FAA AC 23.1309-1 : 2011
Current
The latest, up-to-date edition.
SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
Hardcopy , PDF
English
01-01-2011
1. What is the purpose of this AC?
2. Who does this AC apply to?
3. Cancellation
4. Related regulations and documents
5. Applicability
6. Regulations and AC background
7. Acronyms
8. Definitions
9. Application of section 23.1309(a), (a)(1), (a)(2),
and (a)(3), as adopted by Amendments 23-41 and 23-49
10. Showing compliance with the requirements of
section 23.1309 (a) through Amendment 23-49
11. Application of section 23.1309(a)(4), as adopted by
Amendment 23-49
12. Application of section 23.1309(a)(1) and (a)(2), as
adopted by Amendments 23-62
13. Application of section 23.1309(b), as adopted by
Amendment 23-62
14. Application of section 23.1309(b), as adopted by
Amendments 23-41 and 23-49 and section 23.1309(c),
as adopted by Amendment 23-62
15. Four certification classes of airplanes
16. Safety assessments
17. Failure conditions
18. Assessment methods
19. Assessment of failure condition probabilities and
analysis considerations
20. Operational and maintenance considerations
21. Software and complex hardware DALs for airborne
system and applications
APPENDIX 1 - PARTIAL LIST OF FUNCTIONAL HAZARD ASSESSMENT
(FHA) FOR CONSIDERATION TO MEET 14 CFR PART 23
REQUIREMENTS FOR IFR CLASS I AIRPLANES
APPENDIX 2 - SAMPLE FUNCTIONAL HAZARD ASSESSMENT (FHA) FORMAT
APPENDIX 3 - CALCULATION OF THE AVERAGE PROBABILITY PER
FLIGHT HOUR
Specifies guidance and information for an acceptable means, but not the only means, for showing compliance with the requirements of section 23.1309 (Amendment 23-62) for equipment, systems, and installations in 14 CFR part 23 airplanes.
DocumentType |
Standard
|
Pages |
56
|
PublisherName |
Federal Aviation Administration
|
Status |
Current
|
SAE ARP 1907 : 2016 | AUTOMATIC BRAKING SYSTEMS |
IEC 62396-1:2016 | Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment |
FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
DD IEC TS 62396-1 : DRAFT JUL 2006 | PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT |
FAA AC 20-174 : 2011 | DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
15/30324422 DC : 0 | BS EN 62396-1 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT |
FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
FAA AC 20-170 : 2013 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
SAE ARP 5412 : 2013 | AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS |
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
FAA 8300.16 : 2014 | MAJOR REPAIR AND ALTERATION DATA APPROVAL |
FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
SAE ARP 4032 : 2013 | HUMAN ENGINEERING CONSIDERATIONS IN THE APPLICATION OF COLOR TO ELECTRONIC AIRCRAFT DISPLAYS |
FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
SAE ARP 5414 : 2012 | AIRCRAFT LIGHTNING ZONE |
FAA AC 20-181 : 2014 | AIRWORTHINESS APPROVAL OF ATTITUDE HEADING REFERENCE SYSTEM (AHRS) EQUIPMENT |
ASTM F 3201 : 2016 | Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS) |
ASTM F 2690 : 2008 | Standard Guide for Suggested Procedures for Applying for a Flight Authority for an Unmanned Aircraft System: Part I and Part II (Withdrawn 2014) |
BS IEC 62396-1 : 2016 | PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT |
FAA AC 120-77 : 0 | MAINTENANCE AND ALTERATION DATA |
FAA AC 90-105 : 2016 | APPROVAL GUIDANCE FOR RNP OPERATIONS AND BAROMETRIC VERTICAL NAVIGATION IN THE U.S. NATIONAL AIRSPACE SYSTEM AND IN OCEANIC AND REMOTE CONTINENTAL AIRSPACE |
FAA AC 20-173 : 2011 | INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS |
FAA AC 00-69 : 2017 | BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
FAA AC 20-153 : 2016 | ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES |
SAE AS 8055A : 2015 | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD) |
SAE AIR 1957 : 2015 | HEAT SINKS FOR AIRBORNE VEHICLES |
