SAE ARP 4754 : 2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
Superseded date
28-12-2023
Superseded by
Published date
21-12-2010
Publisher
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Specifies the development of aircraft systems taking into account the overall aircraft operating environment and functions.
| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy |
| SAE AIR 5451 : 2017 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
| 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 |
| SAE AS 5506/1 : 2015 | SAE ARCHITECTURE ANALYSIS AND DESIGN LANGUAGE (AADL) ANNEX VOLUME 1: ANNEX A: ARINC653 ANNEX, ANNEX C: CODE GENERATION ANNEX, ANNEX E: ERROR MODEL ANNEX |
| FAA 8110.105 : 2017 | SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE |
| 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 |
| BS ISO/IEC/IEEE 15288:2015 | Systems and software engineering. System life cycle processes |
| 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 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| IEC 62396-3:2013 | Process management for avionics - Atmospheric radiation effects - Part 3: System design optimization to accommodate the single event effects (SEE) of atmospheric radiation |
| ISO/IEC/IEEE 15288:2015 | Systems and software engineering — System life cycle processes |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| SAE AIR 5317 : 2011 | A GUIDE TO APU HEALTH MANAGEMENT |
| ARINC 655 : 1999 | REMOTE DATA CONCENTRATOR (RDC) GENERIC DESCRIPTION |
| SAE ARP 6803 : 2016 | IVHM CONCEPTS, TECHNOLOGY AND IMPLEMENTATION OVERVIEW |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-55(PT1)/3(2014) : 2014 | REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-56(PT1)/5(2014) : 2014 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-056(PT2)/5(2017) : 2017 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE ON ESTABLISHING A MEANS OF COMPLYING WITH PART 1 |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-56(PT1)/6(2015) : 2015 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 12/30276658 DC : 0 | BS IEC 62396-3 ED 1.0 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 3: OPTIMISING SYSTEM DESIGN TO ACCOMMODATE THE SINGLE EVENT EFFECTS (SEE) OF ATMOSPHERIC RADIATION |
| ARINC 781:2017 | MARK 3 AVIATION SATELLITE COMMUNICATIONS SYSTEMS |
| 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 |
| ARINC 660A : 2001 | CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES |
| SAE AIR5691A : 2017 | GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
| FAA AC 20-173 : 2011 | INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| SAE ARP 6001 : 2012 | AEROSPACE - PASSIVE SIDE STICK UNIT, GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS |
| SAE AS 6163 : 2015 | TEMPERATURE CONTROLLED CONTAINER - PERFORMANCE REQUIREMENTS AND TEST PARAMETERS |
| FAA AC 20-148 : 2004 | REUSABLE SOFTWARE COMPONENTS |
| FAA 8110.55 : 2016 | HOW TO EVALUATE AND ACCEPT PROCESSES FOR AERONAUTICAL DATABASE SUPPLIERS |
| SAE AIR 6027 : 2017 | CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES |
| FAA AC 20-153 : 2016 | ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES |
| SAE AS 6019 : 2012 | ARC FAULT CIRCUIT BREAKER (AFCB), AIRCRAFT, TRIP-FREE 28 VDC |
| SAE ARP 5890 : 2011 | GUIDELINES FOR PREPARING RELIABILITY ASSESSMENT PLANS FOR ELECTRONIC ENGINE CONTROLS |
| SAE ARP 1598 : 2013(R2018) | LANDING GEAR SYSTEM DEVELOPMENT PLAN |
| SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AS 6858 : 2017 | INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT |
| DEFSTAN 00-55(PT1)/4(2016) : 2016 | REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| VDI 4007:2012-06 | Reliability goals - Determination, check, review, certificate |
| VDI 4003:2007-03 | Reliability management |
| ARINC 832 : 2016 | CABIN EQUIPMENT INTERFACES, 4GCN CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM, CABIN DISTRIBUTION SYSTEM |
| FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
| BS ISO/IEC TR 15942:2000 | Information technology. Programming languages. Guide for the use of the Ada programming language in high integrity systems |
| DD IEC TS 62396-3 : DRAFT OCT 2008 | PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 3: OPTIMISING SYSTEM DESIGN TO ACCOMMODATE THE SINGLE EVENT EFFECTS (SEE) OF ATMOSPHERIC RADIATION |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| BS IEC 62396-3:2013 | Process management for avionics. Atmospheric radiation effects System design optimization to accommodate the single event effects (SEE) of atmospheric radiation |
| FAA AC 20-165 : 2015 | AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS |
| RG.AERO 00044 : 2014 | ARP4754A/ED-79A APPLICATION GUIDE |
| FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
| FAA 8400.14 : 0 | AIR CARRIER IFR APPROVAL FOR TRANSPONDER LANDING SYSTEM SPECIAL CATEGORY 1 APPROACHES |
| SAE AS 5116 : 2003 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR GROUND ICE DETECTION SYSTEMS |
| IEC TS 62396-3:2008 | Process management for avionics - Atmospheric radiation effects - Part 3: Optimising system design to accommodate the single event effects (SEE) of atmospheric radiation |
| SAE ARP 6200 : 2014 | TEST REQUIREMENTS AND MEANS FOR COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
| SAE ARP 5150 : 2013 | SAFETY ASSESSMENT OF TRANSPORT AIRPLANES IN COMMERCIAL SERVICE |
| FAA N 8110.110 : 2010 | SOFTWARE APPROVAL GUIDE LINES, CONTINUED |
| SAE AIR 5937 : 2012 | INFORMATION ON ELECTRIC BRAKES |
| 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 ARP 5151 : 2013 | SAFETY ASSESSMENT OF GENERAL AVIATION AIRPLANES AND ROTORCRAFT IN COMMERCIAL SERVICE |
| SAE AIR6326 : 2015 | AIRCRAFT ELECTRICAL POWER SYSTEMS, MODELING AND SIMULATION, DEFINITIONS |
| SAE ARP 5416 : 2013 | AIRCRAFT LIGHTNING TEST METHODS |
| SAE AS 5498 : 2017 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
| SAE AIR 4766 : 2012 | AIR QUALITY FOR COMMERCIAL AIRCRAFT CABINS |
| AOP 52 : 2016 | GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS |
| FAA AC 00-66 : 2015 | SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY |
| EIA STD 4899 : 2017-05 | REQUIREMENTS FOR AN ELECTRONIC COMPONENTS MANAGEMENT PLAN |
| EIA 933 : 2015 | REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE AIR 5372 : 2014 | INFORMATION ON BRAKE-BY-WIRE (BBW) BRAKE CONTROL SYSTEMS |
| FAA AC 43-216 : 2017 | SOFTWARE MANAGEMENT DURING AIRCRAFT MAINTENANCE |
| SAE AS 9115 : 2017 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE, AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO 9100:2016) |
| CAN/CSA-ISO/IEC/IEEE 15288:16 | Systems and software engineering - System life cycle processes (Adopted ISO/IEC/IEEE 15288:2015, first edition, 2015-05-15) |
| SAE AIR 825/6 : 2015 | ON BOARD OXYGEN GENERATING SYSTEMS (MOLECULAR SIEVE) |
| 16/30244282 DC : 0 | BS EN 9115 - QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100) |
| 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 |
| 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 AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE ARP 5764 : 2013(R2018) | AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS |
| SAE ARP 1070E : 2019 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| RG.AERO 00028 : 2005 | ED-80/RTCA DO254 APPLICATION GUIDE |
| 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 ARP 5120 : 2016 | AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE ARP 1070 : 2014 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| ARINC 825 : 2015 | GENERAL STANDARDIZATION OF CAN (CONTROLLER AREA NETWORK) BUS PROTOCOL FOR AIRBORNE USE |
| ASTM F 3178 : 2016 | Standard Practice for Operational Risk Assessment of Small Unmanned Aircraft Systems (sUAS) |
| FAA AC 25.1329-1 : 2016 | APPROVAL OF FLIGHT GUIDANCE SYSTEMS |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| RG.AERO 000721 : 2016 | GENERAL RECOMMENDATIONS FOR THE BIT ARCHITECTURE IN AN INTEGRATED SYSTEM |
| SAE AIR 6218 : 2012 | CONSTRUCTING DEVELOPMENT ASSURANCE PLAN FOR INTEGRATED SYSTEMS |
| SAE ARP 6109 : 2014 | ELECTRONIC ENGINE CONTROL HARDWARE CHANGE MANAGEMENT |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| SAE ARP 1595 : 2013(R2019) | DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
| SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
| SAE ARP 4752 : 2013 | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AIR 4766/2 : 2011 | AIRBORNE CHEMICALS IN AIRCRAFT CABINS |
| ARINC 771 : 2016 | LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEM |
| SAE ARP 5415 : 2008 | USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
| ARINC 842 : 2013 | GUIDANCE FOR USAGE OF DIGITAL CERTIFICATES |
| PREN 9115 : 200P1 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100) |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| FAA AC 20-172 : 2015 | AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS |
| ARINC 808 : 2010 | 3GCN - CABIN DISTRIBUTION SYSTEM |
| 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 |
| FAA AC 33-7 : 2009 | GUIDANCE FOR 30-SECOND AND 2-MINUTE ONE-ENGINE-INOPERATIVE (OEI) RATINGS FOR ROTORCRAFT TURBINE ENGINES |
| 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 ARP6461A:2021 | Guidelines for Implementation of Structural Health Monitoring on Fixed Wing Aircraft |
| SAE AS6858:2017(R2023) | Installation of Fuel Cell Systems in Large Civil Aircraft |
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