RTCA,
Incorporated
Phone:
202-833-9339
Fax:
202-833-9434
List of Available Documents
March 2011
New in this Edition
Change 1 to DO-306, Safety and Performance Standard for Air Traffic Data
Link Services in Oceanic and Remote Airspace (Oceanic SPR Standard)
DO-181E, Minimum Operational Performance Standards for Air Traffic Control Radar
Beacon System/Mode Select (ATCRBS/Mode S) Airborne Equipment
FOREWORD
RTCA,
Incorporated is a not-for-profit corporation formed to
advance the art and science of aviation and aviation electronic systems for the
benefit of the public. The organization functions as a Federal Advisory
Committee and develops consensus based recommendations on contemporary aviation
issues. RTCA’s objectives include but are not limited to:
·
Coalescing aviation system user and
provider technical requirements in a manner that helps government and industry
meet their mutual objectives and responsibilities;
·
Analyzing and recommending solutions
to the system technical issues that aviation faces as it continues to pursue
increased safety, system capacity and efficiency;
·
Developing consensus on the
application of pertinent technology to fulfill user and provider requirements,
including development of minimum operational performance standards for
electronic systems and equipment that support aviation; and
·
Assisting in developing the
appropriate technical material upon which positions for the International Civil
Aviation Organization and the International Telecommunication Union and other
appropriate international organizations can be based.
The organizations’ recommendations are often
used as the basis for government and private sector decisions as well as the
foundation for many Federal Aviation Administration Technical Standard Orders.
Since RTCA is not an official agency of the
United States Government, its recommendations may not be regarded as statements
of official government policy unless so enunciated by the
List of
Available Documents
This catalog lists RTCA documents that are currently
available for sale.
Publication
Formats
All new RTCA documents are produced and distributed electronically via
the RTCA website. Contact RTCA for pricing and availability information
regarding paper copies of RTCA documents.
Index
to RTCA Documents
March 2011
PROCEEDINGS
OF ANNUAL SYMPOSIA
_______________________________________________________
·
DO-326, Airworthiness
Security Process Specification
·
DO-322, Safety,
Performance and Interoperability Requirements Document for ATSA-SURF
Application
·
DO-320, Operational
Services and Environmental Definition (OSED) for Unmanned Aircraft Systems
·
DO-311, Minimum
Operational Performance Standards for Rechargeable Lithium Battery Systems
·
DO-307, Aircraft
Design and Certification for Portable Electronic Device (PED) Tolerance
·
DO-304, Guidance
Material and Considerations for Unmanned Aircraft Systems
·
DO-302, Minimum
Operational Performance Standards (MOPS) for Surveillance Transmit Processing
(STP)
·
DO-299, Report -
Assessment and Recommendations on Visual Alerts and Aural Annunciations for
TCAS II
·
DO-298, Safety
Analysis of Proposed Change to TCAS RA Reversal Logic
·
DO-297, Integrated
Modular Avionics (IMA) Development Guidance and Certification Considerations
·
DO-296, Safety
Requirements for Aeronautical Operational Control (AOC) Datalink Messages
·
DO-295, Civil
Operators’ Training Guidelines for Integrated Night Vision Imaging System
Equipment
·
DO-294C, Guidance on
Allowing Transmitting Portable Electronic Devices (T-PEDs) on Aircraft
·
DO-292, Assessment of
Radio Frequency Interference Relevant to the GNSS L5/E5A Frequency Band
·
DO-291A, Interchange
Standards for Terrain, Obstacle, and Aerodrome Mapping Data
·
DO-285, Next
Generation Air/Ground Communications (NEXCOM) VDL Mode 3 Interoperability
·
DO-280B,
Interoperability Requirements Standard For ATN Baseline 1 (INTEROP ATN B1)
·
DO-279, Next
Generation Air/Ground Communications (NEXCOM) Principles of Operation VDL Mode 3
·
DO-276A, User
Requirements for Terrain and Obstacle Data
·
DO-274, Next
Generation Air/Ground Communications (NEXCOM) Principles of Operation
·
DO-273, Response to
the Report of the RTCA Chairman’s Committee on NEXCOM
·
DO-272B, User
Requirements for Aerodrome Mapping Information
·
DO-268, Concept of
Operations, Night Vision Imaging System for Civil Operators
·
DO-266, Government
and Industry Guidelines and Concepts for NAS Analysis and Redesign
·
DO-263, Application
of Airborne Conflict Management: Detection, Prevention, & Resolution
·
DO-261, NAVSTAR GPS
L5 Signal Specification
·
DO-258A,
Interoperability Requirements for ATS Applications Using ARINC 622 Data Communications
·
DO-255, Requirements
Specification for Avionics Computer Resource (ACR)
·
DO-254, Design
Assurance Guidance for Airborne Electronic Hardware
·
DO-252, Minimum
Interoperability Standards (MIS) for Automated Meteorological Transmission
(AUTOMET)
·
DO-245A, Minimum
Aviation System Performance Standards for Local Area Augmentation System (LAAS)
·
DO-244,
Government/Industry Guidelines and Concept for National Airspace Analysis and
Redesign
·
DO-243, Guidance for
Initial Implementation of Cockpit Display of Traffic Information
·
DO-238, Human
Engineering Guidance for Data Link Systems
·
DO-237, Aeronautical
Spectrum Planning for 1997- 2010
·
DO-235B, Assessment
of Radio Frequency Interference Relevant to the GNSS L1 Frequency Band
·
DO-234, Minimum
Performance and Installation Standards for Runway Guard Lights (RGLs)
·
DO-233, Portable
Electronic Devices Carried on Board Aircraft
·
DO-232, Operations
Concepts for Data Link Applications of Flight Information Services
·
DO-230B, Integrated
Security System Standard for Airport Access Control
·
DO-230A, Standards
for Airport Security Access Control Systems
·
GEO Bias Modeling
Tool for DO-229D
·
DO-227, Minimum
Operational Performance Standards for Lithium Batteries
·
DO-223, Minimum
Operational Performance Standards for Context Management (CM) Equipment
·
DO-222, Guidelines on
AMS(R)S Near-Term Voice Implementation and Utilization
·
DO-221, Guidance and
Recommended Requirements for Airport Surface Movement Sensors
·
DO-219, Minimum
Operational Performance Standards for ATC Two-Way Data Link Communications
·
DO-218B, Minimum
Operational Performance Standards for the Mode S Airborne Data Link Processor
·
DO-216, Minimum
General Specification for Ground-Based Electronic Equipment
·
DO-215A, Guidance on
Aeronautical Mobile Satellite Service (AMSS) End-to-End System Performance
·
DO-213, Minimum
Operational Performance Standards for Nose-Mounted Radomes
·
DO-204A, Minimum
Operational Performance Standards for 406 MHz Emergency Locator Transmitters
(ELT)
·
DO-201A, Standards
for Aeronautical Information
·
DO-200A, Standards
for Processing Aeronautical Data
·
DO-199, Potential
Interference to Aircraft Electronic Equipment from Devices Carried Aboard
·
DO-191, Minimum
Operational Performance Standards for Airborne Thunderstorm Detection Equipment
·
DO-188, Emergency
Locator Transmitter (ELT) Batteries Guidance and Recommendations
·
DO-186B, Minimum
Operational Performance Standards for Airborne Radio Communications Equipment.
·
DO-184, Traffic Alert
and Collision Avoidance System (TCAS) I Functional Guidelines
·
DO-182, Emergency
Locator Transmitter (ELT) Equipment Installation and Performance
·
DO-179, Minimum
Operational Performance Standards for Automatic Direction Finding (ADF)
Equipment
·
DO-178B, Software
Considerations in Airborne Systems and Equipment Certification
·
DO-176, FM Broadcast
Interference Related to Airborne ILS, VOR and VHF Communications
·
DO-169, VHF
Air-Ground Communication Technology and Spectrum Utilization
·
DO-167, Airborne
Electronics and Electrical Equipment Reliability
·
DO-166, Microwave
Landing System (MLS) Implementation
·
DO-165, Initial
Report on Civil Aviation Frequency Spectrum Requirements-1980- 2000
·
DO-164A, Minimum
Performance Standards-Airborne Omega Receiving Equipment
·
DO-162, Report on
Air-Ground Communications-Operational Considerations for 1980 and Beyond
·
DO-161A, Minimum
Performance Standards-Airborne Ground Proximity Warning Equipment
·
DO-160G,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160F,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160E,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160D,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160C,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160B,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-160A,
Environmental Conditions and Test Procedures for Airborne Equipment
·
DO-158, Minimum
Performance Standards-Airborne Doppler Radar Navigation Equipment
·
DO-155, Minimum
Performance Standards-Airborne Low-Range Radar Altimeters
·
DO-148, A New
Guidance System for Approach and Landing
·
DO-144A, Minimum
Operational Characteristics-Airborne ATC Transponder Systems
·
DO-143, Minimum
Performance Standards-Airborne Radio Marker Receiving Equipment Operating on 75
MHz
·
DO-136, Universal
Air-Ground Digital Communication System Standards
·
DO-117, Standard
Adjustment Criteria for Airborne Localizer and Glide Slope Receivers
·
DO-93, Minimum
Performance Standards – Airborne Selective Calling Equipment
·
DO-52, Calibration
Procedures for Signal Generators used in the Testing of VOR and ILS Receivers
·
Task Force 5 –
NextGen Mid-Term Implementation Task Force Report
·
Task Force 5 –
NextGen Mid-Term Implementation Task Force Report– Data Files
·
Task Force 4 – Final
Report of the RTCA Task Force 4 Certification
·
Task Force 3 – Final
Report of RTCA Task Force 3 Free Flight Implementation
·
Task Force 3 –
Interim Report on Free Flight Implementation
·
Task Force 2 – Report
on the Transition to Digital Communications
·
National Airspace
System Concept of Operations and Vision for the Future of Aviation
·
Recommendations
Regarding the Concept of Equipage and Mandated versus Voluntary Considerations
·
National Airspace
System Concept of Operations
·
Issued 12-13-00
Approved by the Free Flight Steering Committee
·
National Airspace
System Concept of Operations, Addendum 4: Free Flight Phase 2
·
Government/Industry
Operational Concept for the Evolution of Free Flight, Edition 2
·
Government/Industry
Operational Concept for the Evolution of Free Flight, Addendum 3: Surveillance
·
Free Flight Action
Plan Update 2
·
Free Flight Action
Plan Update 1
·
Report of the RTCA
Board of Directors' Select Committee on Free Flight
·
Future Flight Data
Collection Committee Final Report
·
Certification
Steering Committee Final Report
·
Portable Hand-Held
GPS Receivers-What You Should Know
·
The Authority of
Agreement—A History of RTCA
PROCEEDINGS OF RTCA ANNUAL SYMPOSIA
·
2004 – Implementing a
“Performance Based” National Airspace System
·
2003 – Modernizing
Air Traffic Management in Today’s Environment
·
2002 – The New
Aviation Environment - Safety, Security and Efficiency
·
2000 – ATC
Modernization – Achieving New Operational Capabilities
·
1999 – Modernization:
Aviation’s Challenge and Opportunity for the New Millennium
·
1998 – Operations,
Certification, & Standards: Cornerstones for the Future
·
1996 – Working
Together to Deliver Free Flight
·
1993 – Implementing
Air Traffic Management – Systems Approach for the 21st Century
·
AERONAUTICAL
TELECOMMUNICATION NETWORK
·
AIRBORNE GROUND
PROXIMITY WARNING EQUIPMENT
·
AIRPORT APPLICABLE
DOCUMENTS
·
AREA NAVIGATION
EQUIPMENT (AIRBORNE)
·
AUTOMATIC DEPENDENT
SURVEILLANCE
·
AUTOMATIC DEPENDENT
SURVEILLANCE – BROADCAST
·
AUTOMATIC DIRECTION
FINDING EQUIPMENT (AIRBORNE)
·
AUTOMATIC FLIGHT
GUIDANCE, CONTROL SYSTEMS AND EQUIPMENT (AFGCS)
·
DISPLAY OF TRAFFIC
INFORMATION
·
DISTANCE MEASURING
EQUIPMENT
·
EMERGENCY LOCATOR
TRANSMITTERS (ELTs)
·
GLOBAL POSITIONING
SYSTEM (GPS)
·
HIGH FREQUENCY DATA
LINK (HFDL)
·
HISTORY
·
INSTRUMENT LANDING
SYSTEM (ILS)
·
LORAN
·
MICROWAVE LANDING SYSTEM
(MLS)
·
NEXTGEN
·
RTCA Task Force 5
NextGen Mid-Term Implementation Task Force Report
·
RTCA Task Force 5
NextGen Mid-Term Implementation Task Force Report –
·
PORTABLE ELECTRONIC
DEVICES (PEDs)
·
PROCEEDINGS OF ANNUAL
SYMPOSIA
·
RADAR
·
REQUIRED NAVIGATION
PERFORMANCE (RNP)
·
SECURITY
·
SOFTWARE
·
TERRAIN AWARENESS and
WARNING SYSTEM (TAWS)
·
TRAFFIC ALERT AND
COLLISION AVOIDANCE SYSTEM (TCAS)
·
TEST PROCEDURES /
CALIBRATION
DOCUMENT ORDERING INFORMATION
General:
All RTCA documents are available for purchase via RTCA’s Web Site,
www.rtca.org.
Prices are
in U.S. dollars. Orders may be placed using the order form included in this
book and faxed to 202-833-9434 or emailed to info@rtca.org. Orders may also be
mailed to RTCA, Inc., 1828 L Street NW, Suite 805, Washington, DC 20036. Please
include both the document number (for numbered documents) and title on your
order.
Document
orders are fulfilled within three (3) business days following receipt of
payment.
Discounts:
RTCA Members, International Associates, and Academic Associates receive
a 60% discount on all documents, unless otherwise stated. Additional discounts
are available for volume orders of a single publication. Contact RTCA for the
specifics on these discounts.
Payment:
Prepayment is required for all RTCA documents and must be made in U.S.
funds drawn on a U.S. bank. In addition to checks and money orders, RTCA
accepts MasterCard, Visa and American Express. Orders are fulfilled upon
receipt of payment.
Shipping & Handling: Standard delivery is via U.S. Postal
Service, UPS Ground or FedEx Ground for U.S., Canada and Mexico orders. All
other orders ship via U.S. Postal Service. Shipping and handling are included
in the purchase price.
Rush
Service: A U.S. $20 rush fee applies for same-day shipment
orders. Orders received after 3:00 PM will be processed the next business
morning. Provide RTCA with your Federal Express account number and shipping
specifications, or indicate that shipping charges should be applied to your credit
card. If no account number is given, your order will ship via standard
delivery.
Wire
Transfer:
Please contact the RTCA accounting department for information regarding payment
by wire transfer – (P) 202-833-9339 (F) 202-833-9434 or email info@rtca.org. A $20.00
fee is charged to receive wire transfers. Please add this amount to your total
payment.
Complete
set availability: Documents DO-52 through DO-326 may be purchased as a
complete set. Please call for pricing.
NUMBERED DOCUMENTS
DO-326, Airworthiness Security Process Specification
Issued 12-08-10 s Prepared by SC-216
The guidance of this
document is intended to augment current guidance for aircraft certification to
handle the information security threat to aircraft safety. It adds data
requirements and compliance objectives, as organized by generic activities for
aircraft development and certification. The document is the first of a series
of documents on Aeronautical Systems Security that together will address
information security for the overall Aeronautical Information System Security
(AISS) of airborne systems with related ground systems and environment. It
addresses only Aircraft Type Certification. Because of the impending
introduction of aircraft with significant security-related features, this
document is proposed for approval in advance of the other documents in this
series to address immediate industry concerns and to establish feedback on its
implementation challenges.
|
Hardcopy |
e-DO-326 (downloadable from www.rtca.org) |
|
List Price US/Canada/Mexico $150.00 All
other countries $187.50 |
Member No Charge Non-Member $187.50 |
|
Member Price US/Canada/Mexico $60.00 All
other countries $75.00 |
|
DO-325, Minimum Operational Performance Standards (MOPS) for Automatic
Flight Guidance and Control Systems and Equipment
Issued 12-08-10 s Prepared by SC-220
This document contains Minimum Operational Performance Standards (MOPS) for
Automatic Flight Guidance and Control Systems (AFGCS) and applicable
interfaces. These standards specify system characteristics that should be
useful to designers, manufacturers, installers and users of the system and
equipment. The system may also provide workload relief to pilots and provide a
means to fly a flight path more accurately to support specific operational
requirements. Standards are included for the automatic flight guidance and
control functions consisting of four equipment classes: Class A, autopilot,
Class B, yaw damper, Class C, flight director, Class D,
auto-thrust/auto-throttle and two categories of aircraft: Airplanes and
Rotorcraft.
|
Hardcopy |
e-DO-325
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$150.00 All other countries $187.50 |
Member
No Charge Non-Member
$187.50 |
|
Member
Price US/Canada/Mexico
$60.00 All other countries $75.00 |
|
DO-324, Safety and
Performance Requirements (SPR) for Aeronautical Information Services (AIS) and
Meteorological (MET) Data Link Services
Issued 12-08-10 s Prepared by SC-206
This document specifies minimal baseline operational Safety and Performance
Requirements (SPR) for the data link delivery of AIS and MET information as the
primary means of communications between air and ground. The aim of the AIS and
MET data link services is to provide aeronautical and meteorological
information for flight efficiency and/or hazard avoidance in all flight
environments. Four AIS/MET data link services are covered in this SPR: an
aeronautical update service that provides current updates of aeronautical
information; and three weather decision services that provide current updates
of meteorological information designed to support flight crew decisions in
three time categories (planning, near term and immediate decisions). The
document is based on a notional architecture and is not intended for
implementation and operational use until validation activities are completed.
