FAA AC 00-66 : 2015
Current
The latest, up-to-date edition.
SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
Hardcopy , PDF
English
01-01-2015
1. Purpose
2. Audience
3. Effective Date
4. Related Publications
5. Definition of Key Terms
6. Background
7. Summary
8. Where to Find This AC
Appendix A - Advisory Circular Feedback Information
Gives information about the availability of resource material on digital data integrity.
| DocumentType |
Standard
|
| Pages |
5
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| FAA AC 20-170 : 2010 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
| FAA AC 20-174 : 2011 | DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA AC 21-50 : 2011 | INSTALLATION OF TSOA ARTICLES AND LODA APPLIANCES |
| FAA 8110.105 : 2017 | SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE |
| FAA AC 33.28-2 : 2003 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| FAA 8110.49 : 2011 | SOFTWARE APPROVAL GUIDELINES |
| FAA AC 35.23-1 : 2011 | GUIDANCE MATERIAL FOR 14 CFR SECTION 35.23, PROPELLER CONTROL SYSTEM |
| FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
| FAA AC 33.28-3 : 2014 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS |
| FAA AC 20-153 : 2016 | ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES |
| FAA AC 20-171 : 2011 | ALTERNATIVES TO RTCA/DO-178B FOR SOFTWARE IN AIRBORNE SYSTEMS AND EQUIPMENT |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| FAA AC 33.28-1 : 0 | COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS |
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