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FAA AC 00-69 : 2017

Current

Current

The latest, up-to-date edition.

BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )

Published date

20-11-2017

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1. PURPOSE
2. AUDIENCE
3. BEST PRACTICES
4. RELATED PUBLICATIONS
5. WHERE TO FIND THIS AC
Appendix A - Advisory Circular Feedback Information

Gives information in the form of 'best practices' and, as such, is not intended as guidance but rather as complementary information to ED-12C/DO-178C (and related documents) and AC 20-115D.

DocumentType
Standard
PublisherName
Federal Aviation Administration
Status
Current

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 AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
FAA AC 35.23-1 : 2011 GUIDANCE MATERIAL FOR 14 CFR SECTION 35.23, PROPELLER CONTROL SYSTEM
FAA AC 33.28-3 : 2014 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
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
RTCA DO 248 : C2011 SUPPORTING INFORMATION FOR DO-178C AND DO-278A
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
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

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