It provides a framework and a methodology to be used as the basis for assessing
implementation of new data link systems or architectures as candidates for AIS
and/or MET data link services.
|
Hardcopy |
e-DO-324
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$185.00 All other countries $231.25 |
Member
No Charge Non-Member $231.25 |
|
Member
Price US/Canada/Mexico
$74.00 All other countries $92.50 |
|
DO-323,
Safety, Performance and Interoperability Requirements
Document for Enhanced Traffic Situational Awareness on the Airport Surface with
Indications and Alerts (SURF IA)
Issued 12-08-10 s Prepared by SC-186
This document provides
the minimum Operational, Safety, and Performance Interoperability Requirements
(SPR) for the implementation of Enhanced Traffic Situational Awareness on the
Airport Surface with Indications and Alerts (SURF IA). The SURF IA application
is fully defined in the Operational Services and Environment Definition (OSED)
found in SPR Appendix A. The SPR can be used as a starting point for the
development of Minimum Operational Performance Standards (MOPS), Technical Standard
Orders (TSOs) or other material to support SURF IA system development or
certification.
|
Hardcopy |
e-DO-323
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$340.00 All other countries $425.00 |
Member
No Charge Non-Member
$425.00 |
|
Member
Price US/Canada/Mexico
$136.00 All other countries $170.00 |
|
Supplement to DO-323, Safety,
Performance and Interoperability Requirements Document for Enhanced Traffic
Situational Awareness on the Airport Surface with Indications and Alerts (SURF
IA)
Issued 12-08-10 s Prepared
by SC-186
This supplement to
DO-323 is in the form of a single zip archive.
This analysis package
provides detailed information about SURF IA. The supplement consists of seven
Excel flies containing the bowtie analysis and other details that are not
included in the SURF IA SPR document, Appendix C (Operational Safety Analysis,
OSA). These supplemental files are provided for safety analysts who want to
understand the SURF IA safety analysis in more detail.
This Supplement is available only by electronic download.
|
Hardcopy |
e-DO-323
– Supplement (downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
N/A All other countries
N/A
|
Member
No Charge Non-Member
$150.00 |
|
Member
Price US/Canada/Mexico
N/A All other countries N/A |
|
DO-322,
Safety, Performance and Interoperability Requirements
Document for ATSA-SURF Application
Issued 12-08-10 s Prepared by SC-186
This document provides the minimum operational, Safety, and Performance
Requirements (SPR) and Interoperability Requirements (INTEROP) for the
implementation of enhanced Airborne Traffic Situational Awareness (ATSA) for
Surface (SURF) Operations. The primary goal of the ATSA-SURF application is to
reduce the potential for errors, runway and taxiway incursions, and collisions
by providing enhanced situational awareness to the flight crew operating an
aircraft on the airport surface, and including final approach, landing and
takeoff operations in the vicinity of the airport surface.
|
Hardcopy |
e-DO-322 (downloadable from www.rtca.org) |
|
List Price US/Canada/Mexico $295.00 All
other countries $368.75 |
Member No Charge Non-Member $368.75 |
|
Member Price US/Canada/Mexico $118.00 All
other countries $147.50 |
|
DO-321, Safety, Performance and Interoperability Requirements
Document for ADS-B Airport Surface Surveillance Application (ADS-B-APT)
Issued 12-08-10 s Prepared by SC-186
This document provides the minimum operational, Safety and Performance
Requirements (SPR) and Interoperability Requirements (INTEROP) for the
implementation of the Automatic Dependent Surveillance-Broadcast Airport
Surface Surveillance Application (ADS-B-APT). The ADS-B-APT application aims at
enhancing aerodrome operations by adding ADS-B surveillance to a non-surveilled
aerodrome and providing the controller with an appropriate graphical display to
view the surveillance data.
This document is intended to support the approval of all elements of
the CNS/ATM system relating to the ADS-B-APT application.
|
Hardcopy |
e-DO-321
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$295.00 All other countries $368.75 |
Member
No Charge Non-Member
$368.75 |
|
Member
Price US/Canada/Mexico
$118.00 All other countries $147.50 |
|
DO-320,
Operational Services and Environmental
Definition (OSED) for Unmanned Aircraft Systems
Issued 06-10-10 s Prepared by SC-203
This
document provides a basis for assessing and establishing operational, safety,
performance, and interoperability requirements for UAS operations in the US
National Airspace System (NAS). An
Unmanned Aircraft System is an unmanned aircraft and its associated components
and persons required for operation. The
OSED encompasses:
• All current
and planned UAS operations that may occur prior to 2025, except those intended
to operate strictly within visual line of sight
• All UAS
types that are in use or in the final stages of development
• All airspace
and operating environments in the current NAS (as described in the FAA NAS
Enterprise Architecture, September 2007) including airport surface and
off-airport operations
• The
operational performance and characteristics of UAS based on known values of
existing systems
|
Hardcopy |
e-DO-320
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$360.00 All other countries $430.00 |
Member
No Charge Non-Member
$430.00 |
|
Member
Price US/Canada/Mexico
$144.00 All other countries $172.00 |
|
DO-319, Safety,
Performance and Interoperability Requirements Document for Enhanced Traffic
Situational Awareness During Flight Operations (ATSA-AIRB)
Issued 03-17-10 s Prepared by SC-186
The
document provides the minimum operational, Safety and Performance Requirements
(SPR) and Interoperability Requirements (INTEROP) for the implementation of
Airborne Traffic Situational Awareness (ATSAW) for “Enhanced Traffic Situational
Awareness during flight operations” (ATSA-AIRB). This application provides flight crews with a
graphical display of AIRB Traffic relative to their aircraft together with
supporting information on that traffic.
The
requirements are necessary to provided adequate assurance that the appropriate
aspects of the relevant Communication Navigation Surveillance and Air traffic
Management (CNS/ATM) system, when operating together, will perform their
intended function in an acceptably safe manner for the operations defined in
the Operational Services and Environment Definition (OSED).
The
document is intended to support the approval of elements of the CNS/ATM system
relating to the ATSA-AIRB application.
|
Hardcopy |
e-DO-319
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$295.00 All other countries $368.75 |
Member
No Charge Non-Member
$368.75 |
|
Member
Price US/Canada/Mexico
$118.00 All other countries $147.50 |
|
DO-318, Safety, Performance
and Interoperability Requirements Document for Enhanced Air Traffic Services in
Radar-Controlled Areas Using ADS-B Surveillance (ADS-B-RAD)
Issued 09-09-09 s Prepared by SC-186
This
document defines and allocates a set of minimum requirements for the end-to-end
operational, safety, performance and interoperability aspects for the
implementations of the ADS-B-RAD application.
The requirements are necessary to provide adequate assurance that the
elements of the relevant Communication, Navigation, and Surveillance and Air
Traffic Management (CNS/ATM) system, when operating together, will
perform
their intended function in an acceptably safe manner for the operations defined
in the Operational Services and Environment Definition (OSED). This system includes ground and airborne
elements. In addition, the document
defines ADS-B requirements applicable to dense airspaces such as those found
in Europe
and the USA.
|
Hardcopy |
e-DO-318
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$340.00 All other countries $425.00 |
Member
No Charge Non-Member
$425.00 |
|
Member
Price US/Canada/Mexico
$136.00 All other countries $170.00 |
|
DO-317, Minimum
Operational Performance Standards (MOPS) for Aircraft Surveillance Applications
System (ASAS)
Issued 04-14-09 s Prepared by SC-186
This
document contains the recommended requirements for the processing and display
of traffic Ownship information for use by the flight crew in processing
airborne applications. The document
considers functional requirements consisting of: Airborne Surveillance and
Separation Assurance Processing (ASSAP), and Cockpit Display of Traffic
Information (CDTI) as described in DO-289, Minimum
Aviation System Performance Standards (MASPS) for Aircraft Surveillance
Applications (ASA). It includes
requirements to support the initial five applications included in DO-289: Enhanced Visual Acquisition (EVAcq), Conflict
Detection (CD), Airport Surface Situational Awareness (ASSA), Final Approach
and Runway Occupancy Awareness (FAROA) and Enhanced Visual Approach
(EVApp). Operational performance
standards for functions or components that exceed the stated minimum
requirements are identified as optional features.
In
order to provide more complete traffic situational awareness, the Traffic Alert
and Collision Avoidance System (TCAS) display should be integrated with the
CDTI on aircraft equipped with TCAS.
This document provides requirements and guidance for integration of TCAS
with ASAS.
|
Hardcopy |
e-DO-317
(downloadable from www.rtca.org) |
|
List
Price US/Canada/Mexico
$295.00 All other countries $368.75 |
Member
No Charge Non-Member
$368.75 |
|
Member
Price US/Canada/Mexico
$118.00 All other countries $147.50 |
|
Supplement
to DO-317, Minimum
Operational Performance Standards (MOPS) for Aircraft Surveillance Applications
System (ASAS)
Issued 04-14-09 s Prepared by SC-186
This
supplement to DO-317 is in the form of a single zip archive. One portion of this archive decompresses into
the stimulus test data described in Section 2.5.7 of this MOPS. The stimulus scenarios reflect all the
appropriate surveillance sources for the scenario (i.e., ADS-B, ADS-R, TIS-B
and TCAS) are provided separately for 1090ES and UAT implementations (due to
the difference in State Vector construction for each). Appendix C of this MOPS describes an example
implementation of the ASSAP algorithms.
A MATLAB implementation of these algorithms (oriented to a 1090ES split
state vector implementation) was developed in support of this MOPS. The other portion of the archive contains the
MATLAB files that
constitute this
ASSAP implementation. This zip file will
extract into two subdirectories: “ASSAP_test_data” which includes the stimulus
scenarios and "ASAS_simulation_1090ES_implementation" which includes
the MATLAB files.
This
Supplement is available only by electronic download.
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DO-316,
Minimum Operational Performance Standards (MOPS) for Global Positioning
System/Aircraft Based Augmentation System Airborne Equipment
Issued 04-14-09 s Prepared by SC-159
This
document contains Minimum Operational Performance Standards for
single-frequency airborne navigation sensor equipment not augmented by ground
or space-based systems. The standards define minimum performance, functions and
features for GPS sensors that provide position information to a multi-sensor
system or separate navigation system.
They also address Area Navigation (RNAV) equipment to be used for the en
route, terminal, and Lateral Navigation (LNAV) phases of flight.
The
basis for this document is RTCA/DO-229D - MOPS for GPS/WAAS Airborne Equipment,
Class
Beta 1 receiver without SBAS requirements.
In
comparison with the older GPS MOPS - RTCA/DO-208… the document reflects:
1) An updated
signal operating environment (updated interference environment),
2) The absence of
Selective Availability (SA) (which was turned off on May 1st 2001 as
a result of a Presidential Directive),
3) Updated RAIM
(Receiver Autonomous Integrity Monitoring) for GPS and,
4) Optional GPS
receiver velocity accuracy and velocity FOM (Figure of Merit) computation.
Note:
WAAS: Wide Area Augmentation Systems
ABAS: Aircraft Based Augmentation Systems
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DO-315A, Minimum
Aviation System Performance Standards (MASPS) for Enhanced Vision Systems,
Synthetic Vision Systems, Combined Vision Systems and Enhanced Flight Vision
Systems
Issued 09-15-10 s Prepared by SC-213
DO-315A adds system design
criteria for use of EFVS to landing with reported visibility as low as 1000ft
RVR (or 300 meters). Specific features
with DO-315A include a touchdown zone requirement and use of a radio altimeter
and flare prompt. The flight test matrix
was expanded, and a transport aircraft appendix was added. Vertical flight path guidance, flare
guidance, pilot monitoring display requirements, and design assurance
requirements were also addressed.
Synthetic vision performance requirements were not changed, but are
planned for next revision.
The
document addresses Enhanced Vision Systems (EVS), Synthetic Vision Systems
(SVS), and Combined Vision Systems (CVS) technologies. The MASPS provides the
high level system requirements for Enhanced, Synthetic, and Combined Vision
Systems when installed in aircraft with the express purpose of gaining no
additional operational credit. Currently,
only EVS technology incorporating an approved Head-Up Display (HUD) is eligible
for operational credit under Title 14 US Code of Federal Regulations (CFR)
§91.175 with the Federal Aviation Administration (FAA). An approved combination of EVS and HUD is
termed an Enhanced Flight Vision System (EFVS) by the FAA.
For the
FAA, EVS for operational credit is called "EFVS", and the term
"EFVS" is used in this document. The EFVS subsections of this MASPS
provide the high level system requirements for Enhanced Flight Vision Systems
when installed in aircraft with the express purpose of gaining additional
operational credit.
The European Aviation Safety Agency (EASA) uses the
term “EVS” as equivalent to the FAA description of EFVS.
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DO-314,
Safety, Performance and Interoperability Requirements Document for Enhanced
Visual Separation on Approach (ATSA-VSA)
Issued 12-16-08 s Prepared by SC-186
This document provides the minimum
operational, Safety, and Performance Requirements (SPR) and Interoperability
Requirements (INTEROP) for the implementation of Airborne Traffic Situational
Awareness (ATSA) for “Enhanced Visual Separation on Approach” (VSA). The ATSA-VSA application is fully defined. The
document defines and allocates the set of minimum requirements for the
end-to-end operational, safety, performance, and interoperability aspects for
implementations of the ATSA-VSA application.
The requirements contained in
this document are necessary to provide adequate assurance that the appropriate
aspects of the relevant Communication Navigation Surveillance and Air Traffic
Management (CNS/ATM) system, when operating together, will perform their
intended function in an acceptably safe manner for the operations defined in
the OSED. The system here includes
ground and airborne elements.
The
document was developed jointly by RTCA Special Committee 186 and EUROCAE
Working Group 51 - within the group commonly referred to as the “ADS-B
Requirements Focus Group” (RFG).
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DO-313, Certification
Guidance for Installation of Non-Essential, Non-Required Aircraft Cabin Systems
and Equipment
Issued 10-02-08 s Prepared by SC-210
This
document provides certification guidance on how to meet the airworthiness
requirements for the installation of non-essential, non-required aircraft Cabin
Systems and Equipment (CS&E) and in doing so enable a standardized approach
across equipment manufacturers and installers. The information contained
herein is applicable to installation methodologies of aircraft CS&E
approved under 14 CFR parts 23, 25, 27 and 29. Both aerospace
manufactured equipment and commercial off the shelf (COTS) equipment is
considered.
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DO-312,
Safety, Performance and Interoperability Requirements Document for the
In-Trail Procedure in Oceanic Airspace (ATSA-ITP) Application
Issued 06-19-08 s Prepared by SC-186
This document provides the minimum operational, safety, and performance requirements (SPR) and interoperability requirements (INTEROP) for the implementation of enhanced Airborne Traffic Situational Awareness (ATSA) for “In-Trail Procedure” (ITP). The objective of the In-Trail Procedure (ITP) is to enable aircraft that desire Flight Level changes in Procedural Airspace to achieve these changes on a more frequent basis, thus improving flight efficiency while maintaining safe separation from other aircraft. The requirements contained in the document are necessary to provide adequate assurance that the appropriate aspects of the relevant Communication Navigation Surveillance and Air Traffic Management (CNS/ATM) system, when operating together, will perform their intended function in an acceptable safe manner for the defined operations. The requirements can be used for approval processes including aircraft type design approval, aircraft operator operational approval, and Air Traffic Services provider operational approval.
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DO-311, Minimum
Operational Performance Standards for Rechargeable Lithium Battery Systems
Issued 03-13-08 s Prepared by SC-211
This
document contains Minimum Operational Performance Standards (MOPS) for rechargeable
Lithium battery systems to be used as permanently installed power sources on
aircraft. Compliance with these
standards is recommended as a means of assuring that the Lithium battery will
perform its intended function(s) safely, under conditions normally encountered
in aeronautical operations. These
standards apply to the chemical composition, cell size, cell construction, cell
interconnection methods within batteries, venting provisions, operational and
storage environments, packaging, handling, test, storage and disposal of
rechargeable Lithium batteries, installed separately or in avionics equipment
aboard aircraft.
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DO-310,
Minimum Operational Performance Standards for GPS Ground-based Regional
Augmentation System Airborne Equipment
Issued 03-13-08 s Prepared by SC-159
The
document contains Minimum Operational Performance Standards (MOPS) for airborne
navigation equipment using signals from the Global Navigation Satellite System
(GNSS) augmented by a Ground-based Regional Augmentation System (GRAS). The document defines minimum performance
requirements, functions and features for GRAS airborne equipment to support all
phases of flight including en-route, terminal, LNAV (Lateral NAVigation),
LNAV/VNAV (Lateral NAVigation/Vertical NAVigation), LP (Localizer Approach with
FAS data but without vertical guidance), LPV (Localizer Precision with Vertical
guidance) (but not CAT-I/II/III). GRAS equipment will be compatible with
the Ground Based Augmentation System (GBAS) and will be able to use the signal
in space for approved approach operations. Compliance with these
standards by manufacturers, installers and users is recommended as a means of
assuring that the equipment will satisfactorily perform its intended functions
under conditions encountered in routine aeronautical operations.
