• FAA AC 23.1309-1 : 2011

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    SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2011

    Publisher:  Federal Aviation Administration

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher Federal Aviation Administration
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE ARP 5770 : 2012 MECHANICAL CONTROL DESIGN GUIDE
    ASTM F 3201 : 2016 Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS)
    FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 1907 : 2016 AUTOMATIC BRAKING SYSTEMS
    FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
    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 23-21 : 2004 AIRWORTHINESS COMPLIANCE CHECKLISTS USED TO SUBSTANTIATE MAJOR ALTERATIONS FOR SMALL AIRPLANES
    FAA N 8200.97 : 2006 AIRMAN AND AIRCRAFT APPROVAL FOR REDUCED VISIBILITY FLIGHT OPERATIONS, INCLUDING CATEGORY 2/3 OPERATIONS
    FAA AC 20-183 : 2014 LASER AIRWORTHINESS INSTALLATION GUIDANCE
    FAA AC 23.1523 : 2005 MINIMUM FLIGHT CREW
    SAE ARP 5589 : 2005 HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS
    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
    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)
    SAE ARP 5672 : 2016 AIRCRAFT PRECIPITATION STATIC CERTIFICATION
    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 20-158 : 2014 THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT
    FAA AC 20-185 : 2015 AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM
    FAA AC 20-165 : 2015 AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS
    FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    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 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION 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)
    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 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 20-150 : 2014 AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION
    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 20-184 : 2015 GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
    SAE ARP 60493 : 2017 GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC)
    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 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
    IEC 62396-1 REDLINE : 2ED 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 20-156 : 2006 AVIATION DATABUS ASSURANCE
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    SAE AS 5498 : 2017 MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS
    FAA AC 20-153 : 2016 ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES
    SAE ARP 4032 : 2013 HUMAN ENGINEERING CONSIDERATIONS IN THE APPLICATION OF COLOR TO ELECTRONIC AIRCRAFT DISPLAYS
    FAA AC 20-172 : 2015 AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS
    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
    SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
    SAE AIR 1957 : 2015 HEAT SINKS FOR AIRBORNE VEHICLES
    FAA AC 23-8 : 2011 FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
    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 121-22 : 2012 MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES
    SAE ARP 5414 : 2012 AIRCRAFT LIGHTNING ZONE
    FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
    FAA AC 20-181 : 2014 AIRWORTHINESS APPROVAL OF ATTITUDE HEADING REFERENCE SYSTEM (AHRS) EQUIPMENT
    FAA AC 20-145 : 2003 GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS
    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
    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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
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