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SAE AIR 5451 : 2017
|
A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
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DD IEC TS 62396-1 : DRAFT JUL 2006
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PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT |
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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 |
|
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 20-148 : 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 |