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DO-309, Minimum
Operational Performance Standards (MOPS) for Helicopter Terrain Awareness and
Warning System (HTAWS) Airborne Equipment
Issued 03-13-08 s Prepared by SC-212
This MOPS defines a Helicopter
Terrain Awareness and Warning System (HTAWS), Airborne System. The HTAWS is an
alerting system intended to provide terrain and obstacle aural and visual
alerts. It is designed to reduce the risk of Controlled Flight into Terrain
(CFIT) accidents by providing increased situational awareness of the
surrounding terrain and obstacles, mainly during the cruise phase in Visual
Meteorological Condition (VMC) and in Instrument Meteorological Condition (IMC)
under Instrument Flight Rules (IFR). HTAWS is not intended to be used as an aid
for navigation.
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DO-308,
Operational Services and Environment Definition (OSED) for Aeronautical
Informational Services (AIS) and Meteorological (MET) Data Link Services
Issued 12-06-07 s Prepared by SC-206
The
document presents the AIS and MET data link services that are envisaged to be
implemented within the next decade in both the
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DO-307, Aircraft Design
and Certification for Portable Electronic Device (PED) Tolerance
Issued 10-11-07 s Prepared by SC-202
This
document recommends aircraft design and certification criteria to tolerate the
operation of PEDs. These aircraft design and certification
recommendations, when implemented in an aircraft design, would reduce the need
for restricting the use of PEDs.
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Change 1 to DO-307
Issued 12-16-08
Change 1 to DO-307 - Aircraft Design and
Certification for Portable Electronic Device (PED) Tolerance corrects
typographical errors, clarifies document language in several places, and aligns
calculated values for Target IPL with the values in DO-294C.
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DO-306, Safety and
Performance Standard for Air Traffic Data Link Services in Oceanic and Remote
Airspace (Oceanic SPR Standard)
Issued 10-11-07 s Prepared by SC-189
This document provides the
operational, safety, and performance requirements (SPR) for the implementation
of air traffic data link services in oceanic and remote airspace, referred to
as Oceanic SPR Standard. It is intended
to support the implementation of communication, navigation, and
surveillance/air traffic management (CNS/ATM) systems in worldwide
application. It provides the minimum
operational, safety, and performance requirements and allocations based on the
results of a coordinated requirements determination process, which included
operational services and environment information capture, operational safety
assessment (OSA), and an operational performance assessment (OPA).
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Change 1 to DO-306
Issued 03-17-11
s Prepared by SC-214
Change 1 to DO-306 - Safety and Performance Standard for Air Traffic Data Link Services in
Oceanic and Remote Airspace (Oceanic SPR Standard) provides unambiguous
Controller-Pilot Datalink Communications (CPDLC) Message definitions that will
be used by FANS 1/A Datalink systems in support of In-Trail Procedures (ITP)
operations. It includes changes resulting from work on Advanced ATS Datalink
services definition. The Sections and Tables affected are provided.
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DO-305, Future Air
Navigation System 1/A (FANS 1/A) - Aeronautical Telecommunications Network
(ATN) Interoperability Standard
Issued 06-26-07 s Prepared by SC-189
This document provides interoperability
requirements to enable FANS 1/A aircraft and ATN aircraft to co-exist in the
same operational environment. The
standard was developed to enable air traffic service providers (ATSPs) to
interoperate with data link equipped aircraft, regardless of which technology
is installed on the aircraft. The
standard is intended for the convergence of oceanic and continental data link
applications. It provides the
interoperability requirements for an aeronautical telecommunication network
baseline 1 (ATN B1) ground system that provides air traffic data link
services to future air navigation system 1/A (FANS 1/A) aircraft in
continental airspace.
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DO-304, Guidance
Material and Considerations for Unmanned Aircraft Systems
Issued 03-22-07 s Prepared by SC-203
This document addresses all
Unmanned Aircraft Systems (UAS) and UAS operations being considered for
realistic implementation in the US National Airspace System (NAS) in the
foreseeable future. It is intended to educate the community and be used to
facilitate future discussions on UAS standards. It provides the aviation
community a definition of UAS, a description of the operational environment,
and a top-level functional break down. The guidance material provides a
framework for developing standards through RTCA Special Committee 203.
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DO-303,
Safety, Performance and Interoperability
Requirements Document for the ADS-B Non-Radar-Airspace (NRA) Application
Issued 12-13-06 s Prepared by SC-186
This
document addresses the operational concept and minimum requirements for the use
of ADS-B Surveillance for ATS services in Non-Radar Areas (ADS-B-NRA).
Annexes of the document contain the Operational Services and Environment
Definition (OSED), a comparative Operational Performance Assessment (OPA), an
Operational Safety Assessment (OHA), and a summary of a published comparative
risk assessment. The results of these assessments have been compiled into
Section 3 of the main body which specifies the minimum operational safety and
performance requirements (SPR). Interoperability requirements specifying
the needed transfer of data between transmitting aircraft and ground domains is
provided in section 4 (INTEROP). This INTEROP specification is presented
at a link-neutral (i.e. MASPS) level. Annex H provides traceability of
Section 4 to specific 1090MHz Extended Squitter interoperability requirements. It was developed jointly with EUROCAE.
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DO-302, Minimum
Operational Performance Standards (MOPS) for Surveillance Transmit Processing
(STP)
Issued 12-13-06 s Prepared by SC-186
This document contains
requirements for interfacing ADS-B avionics to on-board position sources such
as GPS and Flight Management Systems. Proper integration and installation
of ADS-B equipment into aircraft is essential to successful implementation of
ADS-B air-to-ground and air-to-air applications. The Surveillance Transmit Processing (STP) subsystem prepares the
required surveillance information from on-board aircraft sensors for the ADS-B
Transmit Subsystem. STP is a critical subsystem
of the end-to-end system defined in the Minimum Aviation System Performance
Standards (MASPS) for Aircraft Surveillance Application (ASA), (RTCA
DO-289). The standards defined in this version of the STP MOPS have been
scoped to support parameters required for five applications defined in the ASA
MASPS:
· Enhanced Visual Acquisition (EVAcq)
· Conflict Detection (CD)
· Airport Surface Situational
Awareness (ASSA)
· Final Approach and Runway Occupancy
Awareness (FAROA)
· Enhanced Visual Approach (EVApp)
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DO-301, Minimum
Operational Performance Standards for Global Navigation Satellite System (GNSS)
Airborne Active Antenna Equipment for the L1 Frequency Band
Issued 12-13-06 s Prepared by SC-159
This
document contains Minimum Operational Performance Standards (MOPS) for GNSS
airborne active antenna equipment designed to use the GPS or Galileo L1
frequency augmented by other systems/equipment/techniques as appropriate to
meet the performance requirements for primary means of navigation for en route,
terminal, non-precision, and precision approach phases of flight. An
active antenna is one integrated with a preamplifier. Minimum
requirements for passive designs are specified in DO-228 and DO-228, Change
1. This MOPS specifies an alternative to active antenna requirements
specified in DO-228 and DO-228, Change 1
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DO-300,
Minimum Operational Performance
Standards (MOPS) for Traffic Alert and Collision Avoidance System II (TCAS II)
Hybrid Surveillance
Issued 12-13-06 s Prepared by SC-147
This
document will allow TCAS to lower the number of aircraft it actively tracks
through the use of passive tracking aircraft via the Extended Squitter.
(Active tracking is used intermittently to validate the ADS-B data.)
This will allow TCAS to increase its operational range as it will not
need to initiate interference limiting since the number of actively tracked
aircraft will be lower. Hybrid Surveillance will also decrease the
overall RF environment which will bring operational benefits to ADS-B.
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Issued 07-01-09
Change 1 to
DO-300 provides corrections to the test section and provides linkage to
DO-185B.
The change corrects short
comings in the test procedures and highlights the DO-185B requirements on how a
DO-300 compliant TCAS II system should broadcast its hybrid surveillance
capability.
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DO-299,
Report - Assessment and Recommendations on Visual Alerts and Aural
Annunciations for TCAS II
Issued 03-14-06 s Prepared by SC-147
Since the introduction of TCAS II, opposite reactions to Negative
Resolution Advisories (RAs) have been regularly identified and have continued
with TCAS II Version 7. Special Committee 147 was tasked to analyze the
display configurations and aural alerts for Negative RAs. The purpose of
this work was to determine whether problems exist with current display and
annunciation requirements for this class of RA. This report documents
results of SC-147’s analysis and recommends an approach for resolving
identified problems.
The report is structured as follows:
·
Section 1 provides an introduction into the issues
being investigated and a high level overview of the work.
·
Section 2 describes the implementation of various
types of RA displays
·
Section 3 describes the data used in developing the
conclusions and recommendations.
·
Section 4 presents the conclusions reached.
·
Section 5 presents recommendations for corrective
actions to reduce the frequency of opposite responses to Negative RAs. The section also presents recommendations for
further work on other related issues.
·
Appendices are also included in the report to
provide additional details on related issues, data collection methodology, and
data results.
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DO-298, Safety Analysis of Proposed Change to TCAS
RA Reversal Logic
Issued 11-08-05 s Prepared by SC-147
DO-298 is an
SC-147 report which documents analyses recommending changes to the TCAS II
Version 7 collision avoidance logic (Section 2.0 item 2) in accordance with
SC-147 Terms of Reference guidance.
The report was
developed to perform a detailed analysis of the TCAS II Version 7 Resolution
Advisory (RA) sense reversal logic, investigating the safety impacts of
revising the collision avoidance logic to improve the performance of RA
reversals for certain encounter geometries.
Some encounter geometries have been shown to exist which TCAS II Version
7 may not appropriately resolve with RA sense reversals in certain
airspaces. SC-147 has studied the
frequency with which these geometries are operationally experienced and
recommends the changes specified in this report to reduce collision risk in
these encounter geometries.
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DO-297,
Integrated Modular Avionics (IMA) Development Guidance and Certification
Considerations
Issued 11-08-05 s Prepared
by
SC-200
DO-297 contains guidance for Integrated Modular
Avionics (IMA) developers, application developers, integrators, certification
applicants, and those involved in the approval and continued airworthiness of
IMA systems in civil certification projects.
It is focused on IMA-specific aspects of design assurance.
IMA is described as a shared set of flexible,
reusable, and interoperable hardware and software resources that, when
integrated, form a platform that provides services, designed and verified to a
defined set of requirements, to host applications performing aircraft
functions. The primary industry-accepted guidance for satisfying airworthiness
requirements for IMA components is included and it describes application
properties as they relate to their integration with a platform.
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DO-296,
Safety Requirements for
Aeronautical Operational Control (AOC) Datalink Messages
Issued
10-19-04 s Prepared by SC-201
This document provides minimum safety requirements
for Aeronautical Operational Control (AOC) and certain Air Traffic Services
(ATS) datalink messages. Approval via
design assurance alone or design assurance in conjunction with risk reduction
strategies are two means of addressing the hazards identified. This document
recommends alternative strategies for demonstrating to a regulatory authority a
composite approach to safety that is deemed equivalent to that provided solely
by a design assurance solution.
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DO-295, Civil Operators’ Training Guidelines for
Integrated Night Vision Imaging System Equipment
Issued
10-19-04 s Prepared by SC-196
This document presents training guidance that has
been generated from lessons learned by agencies having many years of experience
in the training and operational application of night vision imaging
systems. By tapping this experience base it is hoped that civil aircrew,
through appropriate ground and flight training, will learn how to properly use
night vision imaging systems, thus enhancing the effectiveness of night
operations while mitigating the potential for mishaps relating to the use of
these systems.
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DO-294C,
Guidance on Allowing Transmitting Portable Electronic Devices (T-PEDs) on Aircraft
Issued
12-16-08 s Prepared by SC-202
DO-294C
completes the work of Special Committee (SC) -202 and provides the results of
work on dialog with consumer electronics manufacturers’ associations on
consensus recommendations for facilitating safe use of PEDs onboard aircraft.
Further, the document incorporates the previously released Change 1 to DO-294B,
and addresses changes to align with the work done for DO-307. Changes
were made to introductory materials in Appendix 5.B, Appendix 5.C, Appendix
6.D, and Appendix 10.
The document addresses near-term T-PED technologies
such as existing devices enabled with cellular technologies, wireless local
area networks (WLANS), and wireless personal area networks (WPANS) as well as
emerging PED technologies, for example active RF Identification (RFID) tags, transmitting
medical devices, and picocells for devices enabled by cellular technologies for
use on board aircraft. The document
defines and recommends a process by which aircraft operators and/or
manufacturers may assess the risk if interference due to a specific T-PED
technology within any aircraft type and model
It also provides a means for aviation authorities and others to
determine acceptable and enforceable policies and processes for passenger and
crew use of T-PEDs.
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Issued 12-02-09
s Prepared by SC-211
This document provides guidance for avionics
manufacturers developing Nickel-Cadmium, Nickel Metal-Hydride, and Lead-Acid
batteries to be used as power sources for equipment installed in aircraft. Specifically, the document addresses the
chemical composition, cell size, cell construction, interconnection of the cell
into batteries, venting, operational and storage environments, packaging,
handling, test, storage and disposal. The document includes the new Nickel
Metal-Hydride guidance and the earlier Change 1 that addressed testing concerns
identified by industry.
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DO-292,
Assessment of Radio Frequency Interference Relevant to the GNSS L5/E5A
Frequency Band
Issued
07-29-04 s Prepared by SC-159
DO-292 addresses potential radio frequency
interference (RFI) to the future GNSS L5 signal when used for aeronautical
radio navigation, and where feasible includes RFI considerations relating to
the Galileo E5A signal as well. The
report also evaluates the potential effects of external and on-board signal
environment on the performance of an L5 receiver.
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DO-291A, Interchange Standards for Terrain,
Obstacle, and Aerodrome Mapping Data
Issued 04-14-09 s Prepared
by SC-217/EUROCAE
WG-44
This
document recommends guidelines and requirements for developing a data
interchange format for terrain, obstacle, and aerodrome data. A common
database interchange standard is a key factor in successfully implementing
digital functions in the aviation domain.
Use of information contained in this document will help system designers
assure a common interchange between data originators and data integrators. The
updated version for the exchange standard is published to reflect the industry
changes to the requirement document:
·
Includes
additional features and attributes derived from the changes contained in DO-272B
·
Makes
editorial corrections.
Two
related documents specify requirements for database content and quality:
-
DO-272B, User Requirements for Aerodrome
Mapping Information
-
DO-276A, User Requirements for Terrain
and Obstacle Data
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DO-290, Safety and
Performance Requirements Standard for Air Traffic Data Link Services in
Continental Airspace (Continental SPR Standard)
Issued
04-29-04 s Prepared by SC-189
The document provides the
operational, safety, and performance requirements (SPR) for the implementation
of data link services that support air traffic services (ATS) in continental
airspace. It is intended to support the
implementation of communication, navigation, and surveillance / air traffic
management (CNS/ATM) systems in worldwide application.
The SPR standard is intended
for use with interoperability requirements (INTEROP) standards, and the
guidelines described in RTCA DO-264 “Guidelines for Approval of the Provision
and Use of Air Traffic Services Supported by Data Communications.” These requirements are necessary to provide
adequate assurance that the elements of the CNS/ATM system, when operating
together, will perform their intended function in an acceptably safe
manner.
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Issued 12-13-06 s Prepared
by SC-189
This change minimizes nuisance error messages being
sent to the aircraft when the flight crew initiates a request to the receiving
ATSU prior to the connection being enabled.
The current system provides indication of when the connection has been
established but not when the CPDLC connection has been enabled. The change minimizes nuisance error messages
to the flight crew by providing them indication of the CPDLC connection being
enabled when the R‑ATSU sends a CPDLC message to the aircraft containing
the facility designation, facility name, and facility function. Correct errors: This change corrects an error in the safety
requirement SR 11 for ACL, DCL, and DSC.
The corresponding latency requirement ETRESPONDER is associated
with the time needed to “send” the message, not “receive the message”.
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Change 2 to DO-290
Issued 06-26-07 s Prepared
by SC-189
Change
2 includes clarification and additional guidance for:
1)
A Continental Controller Pilot Data Link Communications (CPDLC) message set
2)
Specifying CPDLC [level] parameter as a vertical range
3)
Mimicking ICAO Doc 4444 message elements using free text
4)
Establishing CPDLC
5)
CPDLC emergency messages
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Issued
12-09-03 s Prepared by SC-186
This document contains minimum
performance standards for airborne equipment to support Airborne Surveillance
Applications. Requirements for five applications are specified in detail; these
are Enhanced Visual Acquisition, Conflict Detection, Enhanced Visual Approach,
Airport Surface Situational Awareness, and Final Approach and Runway Occupancy
Awareness. Preliminary requirements are provided for three applications; these
are Approach Spacing for Instrument Approaches, Independent Closely Spaced
Parallel Runways, and Airborne Conflict Management.
Section 1 contains background and introductory material, Section 2 contains
system level requirements, and Section 3 contains subsystem requirements. There
are 11 appendices including eight application appendices that describe the
applications in detail, and explain the analysis that resulted in the
requirements in the body of the document.
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Change 1 to DO-289
Issued 12-13-06 s Prepared
by SC-186
This change to DO-289 mainly clarifies the
definitions of several parameters transmitted by aircraft in ADS-B
messages. These parameters provide information to the recipient of the
ADS-B message about the quality of the transmitted aircraft position. The
change has been developed in a manner that reflects typically available
aircraft position sources and should not impact ADS-B equipment previously
certified using RTCA DO-260A for 1090 MHz Extended Squitter or RTCA DO-282A for
the Universal Access Transceiver (UAT).
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Issued
10-28-03 s Prepared by SC-198
The document describes the current
situation as well as goals and objectives for transition from analog Air/Ground
(A/G) telecommunications to A/G Very High Frequency (VHF) Digital Link Mode 3
(VDL Mode 3) based integrated voice and data communications. It includes a transition strategy from analog
voice to VDL
Mode 3 digital voice and Aeronautical
Telecommunications Network (ATN) based data communications via VHF Digital Link
Mode 2 and VDL Mode 3.
