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FAA 8110.49 : 2011

Current

Current

The latest, up-to-date edition.

SOFTWARE APPROVAL GUIDELINES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

Chapter 1 - General Information
Chapter 2 - Software Review Process
Chapter 3 - [Reserved]
Chapter 4 - Software Conformity Inspection
Appendix A - Level of Involvement Worksheets
Appendix B - Directive Feedback Information

Specifies Aircraft Certification Service (AIR) offices and designees on how to apply RTCA/DO-178B and RTCA/DO-178C, herein called RTCA/DO-178B/C for approving software used in airborne computers.

DevelopmentNote
Supersedes FAA N 8110.85, FAA N 8110.86, FAA N 8110.87, FAA N 8110.88, FAA N 8110.89, FAA N 8110.90, FAA N 8110.91, FAA N 8110.92, FAA N 8110.93, FAA N 8110.94, FAA N 8110.95 (12/2003) Supersedes FAA N 8110.110. (11/2011)
DocumentType
Standard
Pages
105
PublisherName
Federal Aviation Administration
Status
Current
Supersedes

FAA 8110.105 : 2017 SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA 8110.55 : 2016 HOW TO EVALUATE AND ACCEPT PROCESSES FOR AERONAUTICAL DATABASE SUPPLIERS
FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
FAA AC 43-216 : 2017 SOFTWARE MANAGEMENT DURING AIRCRAFT MAINTENANCE
FAA 8110.4 : 2011 TYPE CERTIFICATION

FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
RTCA DO 330 : 2011 SOFTWARE TOOL QUALIFICATION CONSIDERATIONS
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 21-43 : 2015 PRODUCTION UNDER 14 CFR PART 21, SUBPARTS F, G, K, AND O
FAA AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
FAA 8110.4 : 2011 TYPE CERTIFICATION
FAA AC 33.28-3 : 2014 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
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
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( )
FAA 8040.4 : 2012 SAFETY RISK MANAGEMENT POLICY
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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