typical applications, operational goals and
establishes the basis for the specifications developed in Chapters
2 through 4 of the document. Definitions and assumptions essential
to a proper understanding of this document are also provided in
this chapter.
Chapter 2 describes the overall CNS/ATM system architecture.
Chapter 3 contains the minimum performance specifications for
each subsystem/function that is a required element of minimum
system performance in Chapter 2. These standards specify the
required performance under the standard environmental conditions
described.
Chapter 4 describes the minimum system test procedures to verify
system performance compliance (for example end-to-end performance
verification) and that subsystem performance meets the minimum
performance requirements in Chapters 2 and 3.
Chapter 5 links the contents of the previous four chapters to
future equipment performance specifications. These new documents
will define airborne and ground recorder requirements for CNS/ATM
technology.
The word "subsystem" as used in this document includes all
components that make up a major independent, necessary and
essential functional part of the system so that the system can
properly perform its intended function(s). The guidelines contained
in the latest version of EUROCAE ED-12/RTCA DO-178 should be
considered, even for non-airborne applications, for systems and
subsystems containing software.