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Issued
6-25-03 s Prepared by SC-194
This document addresses the phased implementation process of the ADLS beyond Build 1A in all operational domains and phases of flight. It focuses on Build IIA for domestic en route and Build IIB for terminal area operations. Issues addressed include accommodation, transition and the development of new operational services using data link and integration with ATS decision support tools. It also describes the aviation community consensus regarding the evolution and implementation path for the provision of ATS
over ATN in the NAS.
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Issued 10-11-07
s Prepared by SC-186 Supersedes DO-286A
This
revision to DO-286A separates Automatic Dependent Surveillance - Rebroadcast
(ADS-R) from the TIS-B MASPS. The basic TIS-B services described in
DO-286A remain fundamentally unchanged. The revision includes changes
related to those previously made to RTCA DO-242 - MASPS for Automatic
Dependent Surveillance - Broadcast (ADS-B) and DO-289 - MASPS for
Aircraft Surveillance Applications (ASA). The revision should not
impact equipment previously certified using DO-260A - MOPS for 1090 MHz
Extended Squitter (ADS-B) and TIS-B or DO-286A.
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DO-285, Next Generation
Air/Ground Communications (NEXCOM) VDL Mode 3 Interoperability
Issued 4-10-03 s Prepared by SC-198
This document provides the interoperability requirements
for Air Traffic Services (ATS) supported by NEXCOM Very High Frequency (VHF)
Digital Link (VDL) Mode 3. It identifies NEXCOM interoperability requirements
for ATS supported by digital voice communications in the U.S. National Airspace
System (NAS). Interoperability requirements are the minimum technical and
functional requirements that provide the basis for ensuring compatibility
between the aircraft system, the ATS Provider system, and the operator’s
provisions to use the air traffic services.
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DO-284,
Next Generation
Air/Ground Communication System (NEXCOM) Safety and Performance Requirements
(SPR)
Issued
1-23-03 s Prepared by SC-198
This NEXCOM SPR document defines the
operational safety hazards and performance requirements of the NEXCOM system
(both airborne and ground subsystems). The SPR will be used to coordinate
safety objectives and to allocate performance requirements for the system. It
has been developed using the NEXCOM Operational Safety Assessment (OSA) and the
NEXCOM Operational Performance Assessment (OPA). These two assessments define
the safety functions, performance expectations, and characteristics of the
operational environments needed to support the Air Traffic Services (ATS)
identified in the NEXCOM Operational Services and Environment Definition
(OSED). The SPR document identifies the objectives and allocated requirements
(including substantiation) for a specific operation.
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Change 1 to DO-284
Issued 6-25-03 s Prepared
by SC-198
Change 1 adds new safety requirements
to DO-284. The bit error rate (BER) is now indicated in the integrity value and
this update is included throughout the document.
The number of operational hazards are increased in the Operational Hazard Assessment as outlined below:
- Hazard Class 2 (must be extremely remote) 4 hazards
- Hazard Class 3 (must be remote) 20 hazards
- Hazard Class 4 (may be probable) 5 hazards
Safety goal requirements now total 33. In Appendix B1, Operational Safety Assessment, several tables are updated with new information regarding loss of communication hazards related to interference caused by an analog transmission.
Numerous other minor changes are also
included.
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Issued 10-28-03 s Prepared by SC-181
Supersedes DO-283
This
document supersedes RTCA DO-283, Minimum
Operational Performance Standards for Required Navigation Performance for Area
Navigation, published in October 2002.
The document provides guidance to support the graphic depiction of
navigation data on an electronic map display and is consistent with the
implementation of navigation functions defined in the RNP MASPS, DO-236B. DO-283A provides map display information in
Appendix K, which is new in this version.
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DO-282B,
Minimum Operational Performance Standards for Universal Access Transceiver
(UAT) Automatic Dependent Surveillance – Broadcast
Issued 12-02-09 s Prepared by SC-186
Supersedes DO-282A and Change 1
The
document contains Minimum Operational Performance Standards for airborne
equipment to support Automatic Dependent Surveillance – Broadcast utilizing the
Universal Access Transceiver (UAT). UAT
is a multi-purpose aeronautical data link intended to support not only ADS-B,
but also Flight Information Service – Broadcast (FIS-B), Traffic Information
Service – Broadcast (TIS-B) and, if required in the future, supplementary
ranging and positioning capabilities.
This
revision supersedes DO-280A and incorporates the earlier Change 1. It also addresses issues identified by the
international community resulting from review of ICAO Standards and Recommended
Practices (SARPs) and Technical Manuals for UAT. FAA Technical Standard Order (TSO) – 154c
references this document.
The
document was developed in parallel with DO-260B.
Changes…only
for the revised DO-282B:
•
Added
NIC Supplement to encode a radius of containment for less than 0.3 nautical
mile (retains backward compatibility)
•
State
Vector Element of UAT Messages modified to add Uplink Feedback field to provide
information on reception of Ground Uplinks
•
Mode
Status Element of UAT Messages modified to add new fields (e.g., Single Antenna
Flag, System Design Assurance, SIL Supplement, GVA, UAT IN, 1090ES IN)
•
Target
State Element of UAT Messages modified to reflect changes in Target State data
•
Receiver
upper limit of dynamic range changed from -10 dBm to -3 dBm to improve aircraft
to aircraft minimum distance from 120 feet to 50 feet
•
Mode
A Code transmission inhibited by configuration parameter
•
Latency
requirements added to limit total position data latency to 1.5 seconds
Changes common
to both the revised DO-282B and DO-260B:
•
Eliminated
the Following Fields
–
Receiving
ATC Services (set to reserved)
–
CDTI
Traffic Display Capability
–
IFR
Capability Flag
–
Position
Offset Applied
–
Surveillance
Integrity Level
•
Newly
defined Source Integrity Level is considered equivalent for backward
compatibility with Version 1 receivers)
–
Barometric
Altitude Quality
•
Added
the Following Fields
–
Lateral
and Longitudinal GPS Antenna Offset
•
Encoding
includes a value denoting GPS Antenna Offset has been applied by GPS position
source
–
Integrity
Fields replacing Version 1 Surveillance Integrity Level
•
Source
Integrity Level
•
System
Design Assurance (SDA) Level
•
Source
Integrity Level Supplement
–
1090ES
IN (indicates 1090ES Receive capability)
–
UAT
IN (indicates UAT Receive capability)
–
Geometric
Vertical Accuracy
•
Modified
the Following Fields
–
Aircraft/Vehicle
Length and Width Code modified to add encoded value for “No Data” condition
–
TCAS
Operational
–
NIC
encoding for a radius of containment of less than 0.3 nautical miles added
•
Mode
A Code required to be broadcast when on-the-Ground as well as Airborne
•
Removed
vertical component of NIC, SIL, NACP and NACV
•
Target
State Data has been modified
–
Eliminated
Target Altitude and Target Heading and replaced them with Selected Altitude,
Selected Heading and Barometric Pressure Setting
–
Mode
Bits modified
•
Added
requirements for position source selection
•
Incorporated
an equipage class for single antenna aircraft
•
Modified
the receiver dynamic range requirement for reception from aircraft as close as
50 feet to better support surface applications
The document is available as an
electronic download.
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Issued 11-08-05 s Prepared by SC-172
The changes in DO-281A were made to maintain
requirement traceability and harmonization with the updated ICAO VDL Mode 2
Technical Manual as well as AEEC 631 implementation characteristics.
This document presents Minimum Operational
Performance Standards (MOPS) and test procedures for Aircraft Very High
Frequency (VHF) Digital Link (VDL) Mode 2 physical link and network layer
protocol components of an avionics transmitter/receiver (transceiver). These
transceivers are intended for air-ground (A/G) data communications. Equipment
certified to standards in this MOPS will be compatible with the relevant
Minimum Aviation System Performance Standards (MASPS) in RTCA DO-224B, Signal-in-Space Minimum Aviation System
Performance Standards (MASPS) for Advanced VHF Digital Data Communications
Including Compatibility with Digital Voice Techniques, and with the
International Civil Aviation Organization (ICAO) VDL Mode 2 Technical Manual.
Compliance with this MOPS is one means of assuring that the VDL Mode 2
equipment will function satisfactorily under all conditions normally
encountered in the air traffic control A/G operations and that data formats
will be compatible with the Aeronautical Telecommunication Network (ATN).
This document supersedes DO-281.
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DO-280B,
Interoperability Requirements Standard For ATN Baseline 1 (INTEROP ATN B1)
Issued 06-26-07 s Prepared by SC-189
This
update to DO-280, initially issued in June 2002, includes:
1)
The Controller Pilot Data Link Communications (CPDLC) protected mode feature
2)
Revisions to the ACM Service
3)
An update CPDLC message set per ICAO Doc 4444 & DO-290 – Ch. 2/ED-120 –
Ch. 2
4)
Aircraft timer (tts) made optional
5)
Corrections to the DO-280 “A” version.
DO-280B
provides interoperability requirements for ATN B1 ground systems providing
continental data link services to ATN B1 aircraft.
This
document is compiled in two volumes which are not sold separately:
-
Volume
1, Sections 1 – 4
-
Volume
2, Annexes A – C; Appendices A - C
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DO-279, Next Generation Air/Ground Communications
(NEXCOM) Principles of
Operation VDL Mode 3
Issued
3-5-02 s Prepared by SC-198
This document
characterizes the operational use of VDL Mode 3 integrated voice and data
systems for air/ground communications in the U.S. National Airspace System. The
principles defined are for Air Traffic
Control related
air/ ground communications services that apply to both voice and data
operations.
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DO-278,
Guidelines for Communications, Navigation, Surveillance, and Air Traffic
Management (CNS/ATM) Systems Software Integrity Assurance
Issued
3-5-02 s Prepared by SC-190
This document provides guidelines for the assurance of
software contained in non-airborne CNS/ATM systems. It is intended to be an
interpretive guide for the application of DO-178B/ED-12B, Software
Considerations in Airborne Systems and Equipment Certification, to non-airborne
CNS/ATM systems. DO-178B/ED-12B defines a set of objectives that are
recommended to establish assurance that airborne software has the integrity
needed for use in a safety-related application. These objectives have been
reviewed, and in some cases, modified for application to non-airborne CNS/ATM
systems.
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Issued
3-5-02 s Prepared by SC-188
This document contains Minimum Aviation System
Performance Standards (MASPS) for communications utilizing High Frequency Data
Link systems for the air-ground communications sub-network in an Aeronautical
Telecommunications Network (ATN) environment. The FANS 1/A data link
environment is also addressed. Where systems are global in nature, the system
may have international applications that are taken into consideration.
Compliance with these standards is recommended as one means of assuring that
the system and each subsystem will perform its intended functions(s)
satisfactorily.
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DO-276A, User Requirements for Terrain and Obstacle Data
Issued
8-3-05 s Prepared by SC-193
The
document is harmonized with ICAO SARPS and establishes EGM-96 as the required
gravity model for vertical reference systems.
It accommodates ICAO Annex 15, Aeronautical Information Services,
Amendment 33, and harmonizes the glossary with the latest ICAO annexes. Definitions, features, and attribute names
are now harmonized with DO-291, Interchange Standards for Terrain, Obstacle,
and Aerodrome Mapping Data. It
simplifies the definition of obstacles and terrain and mandated geographical
coordinates. New additional data as well
as time stamps, effectivity, lighting, and marking attributes accommodate user
requirements and insure compliance with the ISO 19000 series. User feedback is added to the list of
verification and validation methods.
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Issued
10-12-01 s Prepared by SC-196
This document
contains Minimum Operational Performance Standards (MOPS) for the aviation
night vision imaging system (NVIS) used to supplement night VFR operations.
NVIS consists of the night vision goggle, interior and exterior lighting,
cockpit transparencies and crew station design and components. Performance and
test procedures are provided for the night vision goggle and lighting. A
section on continued airworthiness contains guidance to ensure the integrated NVIS
equipment installation continues to meet the minimum performance standard once
in operational use.
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DO-274, Next Generation
Air/Ground Communications (NEXCOM) Principles of Operation
Issued
10-12-01 s Prepared by SC-198
This document characterizes the principles of
operational use of integrated digital air/ground voice and data systems in the
domestic National Airspace System (NAS). Ideas presented are intended to
provide a framework for NAS communications subsequent to 2010. NEXCOM
operational objectives, intentions and capabilities are found in section three
and form the basis for success criteria used to determine system acceptability.
Section four describes the operational communications services to be used for
Air Traffic operations. Operational Scenarios are included that describe how
air traffic operations are supported. Section five characterizes the
environment within which NEXCOM is expected to operate.
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DO-273,
Response to the Report of the RTCA Chairman’s Committee on NEXCOM
Issued 10-12-01 s Prepared
by SC-198
In response to a request from the FAA, the RTCA
Chairman’s Committee produced a NEXCOM report that identifies issues attendant
with transitioning Air Traffic Control communications to a digital voice and
data communications system. The Chairman’s Report, completed in August 2000,
provides observations and recommendations that highlight the need for a systems
approach in addressing issues of spectrum, policy, procedure, acquisition,
certification, training, facilities, and maintenance. This document reports
the actions being taken by the FAA, SC-198, and the NEXCOM Aviation Rulemaking
Committee that address these observations and recommendations.
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DO-272B, User Requirements for
Aerodrome Mapping Information
Issued 04-14-09
s Prepared by SC-217/EUROCAE WG-44
There
are a large number of avionics systems in use today that implement DO-272A and
DO-291 requirements. Additional
equipment in the design phase, including airport moving map systems, need
aeronautical information in addition to the current published RTCA
documents. This information includes additional data and specifications
on terrain and airport information. To satisfy this need DO-272B is published
to:
·
Include
requirements listed in ARINC 816-1.
·
Include
requirements listed in AIXM5.0 for Airport Data for all features &
attributes, and numerical requirements that have a positive industry business
impact.
·
Make
editorial corrections.
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Issued 11-8-05 s Prepared by SC-172
DO-271C provides verification procedures for an
aircraft Very High Frequency (VHF) Digital Link (VDL) Mode 3 Transceiver used
for air-ground (A/G) voice and data communications. This revision includes updates based on
changes to RTCA DO-224B, Signal-in-Space
Minimum Aviation System Performance Standards (MASPS) for Advanced VHF Digital
Data Communications Including Compatibility with Digital Voice Techniques,
and includes errata and vocoder test vectors.
This document supersedes
DO-271B.
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Issued
10-12-01 s Prepared by SC-165
The document provides Minimum Aviation System
Performance Standards for data communications utilizing aeronautical mobile
satellite systems for the air-ground communications subnetwork in an
Aeronautical Telecommunications Network (ATN) environment. The document focuses
on data versus voice and covers a broad range of satellite systems to include
the current and next generation satellites. The FANS 1/A data link environment
is also addressed. Where systems are global in nature, the system may have
international applications that are taken into consideration. Communications
supporting the Air Traffic Service (ATS) and Aeronautical Operational Control
(AOC) may be provided by one or more satellite systems, each of which has
particular operating characteristics. This document anticipates that the
system-specific attachment(s) will provide one means of assessing whether a
particular AMS(R)S system is appropriate for a specific operational
environment. The requirements for operational environments are consistent with
DO-264.
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Issued 04-14-09 s Prepared
by SC-215
Communications supporting the Air Traffic Service
(ATS) and Aeronautical Operational Control (AOC) may be provided by one or more
satellite system, each of which has particular operating characteristics. Change 1 to DO-270 - Minimum Aviation System Performance
Standards (MASPS) for the Aeronautical Mobile-Satellite (R) Service (AMS(R)S)
as Used in Aeronautical Data Links provides a system specific description of the Iridium Satellite communication system
configuration including Ground Sub-networks; Iridium Satellite Sub-networks, of
which the Aircraft Earth Station (AES) is one part; and Aircraft Sub-networks. The
minimum system performance standards in Change 1 address only the Satellite
Sub-network.
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Issued
6-12-01 s Prepared by SC-194
This document proposes nine integrated service concepts
identified from a wide list of potential services. The integrated service
concepts were selected as those that may yield attractive benefits to all
stakeholders through integration of Aeronautical Data Link System (ADLS) with
airborne systems and/or ground automation. The services are Basic Information
Exchange: 1) FMS-ATM-AOC Calibration; 2) NAS Status Information; 3) UPT Flight
Planning/ Re-planning; 4) Flexible Arrival and Departure Routing; 5) Surface
Movement; Reduced Separation; 6) Non-radar Environment; 7) Radar Environment;
Communications Management; 8) Automatic Voice Frequency Change; and 9)
Emergency Notification.
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DO-268,
Concept of Operations, Night Vision Imaging System for Civil Operators
Issued 3-27-01 s Prepared
by SC-196
This document describes the concept of operations
supporting the implementation of aviation night vision imaging system (NVIS)
technology into the National Airspace System by civilian aviation
operators. Terminology, capabilities, limitations
and operations for NVIS are discussed as well as training and supporting
agencies. The focus of the document is the safe and efficient implementation of
NVIS during various phases of flight.
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Issued
04-29-04 s Prepared by
SC-195 Supersedes DO-267
The revised MASPS removes the binary
test data sets and establishes a publicly accessible FIS-B Product Registry
that facilitates coordination and publication of specifications for Application
Protocol Data Unit Payload encoding of new FIS products.
