SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2015

Publisher

Federal Aviation Administration

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
RTCA DO 200B : 2015	STANDARDS FOR PROCESSING AERONAUTICAL DATA
FAA AC 20-170 : 2010	INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
RTCA DO 330 : 2011	SOFTWARE TOOL QUALIFICATION CONSIDERATIONS
RTCA DO 178 : C2011	SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
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 ARP 4754 : 2010	GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
FAA 8110.49 : 2011	SOFTWARE APPROVAL GUIDELINES
RTCA DO 254 : 2000	DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
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
RTCA DO 333 : 2011	FORMAL METHODS SUPPLEMENT TO DO-178C AND DO-278A
FAA AC 25.1309-1 : 0	SYSTEM DESIGN AND ANALYSIS
RTCA DO 331 : 2011	MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A
FAA AC 20-115 : 2017	AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
RTCA DO 297 : 2005	Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations<br>
RTCA DO 332 : 2011	OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A
FAA AC 33.28-1 : 0	COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS