FAA AC 20-152 : 2005
Current
The latest, up-to-date edition.
RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
Hardcopy , PDF
English
01-01-2005
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1 PURPOSE
2 WHY USE RTCA/DO-254?
3 WHO CAN USE RTCA/DO-254?
4 FUTURE CHANGES OR REVISIONS
5 RELATED DOCUMENTS
Applies to manufacturers and installers of products or appliances incorporating complex custom micro-coded components with hardware design assurance levels of A, B, and C. Provides a means to gain Federal Aviation Administration (FAA) approval by showing the equipment design is appropriate for its intended function.
| DocumentType |
Standard
|
| Pages |
2
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 20-174 : 2011 | DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA 8110.105 : 2017 | SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE |
| FAA AC 20-170 : 2013 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| FAA AC 20-169 : 2010 | GUIDANCE FOR CERTIFICATION OF MILITARY AND SPECIAL MISSION MODIFICATIONS AND EQUIPMENT FOR COMMERCIAL DERIVATIVE AIRCRAFT (CDA) |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| FAA AC 20-173 : 2011 | INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| SAE AS 6163 : 2015 | TEMPERATURE CONTROLLED CONTAINER - PERFORMANCE REQUIREMENTS AND TEST PARAMETERS |
| FAA AC 20-177 : 2012 | DESIGN AND INSTALLATION GUIDANCE FOR AN AIRBORNE SYSTEM FOR NON-REQUIRED TELECOMMUNICATION SERVICE IN NON-AERONAUTICAL FREQUENCY BANDS |
| FAA AC 00-66 : 2015 | SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE ARP 1070E : 2019 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
| SAE ARP 1070 : 2014 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| FAA AC 25.1329-1 : 2016 | APPROVAL OF FLIGHT GUIDANCE SYSTEMS |
| FAA AC 20-183 : 2014 | LASER AIRWORTHINESS INSTALLATION GUIDANCE |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
| FAA AC 20-150 : 2014 | AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION |
| SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
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