The document contains the MASPS for
FIS-B, an automated, digital data link system that provides timely access to
data link updates of non-control, advisory information needed by pilots to
operate safely and efficiently in the National Airspace System and in
international airspace.
It supports
interoperability between providers of ground and airborne FIS processing
systems by defining a broadcast protocol that may be used in any broadcast medium (i.e., VHF, satellite). The FIS-B broadcast network
organization consists of a physical layer, an International Standards
Organization (ISO) standard-based Data Link Services (DLS) layer, a Network
layer, a FIS-B Application Service Element (ASE), and a FIS-B Application. The physical layer is supplied by the
manufacturer with all the other layers and/or elements defined in the MASPS.
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DO-266, Government and
Industry Guidelines and Concepts for NAS Analysis and Redesign
Issued 12-14-00 s Prepared
by SC-192
This document consists of three volumes. “Volume I: User
Priorities for the National Airspace Redesign” is a summary of user comments
from six recent meetings held throughout the
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DO-265,
Minimum Operational Performance Standards for Aeronautical Mobile High
Frequency Data Link (HFDL)
Issued 12-14-00 s Prepared
by SC-188
This document encompasses standards and descriptions of
a system configuration including Ground Sub-networks; HF Data Link
Sub-networks, of which the aircraft is one part; and aircraft Sub-networks.
However, the specified MOPS in this document address only the aircraft HF Data
Link Sub-network function.
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Issued
12-14-00 s Prepared by SC-189
This document provides guidance material intended for
stakeholders and approval authorities involved in the operational
implementation of the provision and use of air traffic services (ATS) supported
by data communications. These communication services include those such as
communication management and clearances; navigation services such as flight
planning, required navigation performance (RNP) monitoring and gross navigation
error (GNE) prevention and detection; surveillance services such as position
and intent reporting; and services that support ATM automation.
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DO-263, Application of
Airborne Conflict Management: Detection, Prevention, & Resolution
Issued 12-14-00 s Prepared
by SC-186
This document presents an operational concept for the
Application of Airborne Conflict Management (ACM) using Automatic Dependent
Surveillance-Broadcast (ADS-B). The ACM concept includes detecting conflicts,
monitoring for potential conflicts and suggesting resolutions to prevent a
violation of airspace separation criteria against all other properly equipped
aircraft/vehicles. ACM is a core enabling function for the global
implementation of the Free Flight concept, as it will aid pilots to fly
user-preferred trajectories while avoiding conflicts with other aircraft.
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Issued
12-16-08 s Prepared by SC-215
This document contains Minimum Operational
Performance Standards (MOPS) for avionics that provide Aeronautical Mobile
Satellite (R) Services (AMS(R)S) by means of satellite communications
technologies. Each of these technologies is individually and collectively referred
to as a "Next Generation
Satellite System" (NGSS).
Iridium Satellite Normative Appendix: This normative appendix provides
Iridium-specific technical requirements and information regarding the technical
characteristics of an Aircraft Earth Station (AES) operating over the Iridium
satellite network for the purpose of providing Aeronautical Mobile Satellite
(Route) Service or AMS(R)S. The
International Civil Aviation Organization (ICAO) and International
Telecommunications Union (ITU) reserve the designation "(Route)" for
services related to the "safety and regularity of flight along national
and international air routes."
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DO-261, NAVSTAR GPS L5 Signal Specification
Issued 12-14-00 s Prepared
by SC-159
This Specification defines the requirements related to
the signal interface between the Space Segment (SS) of the Global Positioning
System (GPS) and the GPS Navigation Users for the L5 Navigation Signal.
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Issued 12-02-09 s Prepared
by SC-186
This
document contains Minimum Operational Performance Standards (MOPS) for airborne
equipment for Automatic Dependent Surveillance – Broadcast (ADS-B) and Traffic
Information Service – Broadcast (TIS-B) utilizing 1090 MHz Mode-S Extended
Squitter (1090ES). Compliance with these
standards by manufacturers, installers and users is recommended as one means of
assuring that the equipment will satisfactorily perform its intended functions
under conditions encountered in routine aeronautical operations.
This
revision supersedes DO-260A and incorporates the earlier Changes 1 and 2. FAA Technical Standard Order (TSO) C-166b
references this document.
The
document was developed in parallel with DO-282B.
Changes…only
for the revised DO-260B:
•
Added second NIC Supplement to encode a radius
of containment for less than 0.3 nautical mile
–
Moved
the Single Antenna Flag from Airborne Position Messages to Aircraft Operational
Status Messages
–
Replaced
the Single Antenna Flag in Airborne Position Message bit position with a new
NIC Supplement bit
•
Additional
NIC values are encoded for Surface Position Messages using additional NIC
Supplement bit in the Aircraft Operational Status Message transmitted only when
on-the-Ground
•
Test
Message that previously conveyed Mode A Code is no longer transmitted
•
Emergency/Priority
Message was modified to add the Mode A Code and is transmitted continuously
instead of only during an emergency condition
–
Mode
A Code 10008 terminates transmission of Emergency/Priority Message
so message is transmitted only when an emergency condition exists
-
Transmit
rate is 0.2 Hz except it increases to 1.25 Hz for 24 seconds when the Mode A
Code is changed
•
Quantization
of lower values of Surface Movement field in Surface Position Message changed
to add a value denoting “stopped”
–
“Stopped”
is transmitted when the criteria for “low” squitter rate is met
–
This
was done in response to surface application development to support alerting
application requirements on the surface
•
NACV
is now transmitted when on the surface as well as when airborne
•
Target
State and Status Message was modified:
–
New
subtype for the Target State and Status Message because of the modified format
(for backward compatibility)
–
Incorporated
newly defined fields and eliminated emergency/priority and TCAS RA active
subfields
•
TCAS
Resolution Advisory (RA) Message transmitted when a TCAS RA is active providing
data on the RA
–
Transmitted
at a 1.25 Hz rate during and immediately following an active RA
·
Receiver
requirements changed to add requirements to output ADS-B Reports on Version 0,
Version 1 and Version 2 receptions as well as ADS-R Reports on Version 1 and
Version 2 receptions
·
Requirements
added to receiver to support duplicate ICAO 24 bit address detection
·
Modified
CPR Reasonableness Test range criteria when airborne and surface states are
different
·
Type
Code Zero transmission modified so that only Position Messages are transmitted
with Type Code Zero
·
Time
Mark processing modified to handle the case when Time Mark does not occur at the start of the UTC second
·
Receiver
upper limit of dynamic range changed from -20 dBm to 0 dBm to improve aircraft
to aircraft minimum distance from over 500 feet to 50 feet
Changes
common to both the revised DO-260B and DO-282B:
•
Eliminated
the Following Fields
–
Receiving
ATC Services (set to reserved)
–
CDTI
Traffic Display Capability
–
IFR
Capability Flag
–
Position
Offset Applied
–
Surveillance
Integrity Level
•
Newly
defined Source Integrity Level is considered equivalent for backward
compatibility with Version 1 receivers)
–
Barometric
Altitude Quality
•
Added
the Following Fields
–
Lateral
and Longitudinal GPS Antenna Offset
•
Encoding
includes a value denoting GPS Antenna Offset has been applied by GPS position
source
–
Integrity
Fields replacing Version 1 Surveillance Integrity Level
•
Source
Integrity Level
•
System
Design Assurance (SDA) Level
•
Source
Integrity Level Supplement
–
1090ES
IN (indicates 1090ES Receive capability)
–
UAT
IN (indicates UAT Receive capability)
–
Geometric
Vertical Accuracy
•
Modified
the Following Fields
–
Aircraft/Vehicle
Length and Width Code modified to add encoded value for “No Data” condition
–
TCAS
Operational
–
NIC
encoding for a radius of containment of less than 0.3 nautical miles added
•
Mode
A Code required to be broadcast when on-the-Ground as well as Airborne
•
Removed
vertical component of NIC, SIL, NACP and NACV
•
Target
State Data has been modified
–
Eliminated
Target Altitude and Target Heading and replaced them with Selected Altitude,
Selected Heading and Barometric Pressure Setting
–
Mode
Bits modified
•
Added
requirements for position source selection
•
Incorporated
an equipage class for single antenna aircraft
•
Modified
the receiver dynamic range requirement for reception from aircraft as close as
50 feet to better support surface applications
The document
is available as an electronic download.
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Issued
09-13-00 s Prepared by SC-186
This document
contains the Minimum Operational Performance Standards (MOPS) for airborne
equipment for Automatic Dependent Surveillance-Broadcast (ADS-B) utilizing
1090MHz Mode-S extended squitter. ADS-B
is a system for aircraft or surface vehicles, operating within the airport
surface movement area, that periodically transmits its state vector (horizontal
and vertical position, horizontal and vertical velocity) and other information.
This
MOPS describes typical equipment applications and operational goals and along
with DO-242, Minimum Aviation System
Performance Standards for ADS-B, forms the basis for the recommended
performance standards and test procedures.
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Change 1 to DO-260, Minimum Operational Performance Standards for 1090
MHz Automatic Dependent Surveillance – Broadcast (ADS-B)
Issued
06-27-06 s Prepared by SC-186
Change
1 prescribes the changes to DO-260 required for those manufacturers that
produce 1090 MHz equipment for broadcast-only that comply only with
DO-260. It provides additional changes
to the changes which first appeared in Section 1 of the Appendix of FAA TSO
C166, which has been removed from the draft of TSO C166A. Manufacturers that produce 1090 MHz equipment
which will include the ADS-B receive capability must comply with DO-260A,
Change 1 and the latest available version of FAA TSO C166. Change 1 provides
changes for the Air/Ground Determination and its recommended test procedures,
and for the definition of how to encode Navigation Uncertainty Category (NUC)
if the Horizontal Protection Limit (HPL) is not available. Direction is provided for deleting the
Aircraft Trajectory Intent Massages and Aircraft Operational Coordination
Messages. The requirements for the
optional transmission of the ADS-B TEST Message (TYPE Code =23) for transmitting
the Mode 3/A (4096) Code in the
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Issued
9-13-00 s Prepared by SC-186
This document provides a preliminary description of four
potential applications utilizing a CDTI that may enhance current air traffic
operations, describes underlying pilot and controller tasks and
responsibilities, and derives required CDTI capabilities that enable the pilot
to perform these tasks. The application definitions provide sufficient detail
to allow a specification of required CDTI capabilities, so when the
applications are fully developed, tested and evaluated, and certified for use,
the equipment may be capable of facilitating the implementation.
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DO-258A,
Interoperability Requirements for ATS Applications Using ARINC 622 Data
Communications
Issued 4-07-05 s Prepared
by SC-189 Supersedes DO-258 s Errata
Issued 01-11-08
This update aligns the scope of interoperability
requirements for the FANS 1/A technology with the Continental SPR Standard
(DO-290) to include interoperability for interface with HF Data Link (HFDL).
The document, initially issued in September 2000, defines interoperability
requirements for communication services and Air Traffic Services (ATS) applications
and allocates these requirements to stakeholders. It covers: the ATS Facilities
Notification (ATN) application, the Automatic Dependent Surveillance (ADS)
application, the Controller Pilot Data Link Communication (CPDLC) application
and the ARINC data communication.
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Issued 6-25-03 s Prepared
by SC-181
Supersedes DO-257
DO-257A supports the electronic
depiction of airport surface situation awareness (SA) maps and vertical
situation awareness displays. The revision includes requirements and guidelines
for the electronic depiction of airport surface diagrams, ownship, ground path
and vertical profile aspects of the display and associated controls. Two new Sections were added: Section 2.3 -
Aerodrome Moving Map Display (AMMD) and Section 2.4 - Vertical Situation
Awareness Displays (VSAD). Consensus was
reached on hazard
classifications by removing the Major
hazard classification for airborne display from the document. It is understood that a FAA Technical
Standard Order referencing DO-257A will further address hazard classifications.
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Issued 6-20-00 s Prepared
by SC-194
DO-256 defines minimum human factors requirements and
guidelines for air traffic services (ATS) data link communications between air
traffic specialist and a pilot utilizing Aeronautical Telecommunications
Network (ATN). The scope is the initial Controller-Pilot Data Link
Communications (CPDLC) capabilities, which comprise the Build I and Build IA
phases of the
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DO-255,
Requirements Specification for Avionics Computer Resource (ACR)
Issued 6-20-00 s Prepared
by SC-182
DO-255 provides the Requirements Specifications for the
Avionics Computer Resource (ACR) intended to facilitate certification
efficiency and economy of scale for the computer platform. These Requirements
Specifications define a computer platform suitable for hosting multiple,
independent software applications and are seen as an enabling step towards
standardized, re-usable avionics software applications.
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DO-254,
Design Assurance Guidance for Airborne Electronic Hardware
Issued 4-19-00 s Prepared
by SC-180
This document is intended to help aircraft manufacturers
and the suppliers of aircraft electronic systems assure that electronic
airborne equipment safely performs its intended function. The document
identifies design life cycle processes for hardware that includes line
replaceable units, circuit board assemblies, application specific integrated
circuits (ASICs), programmable logic devices, etc. It also characterizes the
objective of the design life cycle processes and offers a means of complying
with certification requirements.
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Issued 12-16-08 s Prepared by SC-159
This document provides the Minimum Operational
Performance Standards (MOPS) for Airborne Navigation Equipment Using the Global
Positioning System (GPS) Augmented by the Local Area Augmentation System
(LAAS). The standards in the document define minimum performance requirements,
functions, and features for LAAS airborne equipment to support CAT I, II and
III precision approach operations. Compliance with these standards by
manufacturers, installers, and users is recommended as a means of assuring that
the equipment will satisfactorily perform its intended functions under
conditions encountered in routine aeronautical operations. DO-253A superseded
DO-253 and included: 1) Recommendations harmonized with the ICAO GNSS Panel
Standards and Recommended Practices (SARPs), 2) The use of LAAS differential
position to support area navigation, and 3) The easing of the LAAS Ground
Subsystem Siting constraints (Ephemeris Error Protection). DO-253B harmonized the
LAAS MOPS with the revised WAAS MOPS - DO-229D. DO-253C
includes the earlier revisions and provides the requirements / standards for
LAAS to support Cat. II and III precision approaches. In addition, the revision incorporates
changes to existing Cat. I and positioning service standards, and includes
velocity requirements to further support ADS-B.
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DO-252, Minimum
Interoperability Standards (MIS) for Automated Meteorological Transmission
(AUTOMET)
Issued
1-11-00 s Prepared by SC-195
This document specifies a set of encoding and decoding
rules to apply to the message format types found in the document. Message
formats are independent of media and protocols used to transfer encoded AUTOMET
messages. AUTOMET operational requirements are not explicitly specified. This
standard ensures that all AUTOMET-compliant air- and ground-based systems will
be able to decode and interpret AUTOMET uplink and downlink messages.
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Issued 1-11-00 s Prepared
by SC-194
The "Plan" document captures the work of the
data link issues team from which SC-194 evolved. This publication documents the
aviation community's consensus on the evolution and implementation path for Air
Traffic Services via data link utilizing the ATN in the U.S. National Airspace
System.
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Issued 1-11-00 s Prepared
by SC-194.
The Aeronautical Data Link System will be incrementally
deployed to leverage existing and evolving technology investments and
emphasize newly developed procedures in the initial steps. This publication
includes sections on infrastructure, procedural
requirements, data link services, and operational scenarios.
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Issued 10-6-99 s Prepared
by SC-186
This planning Guide outlines suggested activities for
the development and implementation of ADS-B applications. It documents the
range of activities that need to be in place to bring an application from an
initial concept to operational use.
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Issued 10-12-01s Prepared
by SC-190 Supersedes DO-248A
DO-178B was published December 1, 1992. Since that date
the aviation community has gained experience using the document and has raised
a number of questions regarding the document’s content and application. DO-248B
includes the material from the Second Annual Report, DO-248A, and adds new
Frequently Asked Questions and Discussion Papers resulting from the committee’s
review of over 330 issues.
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Issued 1-7-99 s Prepared
by SC-159
The report presents material on airport surface
operations and relates it to the use of GNSS. It is intended that the report
provide background information for airport operators/users and equipment
suppliers on the role of GNSS to support airport surface operations, and to
provide guidance for the further development of performance standards. The
report culminates with conclusions pertaining to the use of GNSS for airport
surface operations and identifies issues requiring further study.
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DO-246D,
GNSS Based Precision Approach Local Area Augmentation System (LAAS) –
Signal-in-Space Interface Control Document (ICD)
Issued 12-16-08 s Prepared by SC-159 Supersedes DO-246C
DO-246D includes the earlier document revisions and incorporates
the standards for LAAS to support Cat. II and III precision approaches. DO-246C included
changes to harmonize the document with DO-245A, LAAS MASPS. The three primary areas of change were:
1. Definition of additional data for supporting Cat. II/III
precision approach operations [Additional data blocks 3 and 4 for Message Type
2].
2. Definition of LAAS uplinked Terminal Area Paths (TAP)
data for supporting additional Terminal Area Procedures [Provisions for TAP
data to be included in Message Type 4].
3. All references to pseudolites / Ground Based Ranging
Sources were removed.
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DO-245A, Minimum Aviation
System Performance Standards for Local Area Augmentation System (LAAS)
Issued 12-09-04 s Prepared by
SC-159 Supersedes DO-245
This
document contains the Minimum Aviation System Performance Standards for the
Local Area Augmentation System (LAAS), a system developed to support precision
approach and landing operations and other navigation and surveillance
applications, within a local area including and surrounding an airport.
