• MIL HDBK 516 : C

    Current The latest, up-to-date edition.
    Add to Watchlist
    This Standard has been added successfully to your Watchlist.
    Please visit My Watchlist to see all standards that you are watching.
    Please log in or to add this standard to your Watchlist.
    We could not add this standard to your Watchlist.
    Please retry or contact support for assistance.
    We could not add this standard to your Watchlist.
    Please retry or contact support for assistance.
    You have already added this standard to your Watchlist.
    Visit My Watchlist to view the full list.

    AIRWORTHINESS CERTIFICATION CRITERIA

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

    Add to Watchlist

    Add To Cart

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

    FOREWORD
    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. DEFINITIONS AND ABBREVIATIONS
    4. SYSTEMS ENGINEERING
    5. STRUCTURES
    6. FLIGHT TECHNOLOGY
    7. PROPULSION AND PROPULSION INSTALLATIONS
    8. AIR VEHICLE SUBSYSTEMS
    9. CREW SYSTEMS
    10. DIAGNOSTICS SYSTEMS
    11. AVIONICS
    12. ELECTRICAL SYSTEM
    13. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E[3])
    14. SYSTEM SAFETY
    15. COMPUTER SYSTEMS AND SOFTWARE
    16. MAINTENANCE
    17. ARMAMENTS AND STORES INTEGRATION
    18. PASSENGER SAFETY
    19. MATERIALS
    20. AIR TRANSPORTABILITY, AIRDROP, MISSION/TEST
        EQUIPMENT AND CARGO/PAYLOAD SAFETY
    21. NOTES
    APPENDIX A - AIRWORTHINESS CERTIFICATION CRITERIA
                 POINTS OF CONTACT

    Abstract - (Show below) - (Hide below)

    Sets up the airworthiness certification criteria, standards and methods of compliance to be used in the determination of airworthiness of all manned and unmanned, fixed and rotary wing air systems.

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

    Committee AREA SESS
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    MIL HDBK 510-1 : A AEROSPACE FUELS CERTIFICATION
    MIL HDBK 525 : 0 ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM
    MIL STD 1798 : C MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
    MIL HDBK 510 : A AEROSPACE FUELS CERTIFICATION
    MIL STD 3050 : 0 AIRCRAFT CREW BREATHING SYSTEMS USING ON-BOARD OXYGEN GENERATING SYSTEM (OBOGS)
    MIL HDBK 87213 : A ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS
    MIL HDBK 514 : 0 OPERATIONAL SAFETY, SUITABILITY, & EFFECTIVENESS FOR THE AERONAUTICAL ENTERPRISE
    MIL STD 1791 : C DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
    SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS
    SAE AIR 6027 : 2017 CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES
    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL HDBK 6870 : B NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL-HDBK-6870C:2020 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    RTCA DO 200B : 2015 STANDARDS FOR PROCESSING AERONAUTICAL DATA
    MIL PRF 8565 : K BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 8865 : B AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    FAA AC 20-140 : 2016 GUIDELINES FOR DESIGN APPROVAL OF AIRCRAFT DATA LINK COMMUNICATION SYSTEMS SUPPORTING AIR TRAFFIC SERVICES (ATS)
    MIL STD 188 243 : A TACTICAL SINGLE CHANNEL ULTRA HIGH FREQUENCY (UHF) RADIO COMMUNICATIONS
    STANAG 3971 : 2013 AIR-TO-AIR REFUELLING - ATP-56
    FAA AC 20-170 : 2010 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    FAA AC 25.981-2 : 2008 FUEL TANK FLAMMABILITY REDUCTION MEANS
    FAA AC 33-1 : 0 TURBINE ENGINE FOREIGN OBJECT INGESTION AND ROTOR BLADE CONTAINMENT TYPE CERTIFICATION PROCEDURES
    FAA AC 20-119 : 1983 FUEL DRAIN VALVES
    NASA STD 7009 : 2016 STANDARD FOR MODELS AND SIMULATIONS
    RTCA DO 219 : 1993 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR ATC TWO-WAY DATA LINK COMMUNICATIONS
    STANAG 4671 : 2017 UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS (USAR)
    JSSG 2010 3 : 1998 CREW SYSTEMS COCKPIT/CREW STATIONS/CABIN HANDBOOK
    MIL HDBK 61 : A CONFIGURATION MANAGEMENT GUIDANCE
    MIL STD 1530 : D AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    ARINC 653 : 1997 SUPP 1 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE
    IEEE 1074 : 2006 DEVELOPING A SOFTWARE PROJECT LIFE CYCLE PROCESS
    FAA AC 20-60 : 1968 ACCESSIBILITY TO EXCESS EMERGENCY EXITS
    SAE ARP 5580 : 2012 RECOMMENDED FAILURE MODES AND EFFECTS ANALYSIS (FMEA) PRACTICES FOR NON-AUTOMOBILE APPLICATIONS
    RTCA DO 278 : A2011 SOFTWARE INTEGRITY ASSURANCE CONSIDERATIONS FOR COMMUNICATION, NAVIGATION, SURVEILLANCE AND AIR TRAFFIC MANAGEMENT (CNS/ATM) SYSTEMS
    RTCA DO 330 : 2011 SOFTWARE TOOL QUALIFICATION CONSIDERATIONS
    FAA AC 33-2 : 2013 GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
    MIL C 83124 : 0 CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR
    MIL STD 3013 : A GLOSSARY OF DEFINITIONS, GROUND RULES, AND MISSION PROFILES TO DEFINE AIR VEHICLE PERFORMANCE CAPABILITY
    ADS-65-HDBK : 2004 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS
    SAE AS 6174 : 2014 COUNTERFEIT MATERIEL - ASSURING ACQUISITION OF AUTHENTIC AND CONFORMING MATERIEL
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    JSSG 2010/9 : 1998 CREW SYSTEMS PERSONAL PROTECTION EQUIPMENT HANDBOOK
    RTCA DO 189 : 1985 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE DISTANCE MEASURING EQUIPMENT (DME) OPERATING WITHIN THE RADIO FREQUENCY RANGE OF 960-1215 MHZ
    MIL HDBK 704/6 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, 60 HZ, 115 VOLT (PART 6 OF 8 PARTS)
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL STD 1683 : B CONNECTORS AND JACKETED CABLE, ELECTRIC, SELECTION STANDARD FOR SHIPBOARD USE
    SAE ARP 1493 : 2013 WHEEL AND BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    ASTM F 735 : 2017 : REDLINE Standard Test Method for Abrasion Resistance of Transparent Plastics and Coatings Using the Oscillating Sand Method
    SAE AS 9102 : 2014 AEROSPACE FIRST ARTICLE INSPECTION REQUIREMENT
    FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
    MIL PRF 29595 : A BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL E 22285 : 0 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
    FAA AC 120-40 : 0 AIRPLANE SIMULATOR QUALIFICATION
    MIL HDBK 1763 : 0 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
    IEEE 828 : 2012 CONFIGURATION MANAGEMENT IN SYSTEMS AND SOFTWARE ENGINEERING
    ATP 56 : B AIR TO AIR REFUELLING
    NASA STD 8719.13 : 2013 SOFTWARE SAFETY STANDARD
    AFGS 87219 : B ELECTRICAL POWER SYSTEMS, AIRCRAFT
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    STANAG 4591 : 2008 THE 600 BIT/S, 1200 BIT/S AND 2400 BIT/S NATO INTEROPERABLE NARROW BAND VOICE CODER
    SAE ARP 5089 : 1996 COMPOSITE REPAIR NDT/NDI HANDBOOK
    MIL STD 188/141 : C INTEROPERABILITY AND PERFORMANCE STANDARDS FOR MEDIUM AND HIGH FREQUENCY RADIO SYSTEMS
