• There are no items in your cart

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

11-20-2017

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

View more information
Sorry this product is not available in your region.

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.