This
revision harmonizes the LAAS requirements for supporting Category I operations
and the LAAS differential positioning service with the LAAS MOPS [DO 253A] and
the ICAO Annex 10 GBAS SARPs through Amendment 79. The requirements to support LAAS Category II
and III precision approach operations are added/updated as well as requirements
for the LAAS when supporting complex terminal procedures through the broadcast
of Terminal Area Path (TAP) data using the LAAS VHF Data Broadcast (VDB).
Note: Readers
should be aware that DO-245A has not yet been updated to be consistent with the
current evolution of LAAS requirements.
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DO-244, Government/Industry
Guidelines and Concept for National Airspace Analysis and Redesign
Issued 6-8-98 s Prepared
by SC-192
This document contains two volumes - Volume I, entitled A Concept Document for the Optimization of
the NAS Airspace Structure, presents concepts for a national airspace
assessment and redesign that addresses significant changes to matters
pertaining to the national airspace by the year 2005. Volume II, entitled Guidelines for Conducting Airspace Analysis,
contains the general guidelines for airspace analysis, including metrics,
modeling, and data requirements.
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DO-243, Guidance for Initial
Implementation of Cockpit Display of Traffic Information
Issued 2-19-98 s Prepared
by SC-186
This document provides manufacturers a set of guidelines
in the design and development of an initial set of Cockpit Display of Traffic
Information (CDTI) features. CDTI is the function of presenting surveillance
information about the surrounding traffic to the flight crew. This guidance
document is advisory in nature and its contents are expected to be a subset of
the final CDTI MOPS. That MOPS, when published, will replace this document. In
order to comply with certification standards, manufacturers will be required to
demonstrate that 1) CDTI meets its intended functions, and 2) CDTI does not
interfere with any other aircraft systems. This interim guidance provides a
description of the intended functions of CDTI and as such may aid the
certification process.
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Issued
6-25-02 s Prepared by SC-186
Supersedes DO-242
This document supersedes DO-242 and provides an
up-to-date view of the system-wide operational use of ADS-B. This revised ADS-B MASPS concentrates on four
major areas of development: 1) Separating the accuracy and integrity components
of the Navigation Uncertainty Category (NUC) into the new fields Navigation
Accuracy (NAC) and Navigation Integrity Category (NIC); 2) Reorganization of
the State Vector, Mode-Status, and On-condition reports; 3) Restructuring the
content and manner in which intent information is broadcast; and 4)
Clarification that system requirements at the MASPS level are based on
operational ranges and not particular applications.
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Issued 12-13-06 s Prepared
by SC-186
This change to DO-242A mainly clarifies the
definitions of several parameters transmitted by aircraft in
ADS-B messages. These parameters provide
information to the recipient of the ADS-B message about the quality of the
transmitted aircraft position. The change has been developed in a manner
that reflects typically available aircraft position sources and should not
impact ADS-B equipment previously certified using RTCA DO-260A for 1090 MHz
Extended Squitter or RTCA DO-282A for the Universal Access Transceiver (UAT).
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Issued 10-6-97 s Prepared
by SC-169
The document identifies information to be exchanged by
the ATM system and AOCs using automation and ground-ground communications. It
identifies information needed for both domestic and oceanic operations.
The information
presented extends beyond what is necessary for today's operation paradigm to
include requirements that will facilitate more user flexibility in the future.
Operational scenarios are included.
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Issued 7- 29-97 s Prepared
by SC-162
This document provides standards for Aeronautical
Telecommunication Network functions for aircraft systems and equipment. These
standards are in the form of performance criteria for ATN functions;
qualification criteria for demonstrating performance requirements;
descriptions of evidence that indicate that performance objectives have been
satisfied. Performance objectives, qualification and evidence are discussed as
they relate to satisfying the requirements for airworthiness approval of ATN
functions. The functions covered by the MOPS can be incorporated in a wide
variety of hardware configurations onboard an aircraft. Section 2 of the
document expresses the requirements for airborne ATN systems. Section 3
describes the means of qualification by providing an overview of the testing
process and listing detailed tests.
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Issued 4-2-97 s Prepared by SC-169
Errata Issued 10-17-97
This document presents requirements for the aircraft
equipment associated with Traffic Information Service Data Link (TISDL)
communications. The TIS data link function is intended to improve the safety
and efficiency of “see and avoid” flight by providing pilots with automatic
display of nearby traffic and warnings of any potentially threatening
conditions. The source of TIS information is the file of aircraft tracks
maintained by the ground Mode S sensor providing coverage for a region of
airspace. TIS generates alerts for any traffic aircraft in Mode S coverage that
carry a transponder (ATCRBS or Mode S). TIS provides traffic advisories similar
to those of TCAS-1, but does not provide resolution advisories. Section 1
provides information and assumptions needed to understand the rationale for
equipment characteristics and requirements. Section 2 contains the minimum
performance standards for the equipment. Section 3 describes the performance
required of the installed equipment and Section 4 describes the operational
performance characteristics for equipment installations.
NOTE:
The electronic DO-239 is a pdf file but it is not in searchable format.
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DO-238, Human Engineering
Guidance for Data Link Systems
Issued 4-2-97 s Prepared by SC-169
This document sets forth general, functional,
procedural, and design criteria and recommendations concerning human
engineering of data link systems. The document focuses primarily on
recommendations for data link communications between an air traffic specialist
and a pilot. The document is intended as a guide for the development and
evaluation of data link systems.
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DO-237, Aeronautical Spectrum
Planning for 1997- 2010
Issued 1-27-97 s Prepared by SC-185
The report examines aeronautical Communications,
Navigation, and Surveillance (CNS) services to determine the spectrum
requirements of existing and planned new systems. It represents a major effort
by the aeronautical community to assess “the state of the spectrum” as
requirements change and new technologies are introduced.
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Issued 10-28-03 s
Supersedes DO-236A s Prepared by SC-181
This
document supersedes RTCA DO-236A, Minimum
Aviation System Performance Standards: Required Navigation Performance for Area
Navigation, published in
September 2000.
Special Committee 181 added two new Appendices to DO-236B:
-
Appendix
H, Temperature Compensation Information
-
Appendix
I, RNP RNAV Less Than 0.3NM
Paragraph
3.2.8.6, Temperature Compensation, is updated with additional notes based upon
the new material in Appendix H.
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DO-235B, Assessment of Radio
Frequency Interference Relevant to the GNSS L1 Frequency Band
Issued 03-13-08 s Prepared by SC-159
Supersedes DO-235A
This
document supersedes DO-235A. It departs from the previous assessment
reports by characterizing the “external” (non-aeronautical) Radio Frequency
Interference (RFI) as an aggregate effect. Terrestrial RFI sources are
modeled as being distributed to the radio horizon for the Global Navigation
Satellite System (GNSS) aircraft antenna. On-board non-aeronautical RFI is
also characterized as an aggregate effect from multiple sources distributed
throughout the passenger cabin. Explicit location-dependent GNSS inter-
and intra-system RFI power spectral density values are computed based on
“critical-satellite” configurations for a 30-satellite GPS constellation.
RFI components for new Space Based Augmentation System (SBAS), Quasi-Zenith Satellite System (QZSS) and Galileo
satellite constellations are also determined. Receiver MOPS RFI test
condition modifications are proposed to better address the composite
aeronautical and non-aeronautical RFI environment for certain flight phases and
operations. New potential RFI sources (Mobile
Satellite Service ancillary terrestrial component terminals, GPS
re-radiators) are discussed. Other potential RFI sources are reviewed and
a set of RFI mitigations discussed.
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DO-234, Minimum Performance
and Installation Standards for Runway Guard Lights (RGLs)
Issued 11-15-96 s Prepared
by SC-184
This document contains minimum performance and
installation standards for elevated and in-pavement runway guard lights (RGLs).
These standards provide guidance to designers, installers, manufacturers,
service providers and users of these lights. RGLs are used to enhance the
conspicuity of the runway holding position at airports and are useful for low
visibility operations, situational awareness by pilots and vehicle drivers, and
runway incursion prevention.
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DO-233, Portable Electronic
Devices Carried on Board Aircraft
Issued 8-20-96 s Prepared by SC-177
Errata Issued 8-18-99
This document addresses the potential interference to
installed aircraft electrical and electronic systems from Portable Electronic
Devices (PEDs) carried aboard by passengers. It defines the potential interference
phenomena; outlines the risk potential from interference events; provides test
methods to determine whether or not a potential for interference exists for
certain PEDs, aircraft and combinations thereof; and addresses acceptable
levels of interference. The report also recommends modification of Federal
Aviation Regulation 91.21, continued PEDs testing to identify and better define
the possibility of interference to aircraft electronic systems, increased
public awareness of the potential for interference from PEDs, and the
development and use of devices to detect spurious PEDs emissions.
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DO-232, Operations Concepts
for Data Link Applications of Flight Information Services
Issued 3-13-96 s Prepared by SC-169
This document provides the framework for development of
future FIS data link systems and associated MOPS. The document is designed to:
present the user’s perspective of operational concepts and system
characteristics for FIS data link applications; identify, describe, and
prioritize the FIS data link products and services needed to support both
current and future flight operations in the National Airspace System, including
international oceanic operations; identify infrastructure barriers to
successful implementation and utilization of the priority FIS products.
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Issued 3-13-96 s Prepared by SC-165
This document contains functional and interface
requirements for the implementation and use of Aeronautical Mobile Satellite
Service (AMSS) voice communications in an environment where satellite voice is
a required capability. The information contained herein describes satellite
voice services in the Air Traffic Management (ATM) and Aeronautical Operational
Control (AOC) environments-including requirements for aircraft installations,
satellite services, ground interconnection facilities, and Air Traffic Service
facility capabilities. The scope of this document is focused primarily on the
use of satellite voice in Oceanic and Remote airspace areas.
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DO-230B, Integrated
Security System Standard for Airport Access Control
Issued 06-19-08 s Prepared by SC-207
This
document supersedes DO-230A, "Standards for Airport Security Access
Control Systems," originally published in 2003. It provides standards and guidelines for
implementing access control systems in the context of
an Integrated Security System for an Airport.
The document provides guidance on acquiring and designing such
systems, testing and evaluating system performance, and operational
requirements. The document incorporates
the latest technological advances in security access control systems and
identity management technologies, including smart cards and biometrics. The major areas covered are: system level
requirements, identity management requirements, physical access control
requirements, video surveillance requirements, security operating center
requirements, intrusion detection requirements, communications infrastructure
requirements and general procurement level guidance.
The
document indicates not only what are the current best practices and system
requirements to meet the current regulatory requirements, but also provides
guidance for those airports who wish to go beyond these requirements, and
provides guidance for what the committee believes are logical
and reasonable methods for implementing the advances in security technology.
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DO-230A, Standards for Airport
Security Access Control Systems
Issued 4-10-03 s Prepared by SC-199 Supersedes
DO-230
This document updates RTCA DO-230, Standards for Airport Security Access
Control Systems, originally published in 1996. Using the original DO-230
format, the document has been expanded into the following sections:Section
1 introduces the Access Control Systems (ACS), purpose, scope, goals, and
operational requirements. Section 2
provides guidance for system performance.
Section 3 addresses subsystem performance of access media and
hardware. Section 4 provides guidance
for system verification and validation.
The document also contains the three appendixes that provide guidance
and reference material: Appendix A provides detailed guidance on biometrics and
smart card technologies. Appendix B provides
reference examples of sample reports
commonly found in ACS. Appendix C
provides a list of acronyms and abbreviations used in the document. This material should be useful to airport
operators as a tool to assist in obtaining Airport Improvement Program (AIP)
funding.
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Issued 12-13-06 s Prepared
by SC-159 Errata Issued
07-31-08
This document
contains Minimum Operational Performance Standards (MOPS) for airborne
navigation equipment (2D and 3D) using the Global Positioning System (GPS)
augmented by the Wide Area Augmentation System (WAAS). The primary
areas of change from DO-229C to DO-229D are:
1. Clarifications: Numerous
changes have been incorporated to more clearly describe the meaning and intent
of the requirements. To accomplish this there have been changes in the
requirements text, explanatory notes added to clarify intent, or both.
2. Appendix Updates: Appendices
F and I from DO-229C have been deleted and replaced with entirely new
material. Appendix F now addresses SBAS capability considerations for
ADS-B. Appendix I now contains mode switching process flow diagrams to
aid in understanding the mode transition requirements.
There are three new appendices in DO-229D, Appendix S, Appendix T and
3. Corrections: There are
numerous changes in DO–229D to correct errors in equations and to update
references to other documents. For example, equations in several places
had incorrect signs, symbols, and/or nomenclature. Some of these errors
were noted in the errata sheet and TSO-C145a/C146a. The errors documented
by those sources have been incorporated; and, many additional errors were found
during the review.
Further, the update to DO-229D includes changes related to the changing
environment for GPS and service provider experience gained thru operating SBAS
systems. For example, the narrow-band geostationary satellites in the
WAAS system are in the process of being replaced with wide-band
satellites. A result is that major requirement changes have been incorporated
in DO-229D related to noise, minimum/maximum satellite power levels, and
antenna gains.
4. New Requirements: There are new requirements either
embedded within previously existing requirements from DO-229C, or, captured as
entirely new sections that never previously existed. Some examples are:
- There
is a new requirement for Fault Detection Prediction so that SBAS equipment
provides at least the same capability as TSO-C129a equipment when
operating outside of SBAS coverage.
- There
is a new GEO bias error requirement to account for the net group delay
through the receiver correlator that results from the signal bandwidth of
SBAS satellites compared to GPS satellites.
- There
is a requirement to only use weighted solutions for FDE algorithms.
Section 2.3 for Delta-class receivers has been extensively re-written
and expanded.
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GEO Bias Modeling Tool for
DO-229D
Issued 12-13-06 s Prepared
by SC-159
The GEO Bias tool is a MATLAB script. The GEO
Bias tool is intended to be used by the manufacturer to demonstrate that their GNSS receiver is
compliant with the GEO Bias requirements in DO-229D as described in section
2.1.4.1.5. Appendix T in DO-229D provides a description of this tool
and associated test procedure.
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Issued 11-28-01 s Prepared
by SC-159 Supersedes DO-229B Errata
Issued 8-16-02
This document contains Minimum Operational Performance
Standards (MOPS) for airborne navigation equipment (2D and 3D) using the Global
Positioning System (GPS) augmented by the Wide Area Augmentation System (WAAS).
DO-229C supersedes DO-229B and includes: 1) Message Type 28 information, 2)
Modification of the satellite tracking constraints, 3) Changes to the equipment
classifications and the accommodating document realignment, 4) Interference
environment revisions in Appendix C and 5) New GPS/Inertial requirements in
Appendix R. The regulatory application of these standards is the responsibility
of appropriate government agencies. In the
FAA Technical Standard Order (TSO) - C145 references this document.
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Issued 10-20-95 s Prepared
by SC-159
Defines the antenna performance for antennas that will
be used with GNSS receiver equipment. Contains Minimum Operational Performance
Standards (MOPS) for GNSS airborne antenna equipment designed to use GPS or
GLONASS augmented by other systems/equipment/techniques as appropriate to meet
the performance requirements for primary means of navigation for en route,
terminal, non-precision, and precision approach phases of flight. Incorporated
within these standards are equipment characteristics that should be useful to
users, designers, manufacturers, and installers of equipment.
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Issued 1-11-00 s Prepared
by SC-159
This change was developed in response to inputs from
antenna manufactures. Changes include references to RTCA DO-160D vice DO-160C,
updates minimum frequency range, axial ration, frequency selectivity
requirements, and differential group delay to insure airborne equipment is
protected by the LAAS and WAAS ground monitoring facilities during precision
approach operations.
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DO-227, Minimum Operational
Performance Standards for Lithium Batteries
Issued 6-23-95 s Prepared by SC-168
Contains both requirements and general guidelines
regarding the design, testing, application, handling, storage, and disposal of
lithium cells and batteries. It provides designers, manufacturers, and users of
equipment installed in aircraft with information on the performance
characteristics and operating and environmental limitations of lithium cells
and batteries powering such equipment. Two categories of maximum cell and
battery sizes are identified.
Category
I: Solid-cathode
cells that contain less than 0.15 grams of lithium or lithium alloy, and
batteries that use not more than four such cells.
Category
II: Liquid-cathode
cells that contain less than 0.15 grams of lithium or lithium alloy, or
batteries comprised of these cells. Cells that contain 0.15 to not more than 5
grams of lithium or lithium alloy. Batteries that contain not more than 25
grams lithium or lithium alloy. Cells containing more than 5 grams of lithium
or lithium alloy, or batteries that contain more than 25 grams of lithium or
lithium alloy are beyond the scope of this document.
FAA Technical Standard Order (TSO) – C97 references this document.
NOTE: The electronic DO-227 is a pdf file but it is
not in searchable format.
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Issued 5-25-95 s Prepared
by SC-171 Supersedes DO-198 (SC-151)
This document spans a decade of work by two RTCA Special
Committees (151/171). During this period, alternative technologies to the
Microwave Landing System (e.g., satellite navigation) have evolved. Yet the
need for precision, near-airport area navigation continues. Whatever the
navigation source for an operational capability, much of the material in this
document is germane to any precision, terminal-area navigation system. The
philosophy used in preparing the document was to provide guidance for any
terminal area navigation system, although the specific performance
requirements and test procedures assume the MLS Random (Area) Navigation (RNAV)
sensor inputs.
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Issued 11-17-94 s Prepared
by SC-172
This report
represents a broad study of very high frequency (VHF) air-ground communications
system
improvements. The study includes: (1) gaining an
understanding of the present VHF air-ground communications system, (2) developing
future Air Traffic Service (ATS) and Aeronautical Operational Control (AOC)
communications functional requirements and desirable features,
(3) studying present system improvements, (4) selecting a future system
candidate to pursue towards implementation, and (5) developing
recommendations resulting from this study. Seven candidate future system
alternatives were evaluated against future system requirements and desirable
features and as a result of this study, six recommendations to pursue present
and future system improvements were adopted.
NOTE:
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Issued 8-03-05 s Prepared by SC-172
This
final planned version of the VDL Mode 2 and Mode 3 MASPS consolidates previous
documents. It is synchronized with ICAO SARPS and Technical Manuals for VDL
Modes 2 and 3. Future updates to DO-281A, MOPS for VDL Mode 2, and
DO-271C, MOPS for VDL Mode 3, will be synchronized with DO-224B. Specific
changes include:
·
VDL
Mode 2 – minor updates
·
VDL
Mode 3 – aircraft address space is increased, the aircraft cross-link buss requirement
is removed, ground system requirements are added to accommodate changes, and clarifying definitions are added.
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DO-223, Minimum Operational
Performance Standards for Context Management (CM) Equipment
Issued 7-13-94 s Prepared
by SC-169
Identifies aircraft equipment requirements to support
the forwarding of addresses, such as “log-on”, between aircraft systems and
ground systems. Context management will support Air Traffic Service
communications, such as ATC Two-Way Data Link communications, Automatic
Dependent Surveillance, Flight Information Services, as well as satellite voice
and Aeronautical Operational Communications. Broadcast communications will
probably not use context management.
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DO-222,
Guidelines on AMS(R)S Near-Term Voice Implementation and Utilization
Issued 4-29-94 s Prepared
by SC-165 Errata Issued 6-21-94
Contains operational guidelines and recommendations for
the implementation and utilization of Aeronautical Mobile Satellite (Route)
Services, voice communication functions in the near-term (circa 1993-1996) air
traffic environment. It presents a system-level view of how satellite voice
services can be implemented and used in the Air Traffic Services (ATS) and
Aeronautical Operational Control (AOC) environments inclusive of aircraft
installation requirements, ground infrastructure requirements, and available
AMS(R)S services. This document defines the functions and performance needed to
facilitate the development, implementation, certification, and operational use
of satellite voice in an environment where satellite voice communication is not
yet a required capability for air navigation. It uses as its basis the existing
standards for satellite avionics and ground equipment. It should be useful to
designers, manufacturers, installers, and operators of equipment used in AMSS
voice service.
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DO-221, Guidance and
Recommended Requirements for Airport Surface Movement Sensors
Issued 4-29-94 s Prepared
by SC-178
Provides recommended standards for both sensor and
system characteristics. The primary purpose for these sensors is to operate
stop bars located on taxiways which provide entrance to low visibility runways.
The sensors may also be used for other low visibility functions such as taxiway
light sequencing, runway exiting notification, and presence detection. This
document provides guidance to airport system designers, manufacturers,
installers, and users.
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Issued 9-21-93 s Prepared
by SC-173 s Change 1 issued 6-23-95
Incorporates new radar technology and serves as a
standard for both air carrier and general aviation aircraft. It considers those
requirements and technologies pertinent to general aviation, where limitations
on space and/or weight apply. Compliance with these standards by manufacturers,
installers, and users is recommended as one means of assuring the equipment
will perform its intended function under conditions normally encountered in
routine aeronautical operations.
FAA Technical Standard Order (TSO) – C117a references this document.
NOTE:
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Issued 6-23-95
Change 1 adds new data contained within the NASA Windshear
Simulation Data Sets, standard deviation of rain velocities calculated by
AWDRS, and expanded explanatory notes to the data sets.
NOTE:
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searchable format.
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DO-219, Minimum Operational
Performance Standards for ATC Two-Way Data Link Communications
Issued 8-27-93 s Prepared
by SC-169
Presents the requirements for Two-Way Data Link
Communication (TWDL) services. TWDL services include predeparture clearance,
clearances, reports, and requests. In addition to testing standards, the
document includes functional, performance, interface, and equipment standards
for “ATCCOMM.” The term “ATCCOMM” as used in this document includes all
components and units, including software, necessary for the aircraft equipment
to support TWDL services with an ATC ground system peer via the Aeronautical
Telecommunications Network (ATN).
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DO-218B,
Minimum Operational Performance Standards for the Mode S Airborne Data Link
Processor
NOTE: DO-218B
was removed as an active document as of July 1, 2009. The RTCA Program
Management Committee recommended at their October 2, 2008 meeting that DO-218B
be retired. The requirements that remain
relevant, Appendices B and C, are retained in DO-181D.
Issued 8-27-93 s Prepared
by SC-159 s Change 1, Issued 7-13-94
Reprinted in
April 1995 to include Change 1
Provides the guidelines for a system to support
differential GNSS (DGNSS) special instrument approaches. Requested by the FAA
and consistent with the recommendations of the RTCA GNSS Task Force Report, the
recommended standards in this document are specifically oriented toward
supporting Special Category I precision approaches - specially authorized approaches
made to MLS/ILS Category I minima with DGNSS used to provide navigation
guidance. These approaches are expected to be authorized for specific aircraft
approaching specific airports; thereby, providing the civil aviation community
the basis for developing precision approaches using satellite technology.
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Note: For those
who currently possess a copy of DO-217 printed before April 1994, the following
change may be purchased separately. The prices above reflect the inclusion of
Change 1 into the body of the document.
Issued 8-13-94
Replaces the original Appendix F with one method of
implementing the differential message format described in Appendix A, using VHF
data link. The data link characterized is more robust and may provide growth
potential for Category II/III precision approaches. This change is included in
the April 1995 printing of DO-217.
NOTE:
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Change 2 to DO-217, Minimum Aviation System Performance
Standards DGNSS Instrument Approach System: Special Category 1 (SCAT-1)
Issued 11-15-96
This document recognizes the technology developments
since the original issuance of DO-217 in August 1993. While RTCA/DO-217
including this change does not guarantee interoperability with a future GNSS
CAT-I system, this change does address interoperability among SCAT I systems
and provides a means to improve interoperability.
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DO-216, Minimum General
Specification for Ground-Based Electronic Equipment
Issued 7-14-93 s Prepared
by SC-175
Contains general specification for the procurement of
ground-based electronic equipment by the Federal Aviation Administration. This
material incorporates industry standards to facilitate use of Commercial Off
The Shelf/Non-Development Items (COTS/NDI). This updated Version Downloadable
of FAA Standard G-2100e also contains revised quality assurance provisions and
is expected to be used as a key element in FAA future procurement.
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DO-215A, Guidance on
Aeronautical
Issued 2-21-95 s Prepared
by SC-165 Supersedes DO-215
This document contains guidance for the system and
service requirements performance, availability, and integrity for an End-to-End
System providing Aeronautical Mobile Satellite Services (AMSS) to end users.
The primary elements of the End-to-End System are also
considered individually. The material should be useful to users, designers,
manufacturers, and installers of the AMSS system and its elements.
NOTE:
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Issued 9-28-98
DO-215 originally published May 1993, was updated as
DO-215A in February 1995. It offers the only currently published guidance for
performance, integrity, and availability for data and voice over end-to-end
links and their individual subsystems. New AMSS development activities in
industry and government require criteria for establishing their feasibility and
acceptability. DO‑215A is in widespread use in those regards, and will
fill those needs until a new AMSS MASPS is available. This change provides
needed clarifications and corrections required for applying DO-215A
methodologies to an evolved geo-stationary satellite communications system.
NOTE:
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searchable format.
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Issued 3-2-93 s Prepared
by SC-164 Supersedes DO-170
This document defines audio systems response
characteristics that affect the intelligibility of air-ground speech
communication including review and evaluation of design measures giving promise
of audio response characteristics. It recommends a means for improvement by
users and designers of communications equipment. In addition to postulating
goals and applications, it recommends minimum standards and test procedures for
aircraft microphones (except carbon), aircraft headsets, handsets and
loudspeakers, and aircraft audio systems.
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DO-213, Minimum Operational
Performance Standards for Nose-Mounted Radomes
Issued 1-14-93 s Prepared
by SC-173 s Change 1 issued 6-23-95
Contains minimum operational performance standards for
radomes for use with airborne doppler weather radars having forward-looking
windshear detection capability and for use with airborne weather radars.
T
hese standards specify radome characteristics for
designers, manufacturers, installers, and users of the equipment.
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Issued 6-23-95
Change 1 adds definitions for “Transmission Efficiency,
Minimum,” and “Transmission Efficiency, Average.” The change also includes new
material in Section 2.1.5, Maintenance Performance Rules and Section 2.1.6,
Documentation and Identification; redefines “Side Lobe Upper Limits.
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Issued 10-26-92 s Prepared
by SC-170
Addresses application of the ADS function and recommends
standards for Automatic Dependent Surveillance (ADS) hardware. The document
provides assumptions and information needed to understand the rationale for
equipment requirements and characteristics. The standard defines required
performance under standard operating conditions and stressed physical
environment conditions.
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DO-211,
User Requirements for Future Airport and Terminal Area Communications,
Navigation, and Surveillance
Issued 10-26-92 s Prepared
by SC-166
Presents a comprehensive statement of user requirements
for the next quarter century (to the year 2015). It examines the potential
capabilities of developmental and proposed communications, navigation, and
surveillance (CNS) systems and Air Traffic Management as they could apply in
terminal areas and at airports. The report examines current
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Issued 4-19-00 s Prepared
by SC-165
This standard addresses Aeronautical Mobile Satellite
Services operating in the frequency bands 1.5 and 1.6 GHz. DO-210D updates
DO-210C and contains new material regarding Inmarsat Aero H+/I services,
intermediate-gain antenna, channel descriptions, related physical layer and
management characteristics, and the 4.8 kbps Advanced Multiband Excitation
(AMBE) voice codec. New verification procedures related to priority,
precedence, and preemption are also included. Revisions relate to the Aero H+/I
services, clarifications of requirements, and a review of verification
procedures with respect to the Inmarsat System Definition Manual as well as
ICAO Standards and Recommended Practices. The document includes equipment
performance requirements, recommended bench tests and other performance
verification procedures, and installed equipment tests and operational
performance characteristics. DO-210D supercedes DO-210C and should be useful to
designers, manufacturers, installers, and users of the AMSS system and
equipment.
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Issued 12-14-00 s Prepared
by SC-165
Change 1 addresses Electromagnetic Compatibility (EMC)
issues that required resolution to ease the process of issuing a FAA Technical
Standard Order (TSO) implementing DO-210 D.
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Issued 11-28-01 s Prepared by SC-165
Change 2 updates receiver interference susceptibility
characteristics to include wide-band, as well as narrow-band, interfering
signals. The Change also provides a
complete set of verification procedures for all
requirements, whether contained within DO-210D itself or
invoked by external references.
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Issued 9-19-06 s Prepared by SC-208
Change
3 is intended to harmonize DO-210D and ARINC 741. The scope of Change 3 is
limited to a) changes involving output amplifier intermodulation effects and
tests related to such effects, and, b) changes involving the performance characteristics
such as harmonics, spurious, and noise emissions that depend on the shape of
the diplexer filter. The goal of these changes is to achieve the maximum
commonality possible with ARINC 741, as approved in October 2005.
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Issued 4-23-92 s Prepared
by SC-163 Errata Issued 7-1-92
Sets forth goals and applications and recommends
standards and procedures for systems that provide a means for reducing
simultaneous transmissions that adversely affect two-way voice radio
communications. This specification is applicable to ground-based,
ground-mobile, and airborne two-way UHF and VHF voice radio communications
equipment used for intercommunication and control of air traffic.
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Issued 7-12-91 s Prepared
by SC-159 Change 1 Issued 9-21-93
Sets forth the operational goals and applications, and
recommends standards and test procedures for airborne supplementary navigation
equipment (2D and 3D) using Global Positioning System (GPS) inputs in the en
route, terminal, and approach modes or any combination thereof. A supplemental
navigation system may be used as a primary navigation reference in an aircraft
when an approved and operational sole means navigation system is available. The
report defines performance, functions, and features for 2D airborne equipment,
which performs only lateral guidance, and 3D equipment, which performs both
lateral and vertical guidance.
FAA Technical Standard Order (TSO) – C129a references this document.
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Issued 9-21-93 s Errata
Issued 3-16-95
Change 1 provides editorial changes to subparagraphs on
Marginal Geometry Tests, Good Geometry Tests, and Dynamic Tests. Appendix B has
been rewritten to provide corrected computations to calculate geodesics on the
WGS-84 ellipsoid. A new Appendix K provides simulation of a second-order
Gauss-Markov process.
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Issued 1-25-91 s Prepared
by SC-163
Recommends standards and procedures for systems that
reduce unintentional transmissions and prevent blocked frequencies that
adversely affect two-way voice radio communications. This specification is
applicable to ground-based, ground-mobile, and airborne two-way VHF and UHF
radio voice communications equipment used for control of air traffic.
FAA Technical Standard Order (TSO) – C128 references this document.
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Issued 2-12-90 s Prepared
by SC-161
Sets forth a system description for the
Radiodetermination Satellite Service (RDSS). Provides a description of
non-safety-related functional capabilities that may be provided by and RDSS
system implemented for civil aviation users.
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DO-204A, Minimum Operational Performance Standards
for 406 MHz Emergency Locator Transmitters
(ELT)
Issued 12-06-07 s Prepared
by SC-204
DO-204A incorporates numerous changes to clarify the meaning and intent of the requirements. Text revisions and explanatory notes have been added. COSPAS/SARSAT testing criteria and DO-183 tests have been incorporated into the specification. G-Switch characteristics have been replaced. The document is harmonized with EUROCAE ED-62. Includes test conditions and procedures for installed equipment performance for emergency locator transmitters (ELTs) utilizing the 406.0 to 406.1 MHz band and operating in the COSPAS-SARSAT system.
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Issued 11-28-88 s Prepared
by SC-159
This document reports on the Global Positioning System
(GPS) and related parameters, for operation and use of a GPS-based navigation
system by civil users of the airspace. The report considers the use of GPS both
as a supplemental and as a sole means system for en route, terminal area, and
non-precision approach operations.
Integrity monitoring requirements are presented with a discussion of
suitable methods for determining GPS integrity and broadcasting this
information to civil aeronautical users. Coordinated with EUROCAE.
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DO-201A,
Standards for Aeronautical Information
Issued 4-19-00 s Prepared
by SC-181
This document provides for the improved operational
effectiveness of airborne navigation systems that use stored databases. It
presents a collection of disciplines necessary to provide assurance that
aeronautical information used by the aviation industry meets the high quality
and integrity for safe flight. The information in the document has been
compiled for the purpose of stating aeronautical information requirements of
the aviation industry with emphasis on RNAV operations in RNP airspace. There
is focus on the importance of quality aeronautical information and the fact
that the evolution of computer navigation technology requires a greater
dependency on the accuracy, reliability, integrity, and timely availability of
navigation reference data than ever before. This is a joint RTCA/EUROCAE
document.
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DO-200A,
Standards for Processing Aeronautical Data
Issued 9-28-98 s Prepared
by SC-181
This document provides the minimum standards for the
processing of aeronautical data that are used for navigation, flight planning,
terrain awareness, flight simulators and for other purposes. The standards
cover data processing quality assurance and quality management requirements.
They provide the user the necessary assurance that delivered aeronautical
databases meet the appropriate quality requirements for the data. DO-200A
supports new technology and the expanding scope of aeronautical data by
providing a more structured approach to the extremely important issues of data
quality and data integrity management.
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DO-199, Potential Interference
to Aircraft Electronic Equipment from Devices Carried Aboard
Issued 9-16-88 s Prepared
by SC-156 Supersedes DO-119
Reports on the investigation to determine potential
interference effects to aircraft electronic systems due to emissions from
self-powered portable electronic and electrical devices operated aboard
aircraft. Recommends regulatory actions relating to operation and
identification of passenger-operated devices to assure control of possible
sources of interference and recommends standardized procedures for reporting
suspected interference. Volume I is the basic report and includes background,
data collection, data analysis, conclusions, and recommendations. Volume II
provides amplification or background material for some of the summary data
included in the basic report.
Volume 1
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DO-197A,
Minimum Operational Performance Standards for an Active Traffic Alert and
Collision Avoidance System I (Active TCAS I)
Issued 9-12-94 s Prepared
by SC-147 Errata 11-22-94 Supersedes DO-197
Pertains to aircraft with up to 30 passenger seats as
prescribed by the Federal Aviation Administration (FAA) TCAS rules. Active TCAS
I is an air-to-air interrogation device that provides traffic advice to the
flight crew by alerting them to the presence of a nearby transponder- equipped
aircraft and advising the crew where to look for that aircraft so it can be
visually acquired and avoided if necessary. Unlike TCAS II and TCAS III, Active
TCAS I does not provide conflict resolution advisories.
FAA Technical Standard Order (TSO) – C118 references this document.
NOTE:
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Issued 7-29-97 s Prepared
by SC-147
Analysis of data recorded from TCAS I equipped aircraft
indicated that the TCAS I interference limiting algorithms were causing
acquisition of intruders at low ranges and that the tracks were often
intermittent. This change enhances the minimum TCAS I surveillance performance
by refining the assumptions used in development of the original interference
limiting algorithms. These modifications provide a significant operational
benefit to the operators of TCAS I equipment, without increasing the total
amount of interrogation power transmitted by TCAS I equipped aircraft. Power is
reallocated to more closely reflect the actual operating environment.
NOTE: The electronic DO-197A, Change 1 is a pdf
file but it is not in searchable format.