    MIL D 23222 : A DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    AOP 52 : 2016 GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS
    MIL PRF 81757 : D BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT - GENERAL SPECIFICATION FOR
    FAA AC 33-4 : 0 DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES
    RTCA DO 185 : B2008 CHG NOT 2 13 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 2 (TCAS 2)
    RTCA DO 212 : 1992 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE AUTOMATIC DEPENDENT SURVEILLANCE (ADS) EQUIPMENT
    SAE ARP 8615 : 2011 FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
    MIL HDBK 704/1 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS (PART 1 OF 8 PARTS)
    SAE AS 6081 : 2012 FRAUDULENT/COUNTERFEIT ELECTRONIC PARTS: AVOIDANCE, DETECTION, MITIGATION, AND DISPOSITION - DISTRIBUTORS
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL E 85583 : A ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    MIL T 81259 : B TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
    MIL HDBK 244 : A GUIDE TO AIRCRAFT - STORES COMPATIBILITY
    SAE AS 4273 : 2007 FIRE TESTING OF FLUID HANDLING COMPONENTS FOR AIRCRAFT ENGINES AND AIRCRAFT ENGINE INSTALLATIONS
    MIL STD 1787 : B AIRCRAFT DISPLAY SYMBOLOGY
    STANAG 3278 : 2014 AIRCRAFT TOWING ATTACHMENTS AND DEVICES
    FAA AC 25.994-1 : 0 DESIGN CONSIDERATIONS TO PROTECT FUEL SYSTEMS DURING A WHEELS-UP LANDING
    AFGS 87139 : B LANDING GEAR SYSTEMS
    FAA AC 33.4-2 : 0 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY
    MIL PRF 21480 : B GENERATOR SYSTEM, ELECTRIC POWER, 400 HERTZ, ALTERNATING CURRENT, AIRCRAFT - GENERAL SPECIFICATION FOR
    FAA AC 25-16 : 0 ELECTRICAL FAULT AND FIRE PREVENTION AND PROTECTION
    MIL B 8584 : C BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
    MIL HDBK 704/5 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS THREE PHASE, VARIABLE FREQUENCY, 115 VOLT (PART 5 OF 8 PARTS)
    JSSG 2000 : B AIR SYSTEM
    ASTM G 85 : 2011 : REDLINE Standard Practice for Modified Salt Spray (Fog) Testing
    JSSG 2007 : 0 JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE
    MIL STD 3022 : 0 DOCUMENTATION OF VERIFICATION, VALIDATION, AND ACCREDITATION (VV&A) FOR MODELS AND SIMULATIONS
    SAE ARP 1538 : 2013 ARRESTING HOOK INSTALLATION, LAND-BASED AIRCRAFT
    ATP 3.3.4.2 : 2013 AIR TO AIR REFUELLING
    MIL STD 1791 : C DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
    SAE AIR 1419 : 2013 INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES
    MIL DTL 25959 : H TIE DOWN, TENSIONERS, CARGO, AIRCRAFT
    MIL STD 46855 : A HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT, AND FACILITIES
    SAE AS 1055 : 2013 FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS
    JSSG 2010 13 : 1998 CREW SYSTEMS SURVIVAL, SEARCH, AND RESCUE (SSAR) HANDBOOK
    JSSG 2010 10 : 0 CREW SYSTEMS OXYGEN SYSTEMS HANDBOOK
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    JSSG 2010 : 1998 CREW SYSTEMS
    CFR 21(PTS800-1299) : 0 FOOD AND DRUGS - FOOD AND DRUG ADMINISTRATION, CHAPTER 1 DEPARTMENT OF HEALTH AND HUMAN SERVICES - PARTS 800-1299
    ISO/IEC/IEEE 24765:2017 Systems and software engineering Vocabulary
    FAA AC 33-3 : 0 TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
    MIL L 85314 : A LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR
    MIL STD 1760 : E AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    ASTM F 2156 : 2017 : REDLINE Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    IEEE 12207 : 2008 SYSTEMS AND SOFTWARE ENGINEERING - SOFTWARE LIFE CYCLE PROCESSES
    SAE AS 8091 : 2014 AIRCRAFT JACKING PADS ADAPTERS AND SOCKETS DESIGN AND INSTALLATION OF
    MIL E 7016 : F ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    MIL STD 411 : F AIRCREW STATION ALERTING SYSTEMS
    MIL STD 8591 : 0 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE)
    MIL PRF 7032 : H INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
    NASA GB 8719.13 : 0 NASA SOFTWARE SAFETY GUIDEBOOK
    FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
    SAE AS 5726 : 2013 INTERFACE STANDARD, INTERFACE FOR MICRO MUNITIONS
    FAA AC 20-131 : 0 AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2) AND MODE S TRANSPONDERS
    MIL HDBK 454 : B GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    MIL STD 889 : C DISSIMILAR METALS
    JSSG 2010 7 : 0 CREW SYSTEMS - CRASH PROTECTION HANDBOOK
    MIL HDBK 704/8 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS 28 VDC (PART 8 OF 8 PARTS)
    MIL P 83126 : A PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
    MIL HDBK 828 : C RANGE LASER SAFETY
    SAE AS 9100D : 2016 QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    FAA AC 20-42 : 2011 HAND FIRE EXTINGUISHERS FOR USE IN AIRCRAFT
    JSSG 2010 6 : 1998 CREW SYSTEMS SUBTENANCE AND WASTE MANAGEMENT HANDBOOK
    MIL HDBK 515 : 0 WEAPON SYSTEM INTEGRITY GUIDE (WSIG)
    MIL DTL 85110 : B BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR
    MIL PRF 63029 : J MANUALS, TECHNICAL: REQUIREMENTS FOR OPERATOR'S MANUALS AND CHECKLISTS FOR MANNED AND UNMANNED AIRCRAFT SYSTEMS
    MIL STD 38784 : A GENERAL STYLE AND FORMAT REQUIREMENTS FOR TECHNICAL MANUALS
    MIL HDBK 2066 : 0 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
    SAE AS 1426 : 1980 STANDARD GALLEY SYSTEM SPECIFICATION, PART 1, PERFORMANCE, DESIGN DEVELOPMENT
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    MIL STD 464 : C ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    STANAG 3230 : 2007 EMERGENCY MARKINGS ON AIRCRAFT
    MIL PRF 27260 : D TIE DOWN, CARGO, AIRCRAFT CGU-1/B
    ANSI Z136.1 : 2014 SAFE USE OF LASERS
    MIL STD 1796 : A AVIONICS INTEGRITY PROGRAM (AVIP)
    STANAG 7191 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
    ASTM F 330 : 2016 : REDLINE Standard Test Method for Bird Impact Testing of Aerospace Transparent Enclosures
    ASTM D 2247 : 2015 : REDLINE Standard Practice for Testing Water Resistance of Coatings in 100 % Relative Humidity
    STANAG 3098 : 2014 AIRCRAFT JACKING
    MIL STD 1310 : H SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY
    SAE AS 9103 : 2012 AEROSPACE SERIES - QUALITY MANAGEMENT SYSTEMS - VARIATION MANAGEMENT OF KEY CHARACTERISTICS
    ASTM D 1044 : 2013 : REDLINE Standard Test Method for Resistance of Transparent Plastics to Surface Abrasion
    SAE ARP1870A:1987(S2012) Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)
    MIL HDBK 704/2 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, 400 HZ, 115 VOLT (PART 2 OF 8 PARTS)
    ASME Y14.5 : 2009 DIMENSIONING AND TOLERANCING
    MIL F 17874 : B FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    ATP 3.3.4.5 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    MIL L 85762 : A LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    JSSG 2010 1 : 1998 CREW SYSTEMS ENGINEERING HANDBOOK
