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
|
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| 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 |
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| 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 |
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| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
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| 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 |
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| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
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| FAA AC 33.75-1 : 2007 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS |
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