SAE ARP 5677 : 2012 | HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS |
FAA AC 20-177 : 2012 | DESIGN AND INSTALLATION GUIDANCE FOR AN AIRBORNE SYSTEM FOR NON-REQUIRED TELECOMMUNICATION SERVICE IN NON-AERONAUTICAL FREQUENCY BANDS |
FAA AC 120-86 : 2005 | AIRCRAFT SURVEILLANCE SYSTEMS AND APPLICATIONS |
FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
FAA 8110.49 : 2011 | SOFTWARE APPROVAL GUIDELINES |
FAA AC 20-165 : 2015 | AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS |
FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
FAA AC 23-11 : 2009 | 14 CFR PART 23 TYPE CERTIFICATION OF AN AIRPLANE ORIGINALLY CERTIFICATED TO EUROPEAN AVIATION SAFETY AGENCY (EASA) (CS-VLA) STANDARDS OR JOINT AVIATION REQUIREMENTS - VERY LIGHT AIRPLANE (JAR-VLA) |
FAA N 8110.110 : 2010 | SOFTWARE APPROVAL GUIDE LINES, CONTINUED |
IEC TS 62396-1:2006 | Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment |
SAE AS 5498 : 2017 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
SAE ARP 5416 : 2013 | AIRCRAFT LIGHTNING TEST METHODS |
SAE ARP 5119 : 2013 | LOCATION OF AND DISPLAY SYMBOLOGY REQUIREMENTS FOR HEAD-DOWN ELECTRONIC FLIGHT DISPLAYS FOR STEEP IMC APPROACHES |
FAA AC 121-22 : 2012 | MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES |
FAA AC 00-66 : 2015 | SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
SAE ARP 5770 : 2012 | MECHANICAL CONTROL DESIGN GUIDE |
FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
FAA N 8200.97 : 2006 | AIRMAN AND AIRCRAFT APPROVAL FOR REDUCED VISIBILITY FLIGHT OPERATIONS, INCLUDING CATEGORY 2/3 OPERATIONS |
SAE ARP 5589 : 2005 | HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS |
SAE ARP 5672 : 2016 | AIRCRAFT PRECIPITATION STATIC CERTIFICATION |
FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
FAA AC 120-76 : 2017 | AUTHORIZATION FOR USE OF ELECTRONIC FLIGHT BAGS |
11/30246255 DC : 0 | BS EN 62396-1 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT |
SAE ARP 5430 : 2013 | HUMAN INTERFACE CRITERIA FOR VERTICAL SITUATION AWARENESS DISPLAYS |
FAA AC 33.75-1 : 2007 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS |
FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
FAA AC 23-21 : 2004 | AIRWORTHINESS COMPLIANCE CHECKLISTS USED TO SUBSTANTIATE MAJOR ALTERATIONS FOR SMALL AIRPLANES |
FAA AC 20-183 : 2014 | LASER AIRWORTHINESS INSTALLATION GUIDANCE |
FAA AC 23.1523 : 2005 | MINIMUM FLIGHT CREW |
FAA AC 20-185 : 2015 | AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM |
FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
FAA AC 20-150 : 2014 | AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION |
SAE ARP 60493 : 2017 | GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC) |
FAA AC 20-172 : 2015 | AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS |
FAA AC 20-149 : 2015 | INSTALLATION GUIDANCE FOR DOMESTIC FLIGHT INFORMATION SERVICE - BROADCAST |
FAA AC 120-28 : 0 | CRITERIA FOR APPROVAL OF CATEGORY 3 WEATHER MINIMA FOR TAKEOFF, LANDING, AND ROLLOUT |
FAA AC 20-145 : 2003 | GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS |
IEC 62396-1:2016 RLV | Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment |
SAE ARP 6023 : 2013 | HUMAN ENGINEERING CONSIDERATIONS FOR IMPLEMENTING ENHANCED SYNTHETIC VISION SYSTEMS IN VERTICAL FLIGHT CAPABLE PLATFORMS |
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
FAA 8110.4 : 2011 | TYPE CERTIFICATION |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
FAA 8110.10 : 0 | APPROVALS OF MAJOR MODIFICATIONS/ALTERATIONS |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
FAA AC 21.101-1 : 2016 | ESTABLISHING THE CERTIFICATION BASIS OF CHANGED AERONAUTICAL PRODUCTS |
FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
FAA AC 23-17 : 2011 | SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
FAA AC 33.75-1 : 2007 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS |
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.