    SAE AS 1831 : 1997 ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
    MIL STD 1568 : D MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL L 8552 : C LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
    MIL PRF 5920 : F MANUALS, TECHNICAL - SAMPLE BASIC WEIGHT CHECKLISTS AND LOADING DATA
    JSSG 2001 : B AIR VEHICLE
    MIL HDBK 5400 : 0 ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR
    SAE AS 8049/1 : 2016 PERFORMANCE STANDARDS FOR SIDE-FACING SEATS IN CIVIL ROTORCRAFT, TRANSPORT AIRCRAFT, AND GENERAL AVIATION AIRCRAFT
    MIL STD 1290 : A LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE
    MIL STD 3024 : 0 PROPULSION SYSTEM INTEGRITY PROGRAM (PSIP)
    MIL HDBK 217 : F RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    SAE AS 8049 : 2015 PERFORMANCE STANDARD FOR SEATS IN CIVIL ROTORCRAFT, TRANSPORT AIRCRAFT, AND GENERAL AVIATION AIRCRAFT
    MMPDS 08 : 2013 METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) - COMPLETE SET INCLUDES 9 CHAPTERS
    MIL S 8812 : D STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
    SAE ARP 1834 : 1997 FAULT/FAILURE ANALYSIS FOR DIGITAL SYSTEMS AND EQUIPMENT
    FAA AC 20-145 : 2003 GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS
    MIL STD 461 : G REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MIL HDBK 2165 : 0 TESTABILITY PROGRAM FOR SYSTEMS AND EQUIPMENTS
    ISO/IEC 12207:2008 Systems and software engineering Software life cycle processes
    MIL STD 27733 : 0 MODIFICATION AND MARKING REQUIREMENTS FOR TEST EQUIPMENT IN AEROSPACE VEHICLES AND RELATED SUPPORT EQUIPMENT
    JSSG 2010 11 : 1998 CREW SYSTEMS EMERGENCY EGRESS HANDBOOK
    MIL STD 3009 : 0 LIGHTING, AIRCRAFT, NIGHT VISION IMAGING SYSTEM (NVIS) COMPATIBLE
    MIL STD 188/242 : 0 INTEROPERABILITY AND PERFORMANCE STANDARDS FOR TACTICAL SINGLE CHANNEL VERY HIGH FREQUENCY (VHF) RADIO EQUIPMENT
    MIL HDBK 87213 : A ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS
    NFPA 70 : 2017 NATIONAL ELECTRICAL CODE
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    MIL STD 1399/300 : B ELECTRIC POWER, ALTERNATING CURRENT
    FAA AC 120-63 : 0 HELICOPTER SIMULATOR QUALIFICATION
    IEEE C95.1 : 2005 SAFETY LEVELS WITH RESPECT TO HUMAN EXPOSURE TO RADIO FREQUENCY ELECTROMAGNETIC FIELDS, 3 KHZ TO 300 GHZ
    MIL T 6053 : C TEST, IMPACT, SHOCK ABSORBER, LANDING GEAR, AIRCRAFT
    MIL HDBK 299 : 0 CABLE COMPARISON HANDBOOK DATA PERTAINING TO ELECTRIC SHIPBOARD CABLE
    MIL PRF 5041 : K TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
    NFPA 1 : 2018 FIRE CODE
    AFGS 87256 : (1) INTEGRATED DIAGNOSTICS
    JSSG 2010 14 : 1998 CREW SYSTEMS AIRCRAFT WINDSHIELD/CANOPY SYSTEMS AND TRANSPARENT ENCLOSURES HANDBOOK
    SAE AIR 5826 : 2017 DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
    RTCA DO 186 : B2005 Minimum Operational Performance Standards for Airborne Radio Communications Equipment Operating Within the Radio Frequency Range 117.975 - 137.000 MHz
    MIL DTL 7700 : H FLIGHT MANUAL, PERFORMANCE DATA APPENDIX, MISSION CREW MANUAL, SUPPLEMENTAL MANUAL, AND ABBREVIATED FLIGHT CREW CHECKLIST
    SAE ARP 5583 : 2010 GUIDE TO CERTIFICATION OF AIRCRAFT IN A HIGH-INTENSITY RADIATED FIELD (HIRF) ENVIRONMENT
    IEEE 1220 : 2005 STANDARD FOR APPLICATION AND MANAGEMENT OF THE SYSTEMS ENGINEERING PROCESS
    MIL STD 7179 : A FINISHES, COATINGS, AND SEALANTS, FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEMS
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    SAE AS 18012 : 1998 MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF
    MIL STD 1399/390 : 0 INTERFACE STANDARD FOR SHIPBOARD SYSTEMS - ELECTRIC POWER, DIRECT CURRENT, (OTHER THAN SHIP'S BATTERY) FOR SUBMARINES (METRIC)
    STANAG 3447 : 2016 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
    MIL W 5013 : L WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR
    FAA AC 91-85 : 2016 AUTHORIZATION OF AIRCRAFT AND OPERATORS FOR FLIGHT IN REDUCED VERTICAL SEPARATION MINIMUM (RVSM) AIRSPACE
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    IEEE 1012 : 2012 SYSTEM, SOFTWARE, AND HARDWARE VERIFICATION AND VALIDATION
    JSSG 2009 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    MIL STD 1472 : G HUMAN ENGINEERING
    RTCA DO 333 : 2011 FORMAL METHODS SUPPLEMENT TO DO-178C AND DO-278A
    FAA AC 20-30 : 0 AIRCRAFT POSITION LIGHT AND ANTICOLLISION LIGHT INSTALLATIONS
    MIL STD 188/181 : C CHANGE 3 INTEROPERABILITY STANDARD FOR ACCESS TO 5-KHZ AND 25-KHZ UHF SATELLITE COMMUNICATIONS CHANNELS
    SAE ARP 1420 : 2002 GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
    JSSG 2010 12 : 0 CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK
    SAE AMS 3694 : 2012 AERODYNAMIC SMOOTHING COMPOUND, FLEXIBLE, -55 DEGREES TO +130 DEGREES C (-65 DEGREES TO +270 DEGREES F)
    STANAG 4101 : 0 TOWING ATTACHMENTS
    MIL HDBK 704/4 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, VARIABLE FREQUENCY, 115 VOLT (PART 4 OF 8 PARTS)
    RTCA DO 181 : E2011 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIR TRAFFIC CONTROL RADAR BEACON SYSTEM/MODE SELECT (ATCRBS/MODE S) AIRBORNE EQUIPMENT
    FAA AC 25.963-1 : 0 FUEL TANK ACCESS COVERS
    MIL DTL 85025 : B NATOPS PROGRAM TECHNICAL PUBLICATIONS AND PRODUCTS - STYLE, FORMAT, AND COMMON TECHNICAL CONTENT
    JSSG 2010 2 : 1998 CREW SYSTEMS CREW STATION AUTOMATION, INFORMATION AND CONTROL DISPLAY MANAGEMENT HANDBOOK
    MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    FAA AC 90-96 : 2005 APPROVAL OF U.S. OPERATORS AND AIRCRAFT TO OPERATE UNDER INSTRUMENT FLIGHT RULES (IFR) IN EUROPEAN AIRSPACE DESIGNATED FOR BASIC AREA NAVIGATION (B-RNAV)/RNAV 5 AND PRECISION AREA NAVIGATION (P-RNAV)
    MIL-STD-1474E:2015 NOISE LIMITS
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    MIL HDBK 310 : 0 DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS
    RTCA DO 331 : 2011 MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A
    STANAG 3899 : 0 GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES
    MIL HDBK 1599 : A BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
    MIL STD 805 : B TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
    FAA AC 33.76-1 : 2009 BIRD INGESTION CERTIFICATION STANDARDS
    FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
    FAA AC 25-9 : 0 SMOKE DETECTION, PENETRATION AND EVACUATION TESTS AND RELATED FLIGHT MANUAL EMERGENCY PROCEDURES
    MIL HDBK 470 : A DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1
    EIA 632 : 1999 PROCESSES FOR ENGINEERING A SYSTEM
    ADS-63-SP : 2001 AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS
    SAE AS 8584 : 2013 BRAKE SYSTEMS, WHEEL, MILITARY AIRCRAFT
    MIL HDBK 1587 : 0 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 25.981-1 : 2008 FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
