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FAA AC 25.1309-1 : 0

Current

Current

The latest, up-to-date edition.

SYSTEM DESIGN AND ANALYSIS

Available format(s)

Hardcopy , PDF

Language(s)

English

€35.89
Excluding VAT

1 PURPOSE
2 CANCELLATION
3 APPLICABILITY
4 BACKGROUND
5 THE FAA FAIL-SAFE DESIGN CONCEPT
6 DEFINITIONS
7 DISCUSSION
8 ACCEPTABLE TECHNIQUES
9 QUALITATIVE ASSESSMENT
10 QUANTITATIVE ASSESSMENT
11 OPERATIONAL AND MAINTENANCE CONSIDERATIONS
12 STEP-BY-STEP GUIDE

Explains various acceptable means for showing compliance with the requirements of Section 25.1309(b), (c) and (d) of the Federal Aviation Regulations (FAR).

DocumentType
Standard
Pages
19
PublisherName
Federal Aviation Administration
Status
Current

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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
GEIA STD 0010 : 2008 BEST PRACTICES FOR SYSTEM SAFETY PROGRAM DEVELOPMENT AND EXECUTION
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 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
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
SAE AIR 6441 : 2015 INFORMATION ON PARKING BRAKE SYSTEMS
FAA AC 33.4-3 : 2005 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS; AIRCRAFT ENGINE HIGH INTENSITY RADIATED FIELDS (HIRF) AND LIGHTNING PROTECTION FEATURES
FAA 8300.16 : 2014 MAJOR REPAIR AND ALTERATION DATA APPROVAL
FAA AC 25.1701-1 : 2007 CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES
ARINC 660B : 2014 CNS/ATM AVIONICS ARCHITECTURES SUPPORTING NEXTGEN/SESAR CONCEPTS
FAA AC 20-184 : 2015 GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
SAE AS 6858 : 2017 INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT
SAE AIR 4766/2 : 2011 AIRBORNE CHEMICALS IN AIRCRAFT CABINS
SAE ARP4032B HUMAN ENGINEERING CONSIDERATIONS IN THE APPLICATION OF COLOR TO ELECTRONIC AIRCRAFT DISPLAYS
FAA AC 25.1353-1 : 2007 ELECTRICAL EQUIPMENT AND INSTALLATIONS
FAA AC 25.703-1 : 0 TAKEOFF CONFIGURATION WARNING SYSTEMS
SAE ARP1834B FAULT/FAILURE ANALYSIS FOR DIGITAL SYSTEMS AND EQUIPMENT
SAE ARP 6803 : 2016 IVHM CONCEPTS, TECHNOLOGY AND IMPLEMENTATION OVERVIEW
FAA AC 25.1322-1 : 2010 FLIGHTCREW ALERTING
FAA AC 20-181 : 2014 AIRWORTHINESS APPROVAL OF ATTITUDE HEADING REFERENCE SYSTEM (AHRS) EQUIPMENT
FAA AC 25.1357-1 : 2007 CIRCUIT PROTECTIVE DEVICES
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 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
SAE ARP 5672 : 2016 AIRCRAFT PRECIPITATION STATIC CERTIFICATION
SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
SAE AS 6163 : 2015 TEMPERATURE CONTROLLED CONTAINER - PERFORMANCE REQUIREMENTS AND TEST PARAMETERS
FAA AC 00-69 : 2017 BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 25.1360-1 : 2007 PROTECTION AGAINST INJURY
FAA AC 25.1419-1 : 0 CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES FOR FLIGHT IN ICING CONDITIONS
FAA AC 20-153 : 2016 ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES
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 AIR 4766 : 2012 AIR QUALITY FOR COMMERCIAL AIRCRAFT CABINS
FAA AC 25.1365-1 : 2007 ELECTRICAL APPLIANCES, MOTORS, AND TRANSFORMERS
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
SAE ARP1907C AUTOMATIC BRAKING SYSTEMS
SAE ARP 6467 : 2014 HUMAN FACTORS MINIMUM REQUIREMENTS AND RECOMMENDATIONS FOR THE FLIGHT DECK DISPLAY OF DATA LINKED NOTICES TO AIRMEN (NOTAMS)
FAA AC 20-167 : 2016 AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT
FAA AC 120-86 : 2005 AIRCRAFT SURVEILLANCE SYSTEMS AND APPLICATIONS
FAA 8110.49 : 2011 SOFTWARE APPROVAL GUIDELINES
ARINC 628P7-2:2013 CABIN EQUIPMENT INTERFACES (CEI) - PART 7: CABIN EQUIPMENT COOLING GENERAL SPECIFICATION
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 25.1419-2 : 2009 COMPLIANCE WITH THE ICE PROTECTION REQUIREMENTS OF SECTION 25.1419(E), (F), (G), AND (H)
SAE ARP5589 Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance Displays
SAE ARP 5580 : 2012 RECOMMENDED FAILURE MODES AND EFFECTS ANALYSIS (FMEA) PRACTICES FOR NON-AUTOMOBILE APPLICATIONS
SAE ARP 5430 : 2013 HUMAN INTERFACE CRITERIA FOR VERTICAL SITUATION AWARENESS DISPLAYS
FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
SAE AS4914D AIRCRAFT FLUORESCENT LIGHTING BALLAST/FIXTURE SAFETY STANDARD
SAE ARP 5416 : 2013 AIRCRAFT LIGHTNING TEST METHODS
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 N 8200.97 : 2006 AIRMAN AND AIRCRAFT APPROVAL FOR REDUCED VISIBILITY FLIGHT OPERATIONS, INCLUDING CATEGORY 2/3 OPERATIONS
FAA AC 20-158 : 2014 THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT
SAE ARP5412B AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
FAA AC 25-28 : 2014 COMPLIANCE OF TRANSPORT CATEGORY AIRPLANES WITH CERTIFICATION REQUIREMENTS FOR FLIGHT IN ICING CONDITIONS
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
MIL-HDBK-87213 Revision A:2005 ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS
FAA AC 20-151 : 2017 AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2), VERSIONS 7.0 & 7.1 AND ASSOCIATED MODE S TRANSPONDERS
SAE AIR 1957 : 2015 HEAT SINKS FOR AIRBORNE VEHICLES
FAA AC 33.75-1 : 2007 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS
FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
SAE ARP1619B REPLACEMENT AND MODIFIED BRAKES AND WHEELS
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 25-10 : 0 GUIDANCE FOR INSTALLATION OF MISCELLANEOUS, NON-REQUIRED ELECTRICAL EQUIPMENT
FAA AC 25-15 : 1989 APPROVAL OF FLIGHT MANAGEMENT SYSTEMS IN TRANSPORT CATEGORY AIRPLANES
FAA AC 25.1329-1 : 2016 APPROVAL OF FLIGHT GUIDANCE SYSTEMS
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
FAA N 8000.326 : 2006 GUIDELINES FOR AIRWORTHINESS AND OPERATIONAL APPROVAL AND PROCEDURE DESIGN FOR NON-14 CFR PART 97 RNP SAAAR APPROACH PROCEDURES
FAA AC 20-183 : 2014 LASER AIRWORTHINESS INSTALLATION GUIDANCE
FAA AC 20-131 : 0 AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2) AND MODE S TRANSPONDERS
MIL-HDBK-525 Base Document:2013 ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM
SAE ARP 6461 : 2013 GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT
FAA AC 20-185 : 2015 AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM
FAA AC 25-12 : 0 AIRWORTHINESS CRITERIA FOR THE APPROVAL OF AIRBORNE WINDSHEAR WARNING SYSTEMS IN TRANSPORT CATEGORY AIRPLANES
FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
FAA AC 90-101 : 2011 APPROVAL GUIDANCE FOR RNP PROCEDURES WITH AR
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 AIR 5128 : 2012 ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS
FAA AC 20-172 : 2015 AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS
FAA AC 25-25 : 2014 PERFORMANCE AND HANDLING CHARACTERISTICS IN ICING CONDITIONS
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 25.1362-1 : 2007 ELECTRICAL SUPPLIES FOR EMERGENCY CONDITIONS
FAA AC 39-8 : 0 CONTINUED AIRWORTHINESS ASSESSMENTS OF POWERPLANT AND AUXILIARY POWER UNIT INSTALLATIONS OF TRANSPORT CATEGORY AIRPLANES
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

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