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Issued 11-17-86 s Prepared
by SC-153 Supersedes DO-149 and DO-153A
Sets forth operational goals and applications, and
recommends standards and test procedures for airborne VHF Omnirange (VOR)
receiving equipment. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C40c references this document.
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Issued 11-17-86 s Prepared
by SC-153 Supersedes DO-131A
Postulates operational goals and applications, and
recommends standards and test procedures for airborne ILS localizer receiving
equipment. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C36e references this document.
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Issued 11-17-86 s Prepared
by SC-137 Supersedes DO-159
Sets forth operational goals and applications, and
recommends standards and test procedures for airborne area navigation equipment
(2D and 3D) using Loran-C inputs. Includes test conditions and procedures for installed
Loran-C receiving equipment performance and operational characteristics with
test procedures. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C60b references this document.
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Issued 9-19-86 s Prepared
by SC-155
Reports on the operational requirements for
communications, navigation, and surveillance services likely to be required in
the 2010 time frame as foreseen by airspace users. Investigates new concepts
and technology, including the use of satellites, which may have applications in
a future airspace management system. Institutional, economic, and transitional
issues are assessed from
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Issued 7-18-86 s Prepared
by SC-153 Supersedes DO-132A
Postulates operational goals and applications, and
recommends standards and test procedures for airborne ILS glide slope receiving
equipment. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C34e references this document.
NOTE:
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DO-191, Minimum Operational Performance Standards
for Airborne Thunderstorm Detection Equipment
Issued 5-16-86 s Prepared
by SC-154
Defines the capabilities and limitations of the various
methods of airborne thunderstorm detection and determines the correlation
between the detection of electrical activity, precipitation, and any other
phenomena that is measured or detected and likely to be hazardous to flight
operations.
FAA Technical Standard Order (TSO) – C110a references this document.
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Issued 5-16-86 s Prepared
by SC-137 Supersedes DO-140
Postulates operational goals and applications, and
recommends standards and test procedures for airborne area navigation equipment
(2D and 3D) using Omega/VLF signals. Includes test conditions and procedures
for installed equipment performance and operational
characteristics with test procedures. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C120 references this document.
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Issued 9-20-85 s Prepared
by SC-149 Supersedes DO-141 and DO-151A
Postulates operational goals and applications, and
recommends standards and test procedures for airborne distance measuring
equipment (DME). It updates the former DME operational characteristics and
performance standards for airborne equipment that operates with conventional
DME (DME/N) ground facilities and establishes standards for airborne equipment
which will operate with both DME/N and precision DME (DME/P) ground facilities.
Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C66c references this document.
NOTE:
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DO-188, Emergency Locator
Transmitter (ELT) Batteries Guidance and Recommendations
Issued 11-13-84 s Prepared
by SC-136
Provides guidelines and recommendations concerning ELT
battery construction, storage, and methodology for qualifying replacement
batteries. An appendix concerning considerations for design and manufacture of
batteries for ELTs is included.
FAA Technical Standard Order (TSO) – C91a references this document.
NOTE:
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Issued 11-13-84 s Prepared
by SC-137
Postulates operational goals and applications, and
recommends standards and test procedures for airborne area navigation equipment
(2D and 3D) using multi-sensor inputs. Includes test conditions and procedures
for installed equipment performance and operational characteristics with test
procedures. Coordinated with
EUROCAE.
FAA Technical Standard Order (TSO) – C115b references this document.
NOTE:
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DO-186B,
Minimum Operational Performance Standards for Airborne Radio Communications
Equipment.
Issued 11-08-05 s Prepared
by SC-172
DO-186B recommends standards and test procedures
for airborne VHF communication transmitters and includes test conditions and
procedures for installed equipment. This
update incorporates Changes 1 and 2 of DO-186A and establishes performance
standards for equipment designed for offset carrier operations, i.e., equipment
classes A and C. An exclusion band to
enable a successful and appropriate Radio Frequency Susceptibility Test (DO-160
Section 20.0) is defined. The document
also includes class E receivers which are able to be used in an 8.33 kHz
channel separation environment.
This document supersedes DO-186A.
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Issued 06-19-08 s Prepared by SC-147
Errata Issued 7-14-08
This document
provides Version Downloadable 7.1 of the TCAS II logic and sets forth the
minimum operational performance standards for TCAS II equipment. The main
changes are the enhancement of the Resolution Advisory Sense reversal function,
and the replacement of “Adjust Vertical Speed, Adjust” Resolution Advisories by
“Level Off, Level Off” advisories.
Volume I
contains the rationale for equipment characteristics, minimum performance
standards, bench test procedures, and installed equipment performance. Volume
II presents the required collision avoidance algorithms in a state chart
formulation with informational commentary text. Attachment A provides both high
and low level pseudocode representations of the collision avoidance algorithms.
The standards and performance requirements in the document ensure that TCAS II
is fully interoperable with other elements and equipment of the National
Airspace System.
Document
available only as an electronic download.
An Errata is
provided with purchase of the document.
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Issued 07-01-09
Change 1 to DO-185B specifies changes to
the TCAS II requirements.
Section
1 provides the text changes to Volume I. The change affects the “middle”
aircraft of a multi-threat situation, and removes the feature that would have
required a green arc to accompany that aircraft’s RA.
Section
2 provides changes to the Pseudocode in Volume II, Attachment A. It clarifies the coding of certain bits
reporting Hybrid Surveillance capability within the Data Link Capability
Report, to be consistent with a change made to DO-300.
Section
3 provides changes to the state charts in Volume II.
Section
4 provides changes to the TSIM data set that is specified for the verification
of the TCAS implementation. This material is not part of DO-185B, but is
accompanying material distributed by FAA, not by RTCA.
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Issued 12-16-97 s Prepared by SC-147
This document provides Version Downloadable 7.0 of the
TCAS II logic and sets forth the minimum operational performance standards for
TCAS II equipment. Among the changes, this Version Downloadable improves the
system's surveillance performance and modifies the interference limiting
algorithms to account for aircraft densities near airports as well as to permit
longer range surveillance. Improvements have been made in tracking Mode S
targets and in permitting TCAS to receive the extended Mode S squitter. To
preclude repeatedly issuing Traffic Advisories (TA) against the same target,
changes have been made to ensure that a target's TA status is maintained in
slow closure situations by using more stringent drop criteria. Other changes
include credibility checks to ensure integrity of the data being supplied to
the collision avoidance logic and additional, more thorough tests for installed
equipment.
Volume I contains the rationale for equipment
characteristics, minimum performance standards, bench test procedures, and
installed equipment performance. Volume II presents the required collision
avoidance algorithms in a state chart formulation with informational commentary
text. Attachment A provides both high and low level pseudocode representations
of the collision avoidance algorithms. The standards and performance requirements
in the document ensure that TCAS II is fully interoperable with other elements
and equipment of the National Airspace System.
Note:
TSO-C119b -Requests for a Copy of the CD-ROM Titled “TSO
C119B Changes to DO-185A, Approved by
SC-147 RWG* dated December 4, 1998 should be directed
to: Federal Aviation Administration, Headquarters, Technical Programs &
Continued Airworthiness Branch (AIR-120), (P) 202-267-9578.
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DO-184, Traffic Alert and
Collision Avoidance System (TCAS) I Functional Guidelines
Issued 5-13-83 s Prepared
by SC-147
Sets forth minimum requirements, and describes the
various elements of TCAS I. Discusses both passive and active TCAS I
applications. Provides the minimum performance requirements for electromagnetic
compatibility for an active TCAS I and test procedures for both active and
passive systems. Appendix A addresses cross-link advisories.
NOTE: The electronic DO-184 is a pdf file but it is
not in searchable format.
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Issued 5-13-83 s Prepared by SC-136
Supersedes DO-145, DO-146 and
DO-168 s Change 1 issued 1-17-86
Postulates operational goals and applications, and
recommends standards and test procedures for emergency locator transmitters.
Includes test conditions and procedures for installed equipment performance and
operational characteristics with test procedures.
FAA Technical Standard Order (TSO) – C91a references this document.
NOTE:
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DO-182, Emergency Locator
Transmitter (ELT) Equipment Installation and Performance
Issued 11-17-82 s Prepared
by SC-136
Provides analyses of ELT performance in regard to false
alarms and activations in crash environments; provides criteria and guidelines
for placement and installation of ELTs in aircraft; reports on ELT system
performance in a variety of typical installations; and provides specific
recommendations on all of the above standards.
NOTE: The electronic DO-182 is a pdf file but it is
not in searchable format.
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Issued 03-17-11 s Prepared
by SC-209 Supersedes DO-181D
This
document supersedes DO-181D published in 2008. It provides standards for Mode S
airborne equipment (Mode S implies a combined ATCRBS/Mode S capability).
Incorporated within these standards are system characteristics that will be
helpful to users of the system as well as designers, manufacturers and
installers. The document considers an equipment configuration consisting of
transponder, control panel, antenna and interconnecting cables. Level 1 through
Level 5 transponders are addressed and test procedures are provided as well as
information for optional features. It reflects issues identified and discussed
by the ICAO Aeronautical Surveillance Panel Technical Subgroup and reported by
Civil Aviation Authorities since the publication of DO-181D in October 2008.
The document is a coordinated effort with EUROCAE WG-49 and includes changes
resulting from DO-260B, ADS-B MOPS, published in December 2009. Appendix E
details the Changes from DO-181D to DO-181E.
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Issued 5-24-90 s Prepared by SC-137 Supersedes
DO-180
Postulates operational goals and applications and
recommends standards and test procedures for airborne area navigation equipment
(2D and 3D) using sensor inputs from a single collocated VOR/DME station.
Includes test conditions and procedures for installed equipment performance
and operational characteristics with test procedures. Coordinated with EUROCAE.
NOTE: The electronic DO-180A is a pdf file but it
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DO-179, Minimum Operational
Performance Standards for Automatic Direction Finding (ADF) Equipment
Issued 5-13-82 s Prepared
by SC-146 Supersedes DO-137 and DO-142
Postulates operational goals and applications and
recommends standards and test procedures for airborne automatic direction
finding equipment. Includes test conditions and procedures for installed equipment
performance and operational characteristics with test procedures. Coordinated
with EUROCAE.
Coordinated with EUROCAE FAA Technical Standard Order (TSO) – C41d references this document.
NOTE: The electronic DO-179 is a pdf file but it is
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DO-178B, Software
Considerations in Airborne Systems and Equipment Certification
Issued 12-1-92 s Prepared by SC-167
Advisory Circular s Supersedes
DO-178A s Errata Issued 3-26-99 s
Provides guidance for determining, in a consistent manner and with an
acceptable level of confidence, that the software aspects of airborne systems
and equipment comply with airworthiness requirements.
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Issued
7-17-81 s Change 1 s Change 2 issued 9-19-86 s Prepared by SC-139
Postulates operational goals and applications, and
recommends standards and test procedures for use of Microwave Landing System
(MLS) airborne receiving equipment. Includes test conditions and procedures for
installed equipment performance and operational characteristics with test
procedures. Coordinated with EUROCAE.
FAA Technical Standard Order (TSO) – C104 references this document.
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DO-176, FM Broadcast
Interference Related to Airborne ILS, VOR and VHF Communications
Issued 11-18-81 s Prepared
by SC-141
Reviews the various aspects of the problem of commercial
FM broadcast stations contributing to the interference of airborne systems.
Recommends improved intra-governmental coordination procedures and recommends
steps to limit growth of the problem, to reduce the problem with installed
receivers, and to minimize the problem with new receivers or installations.
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Issued 1-23-81 s Prepared
by SC-143
Postulates operational goals and applications,
recommends standards and test procedures for ground-based automated weather
observation equipment. Provides system characteristics for users, designers,
manufacturers, and installers of such equipment of interest to various users,
including airfield operations, meteorological services, aviation
administrations, airplane and helicopter operators, etc. Includes test
conditions and procedures for installed system performance and operational characteristics
with test procedures.
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Issued 3-20-81 s Prepared
by SC-133
Postulates operational goals and applications, and
recommends standards and test procedures for use of weather and ground mapping
radar indicators for display of non-radar graphic and/or alphanumeric data.
Includes test conditions and procedures for installed equipment performance and
operational characteristics with test procedures.
FAA Technical Standard Order (TSO) – C105 references this document.
NOTE:
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Issued 11-19-80 s
Corrigendum/Errata/Change 1 s Supersedes DO-134
s Prepared by SC-133
Postulates operational goals and applications;
recommends standards and test procedures for airborne weather and ground
mapping pulsed radars. Takes into account new radar technology and is
applicable to both large aircraft and general aviation aircraft systems.
Includes test conditions and procedures for
installed equipment performance and operational
characteristics with test procedures.
FAA Technical Standard Order (TSO) – C63c references this document.
NOTE:
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Issued
11-19-80 s Change 1 s Prepared by SC-133
Postulates operational goals and applications, and
recommends standards and test procedures for Airborne Radar Approach (ARA)
systems for helicopters, particularly when operating under IFR, IMC conditions,
or at night, including standards for the ground-based radar beacon. Includes
test conditions and procedures for installed equipment performance and
operational characteristics with test procedures.
FAA Technical Standard Order (TSO) – C102 references this document.
NOTE:
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Issued 1-25-80 s Prepared
by SC-134
Provides rationale and recommendations for various
conditions and procedures that could provide major benefits to those
responsible for drafting legislation, policies, procedures, and guidelines for
the acquisition and support of electronic test equipment.
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DO-169,
VHF Air-Ground Communication Technology and Spectrum Utilization
Issued 7-20-79 s Prepared
by SC-140
Reports on VHF (118-136 MHz) spectrum utilization
including the investigation of modulation techniques and reduced channel
separation. Identifies problem areas and recommends, among other things, use of
reduced channel spacing on a selective basis.
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DO-167, Airborne Electronics
and Electrical Equipment Reliability
Issued 9-16-77 s Prepared
by SC-130
Provides a tutorial discussion on reliability related to
aircraft accidents. Discusses airborne electronic equipment failures and means
of reducing failures, and presents arguments against use on MTBF and MTBR as
reliability measures for use in RTCA MPSs and FAA TSOs.
NOTE:
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DO-166, Microwave Landing System (MLS) Implementation
Issued 7-15-77 s Prepared
by SC-125
Reports on a study of develop user recommendations for a
national implementation policy for MLS as the primary landing system in service
by the year 2000. Volume I provides recommendations on how best to transition
from ILS to MLS; recommends implementation strategy and a national
implementation policy, which are summarized in a findings and recommendations
chapter. Volume II includes six appendices, which are the reports of working
groups in special categories such as Benefits, Airborne Systems Operational
Capabilities, and Civil System Costs.
NOTE:
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searchable format.
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Volume 2
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e-DO-166
V2 (downloadable from www.rtca.org)
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$87.00 All other countries
$113.10 |
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DO-165, Initial Report on
Civil Aviation Frequency Spectrum Requirements-1980- 2000
Issued 5-27-76 s Prepared
by SC-129
Provides a comprehensive report on civil aviation's
frequency requirements. Appendices recommend revisions to the ITU Table of
Allocations and the footnotes thereto. Provides justification for stated operational
requirements; provides an aviation forecast.
Hardcopy
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$63.00 All other countries
$90.00 Member Price US/Canada/Mexico
$25.20 All other countries $36.00 |
DO-164A, Minimum Performance
Standards-Airborne Omega Receiving Equipment
Issued 9-21-79 s
Superseded DO-164 s Prepared by SC-138
Recommends standards and test procedures for airborne
Omega Navigation Receivers, Systems Sensors, and Navigation Systems. Also
included are operational characteristics. Appendices include conditions for
testing, detailed test procedures, and a description of Omega Error Mechanisms.
FAA Technical Standard Order (TSO) – C94a references this document.
Hardcopy
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$48.00 All other countries
$75.00 Member Price US/Canada/Mexico
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Issued 3-19-76 s Errata s Supersedes DO-48A
and DO-49A s Prepared by SC-131
Recommends standards and test procedures for HF/SSB
receivers and transmitters designed to operate in a 3 kHz channel environment.
Also includes standards for the provision of AM equivalent mode of operation.
Appendices include conditions for testing and detailed test procedures.
FAA Technical Standard Order (TSO) – C31d and C32d reference this document.
NOTE:
The electronic DO-163 is a pdf file but it is not in searchable format.
Hardcopy
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e-DO-163
(downloadable from www.rtca.org)
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$48.00 All other countries
$75.00 |
Member No Charge Non-Member
$60.00 |
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DO-162, Report on Air-Ground
Communications-Operational Considerations for 1980 and Beyond
Issued 10-17-75 s Prepared
by SC-120
Provides an analysis of air-ground communications
requirements anticipated for the post-1980 time frame. Includes definitions of
US aviation system and future trends, requirements, systems concepts, and
recommendations. This is a companion report to RTCA
Paper No. 128-72/EC-671 issued 8-18-72, entitled Proposed US National Aviation
Standard for the VHF A/G Communications System.
Hardcopy
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DO-161A, Minimum Performance
Standards-Airborne Ground Proximity Warning Equipment
Issued 5-27-76 s Prepared
by SC-128 Supersedes DO-161
Recommends standards and test procedures for Ground
Proximity Warning Equipment. This is a revision of DO-161 and includes changes
(1 & 2) to that document and other improvements suggested by operating
experience. Appendices include envelopes of conditions for warning, conditions
for testing, and detailed test procedures.
FAA Technical Standard Order (TSO) – C92c references this document.
NOTE:
The electronic DO-161A is a pdf file but it is not in searchable format.
Hardcopy
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e-DO-161A
(downloadable from www.rtca.org)
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