    FAA AC 33-5 : 0 TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
    MIL PRF 5096 : F MANUALS, TECHNICAL - INSPECTION AND MAINTENANCE REQUIREMENTS - ACCEPTANCE AND FUNCTIONAL CHECK FLIGHT PROCEDURES AND CHECKLISTS - INSPECTION WORK CARDS, AND CHECKLISTS, PREPARATION OF
    MIL PRF 85676 : A LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY
    SAE ARP 1070 : 2014 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    MIL HDBK 6870 : B NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    FAA AC 120-42 : 2008 EXTENDED OPERATIONS (ETOPS AND POLAR OPERATIONS)
    MIL STD 331 : D FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR
    MIL STD 2161 : C PAINT SCHEMES AND EXTERIOR MARKINGS FOR U.S. NAVY AND MARINE CORPS AIRCRAFT
    FAA AC 43.13-1 : 0 ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR
    FAA AC 20-41 : A SUBSTITUTE TECHNICAL STANDARD ORDER (TSO) AIRCRAFT EQUIPMENT
    FAA AC 25.853-1 : 0
    EIA SEB6 : A1990 SYSTEM SAFETY ENGINEERING IN SOFTWARE DEVELOPMENT
    GEIA EIA649B:2011 CONFIGURATION MANAGEMENT STANDARD
    MIL STD 1798 : C MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
    MIL HDBK 704/7 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS 270 VDC (PART 7 OF 8 PARTS)
    SAE ARP 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    FED STD 595 : C COLORS USED IN GOVERNMENT PROCUREMENT
    NASA STD 8739.8 : 2004 SOFTWARE ASSURANCE STANDARD
    RTCA DO 236 : C2013 CHG 1 2014 MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION
    MIL STD 1289 : D AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS
    MIL PRF 7115/4 : A CONVERTER, AIRCRAFT 300 AMPERE, TYPE 2, CLASS A, FAN COOLED
    RTCA DO 255 : 2000 Requirements Specification for Avionics Computer Resource (ACR)
    FAA AC 25-17 : 2009 TRANSPORT AIRPLANE CABIN INTERIORS CRASHWORTHINESS HANDBOOK
    MIL A 19736 : A AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    FAA AC 20-128 : 0 DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
    MIL STD 188/182 : B CHANGE 3 INTEROPERABILITY STANDARD FOR UHF SATCOM DAMA ORDERWIRE MESSAGES AND PROTOCOLS
    MIL HDBK 221 : 0 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
    RTCA DO 297 : 2005 Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations
    JSSG 2010 5 : 0 CREW SYSTEMS AIRCRAFT LIGHTING HANDBOOK
    FAA AC 25.869-1 : 2007 FIRE PROTECTION: SYSTEMS
    MIL HDBK 419 : A GROUNDING, BONDING, AND SHIELDING FOR ELECTRONIC EQUIPMENTS AND FACILITIES - VOLUME 1: BASIC THEORY & VOLUME 2: APPLICATIONS
    FAA AC 20-148 : 2004 REUSABLE SOFTWARE COMPONENTS
    FAA AC 20-29 : 0 USE OF AIRCRAFT FUEL ANTI-ICING ADDITIVES
    MIL HDBK 2084 : 0 GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT
    RTCA DO 332 : 2011 OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A
    SAE AIR 4845 : 1993 THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT
    SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
    MIL HDBK 1760 : A AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    ARINC 609 : 1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS
    MIL STD 1425 : A SAFETY DESIGN REQUIREMENTS FOR MILITARY LASERS AND ASSOCIATED SUPPORT EQUIPMENT
    MIL HDBK 704/3 : 0 GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS THREE PHASE, 400 HZ, 115 VOLT (PART 3 OF 8 PARTS)
    MIL STD 961 : E DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
    FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective