FAA AC 00-69 : 2017
Current
The latest, up-to-date edition.
BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
20-11-2017
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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