FAA 8110.49 : 2011
Current
The latest, up-to-date edition.
SOFTWARE APPROVAL GUIDELINES
Hardcopy , PDF
English
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)
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| 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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