MIL-HDBK-516 Revision C:2014
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AIRWORTHINESS CERTIFICATION CRITERIA
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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
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.
| Committee |
AREA SESS
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| DocumentType |
Standard
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| Pages |
528
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-HDBK-525 Base Document:2013 | ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM |
| MIL-STD-1791 Revision C:2017 | DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| MIL-STD-3050 Base Document:2015 | AIRCRAFT CREW BREATHING SYSTEMS USING ON-BOARD OXYGEN GENERATING SYSTEM (OBOGS) |
| SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| SAE AIR6027A | Considerations for Safe Store Operation on Manned and Unmanned Vehicles |
| MIL-HDBK-6870 Revision B:2012 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL-HDBK-6870 Revision C:2020 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL-HDBK-87213 Revision A:2005 | Electronically / Optically Generated Airborne Displays |
| MIL-HDBK-514 Base Document:2003 | OPERATIONAL SAFETY, SUITABILITY, & EFFECTIVENESS FOR THE AERONAUTICAL ENTERPRISE |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
| MIL-PRF-8565 Revision K:2001 | BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8865 Revision B:1987 | 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 Revision A:2014 | 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 Base Document:1998 | CREW SYSTEMS COCKPIT/CREW STATIONS/CABIN HANDBOOK |
| MIL-HDBK-61 Revision A:2001 | CONFIGURATION MANAGEMENT GUIDANCE |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| ARINC 653 : 1997 SUPP 1 | AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE |
| IEEE 1074-2006 | IEEE Standard for 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 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
| MIL-STD-3013 Revision A:2008 | 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 AS6174A | Counterfeit Materiel; Assuring Acquisition of Authentic and Conforming Materiel |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| JSSG-2010-9 Base Document: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 Base Document:2004 | 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 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-1683 Revision B:1989 | CONNECTORS AND JACKETED CABLE, ELECTRIC, SELECTION STANDARD FOR SHIPBOARD USE |
| SAE ARP1493C | Wheel and Hydraulically Actuated Brake Design and Test Requirements for Military Aircraft |
| MIL-A-8863 Revision C:1993 | 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 AS9102B | 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 Revision A:2011 | BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-E-22285 Base Document:1959 | EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
| FAA AC 120-40 : 0 | AIRPLANE SIMULATOR QUALIFICATION |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| IEEE 828-2012 | IEEE Standard for Configuration Management in Systems and Software Engineering |
| ATP 56 : B | AIR TO AIR REFUELLING |
| NASA STD 8719.13 : 2013 | SOFTWARE SAFETY STANDARD |
| AFGS-87219 Revision B:2012 | 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 Revision C:2011 | INTEROPERABILITY AND PERFORMANCE STANDARDS FOR MEDIUM AND HIGH FREQUENCY RADIO SYSTEMS |
| MIL-D-23222 Revision A:1971 | DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
| AOP 52 : 2016 | GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS |
| MIL-PRF-81757 Revision D:1999 | 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 |
| ASME Y14.5 : 2009 | DIMENSIONING AND TOLERANCING |
| SAE ARP8615 | Fuel System Components: General Specification For |
| MIL-HDBK-704-1 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics (Part 1 of 8 Parts) |
| SAE AS6081 | Fraudulent/Counterfeit Electronic Parts: Avoidance, Detection, Mitigation, and Disposition - Distributors |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| MIL-T-81259 Revision B:1991 | TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| SAE AS4273A | Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations |
| MIL-STD-1787 Revision B:1996 | 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 Revision B:2013 | 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 Revision B:2010 | 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 Revision C:1970 | BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
| MIL-HDBK-704-5 Base Document:2004 | 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 Revision B:2004 | AIR SYSTEM |
| ASTM G 85 : 2011 : REDLINE | Standard Practice for Modified Salt Spray (Fog) Testing |
| JSSG-2007 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
| MIL-STD-3022 Base Document:2008 | 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 Revision C:2017 | DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
| SAE AIR1419B | Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines |
| MIL-DTL-25959 Revision H:2012 | TIE DOWN, TENSIONERS, CARGO, AIRCRAFT |
| MIL-STD-46855 Revision A:2011 | HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT, AND FACILITIES |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| JSSG-2010-13 Base Document:1998 | Crew Systems Survival, Search, and Rescue (SSAR) Handbook |
| JSSG-2010-10 Base Document:1998 | Crew Systems Oxygen Systems Handbook |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| JSSG-2010 Base Document: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 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-STD-1760 Revision E:2007 | 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 AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| IEEE/ISO/IEC 12207-2008 | ISO/IEC/IEEE International Standard - 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 Revision F:1976 | 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 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
| MIL-STD-8591 Base Document:2005 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
| MIL-PRF-7032 Revision H:2010 | 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 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| JSSG-2010-7 Base Document:1998 | Crew Systems Crash Protection Handbook |
| MIL-HDBK-704-8 Base Document:2004 | 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 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-HDBK-828 Revision C:2017 | RANGE LASER SAFETY |
| SAE AS9100D | Quality Management Systems - Requirements for Aviation, Space, and Defense Organizations |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| FAA AC 20-42 : 2011 | HAND FIRE EXTINGUISHERS FOR USE IN AIRCRAFT |
| JSSG-2010-6 Base Document:1998 | Crew Systems Sustenance and Waste Management Handbook |
| MIL-HDBK-515 Base Document:2002 | WEAPON SYSTEM INTEGRITY GUIDE (WSIG) |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| MIL-PRF-63029 Revision J:2014 | MANUALS, TECHNICAL: REQUIREMENTS FOR OPERATOR'S MANUALS AND CHECKLISTS FOR MANNED AND UNMANNED AIRCRAFT SYSTEMS |
| MIL-STD-38784 Revision A:2011 | GENERAL STYLE AND FORMAT REQUIREMENTS FOR TECHNICAL MANUALS |
| MIL-HDBK-2066 Base Document:1999 | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN |
| SAE AS1426B | Standard Galley System Specification, Part I, Performance, Design, Development |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| STANAG 3230 : 2007 | EMERGENCY MARKINGS ON AIRCRAFT |
| MIL-PRF-27260 Revision D:2013 | TIE DOWN, CARGO, AIRCRAFT CGU-1/B |
| ANSI Z136.1 : 2014 | SAFE USE OF LASERS |
| MIL-STD-1796 Revision A:2011 | 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 Revision H:2009 | SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
| SAE AS9103A | 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 | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
| MIL-HDBK-704-2 Base Document:2004 | 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) |
| MIL-F-17874 Revision B:1965 | 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 ARP994B | Design of Tubing Installations for Aerospace Hydraulic Systems |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| JSSG-2010-1 Base Document:1998 | Crew Systems Engineering Handbook |
| SAE AS 1831 : 1997 | ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| MIL-L-8552 Revision C:1965 | LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
| MIL PRF 5920 : F | MANUALS, TECHNICAL - SAMPLE BASIC WEIGHT CHECKLISTS AND LOADING DATA |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| MIL-HDBK-5400 Base Document:1995 | Electronic Equipment, Airborne General Guidelines for |
| SAE AS8049/1A | Performance Standards for Side-Facing Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL-STD-3024 Base Document:2008 | PROPULSION SYSTEM INTEGRITY PROGRAM (PSIP) |
| MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
| SAE AS8049C | 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 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| MIL-STD-882 Revision E:2012 | System Safety |
| SAE ARP1834A | FAULT/FAILURE ANALYSISFor 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 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-HDBK-2165 Base Document:1995 | Testability Program for Systems and Equipments |
| ISO/IEC 12207:2008 | Systems and software engineering — Software life cycle processes |
| MIL-STD-27733 Base Document:1998 | MODIFICATION AND MARKING REQUIREMENTS FOR TEST EQUIPMENT IN AEROSPACE VEHICLES AND RELATED SUPPORT EQUIPMENT |
| JSSG-2010-11 Base Document:1998 | Crew Systems Emergency Egress Handbook |
| MIL-STD-3009 Base Document:2001 | LIGHTING, AIRCRAFT, NIGHT VISION IMAGING SYSTEM (NVIS) COMPATIBLE |
| MIL-STD-188-242 Base Document:1985 | Interoperability and Performance Standards for Tactical Single Channel Very High Frequency (VHF) Radio Equipment |
| MIL-HDBK-87213 Revision A:2005 | 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 Revision B:2008 | ELECTRIC POWER, ALTERNATING CURRENT |
| FAA AC 120-63 : 0 | HELICOPTER SIMULATOR QUALIFICATION |
| IEEE C95.1-2005 | IEEE Standard for Safety Levels with Respect to Human Exposure to Radio Frequency Electromagnetic Fields, 3 kHz to 300 GHz |
| MIL-T-6053 Revision C:1977 | Tests, Impact, Shock Absorber Landing Gear, Aircraft |
| MIL-HDBK-299 Base Document:1989 | CABLE COMPARISON HANDBOOK DATA PERTAINING TO ELECTRIC SHIPBOARD CABLE |
| MIL PRF 5041 : K | TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| NFPA 1 : 2018 | FIRE CODE |
| AFGS-87256 Base Document:1991 | INTEGRATED DIAGNOSTICS |
| SAE AIR5826B | 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 Revision H:2014 | FLIGHT MANUAL, PERFORMANCE DATA APPENDIX, MISSION CREW MANUAL, SUPPLEMENTAL MANUAL, AND ABBREVIATED FLIGHT CREW CHECKLIST |
| SAE ARP5583A | Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) Environment |
| IEEE 1220-2005 | IEEE Standard for Application and Management of the Systems Engineering Process |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| SAE AS18012 | Markings for Aircrew Station Displays Design and Configuration of |
| MIL-STD-1399-390 Base Document:1987 | 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 Revision L:1991 | 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 AS50881F | Wiring Aerospace Vehicle |
| IEEE 1012-2012 | IEEE Standard for System and Software Verification and Validation |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-STD-1472 Revision G:2012 | 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 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| SAE AMS3694B | Aerodynamic Smoothing Compound, Flexible −55° to +130°C (−65° to +270°F) |
| STANAG 4101 : 0 | TOWING ATTACHMENTS |
| MIL-HDBK-704-4 Base Document:2004 | 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 Revision B:2007 | NATOPS PROGRAM TECHNICAL PUBLICATIONS AND PRODUCTS - STYLE, FORMAT, AND COMMON TECHNICAL CONTENT |
| JSSG-2010-2 Base Document:1998 | Crew Systems Crew Station Automation, Information and Control/Display Management Handbook |
| MIL-A-18717 Revision C:1993 | 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-1474 Revision E:2015 | NOISE LIMITS |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| MIL-HDBK-310 Base Document:1997 | 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 Revision A:1997 | BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS |
| MIL-STD-805 Revision B:1987 | 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 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| 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 AS8584B | Brake Systems, Wheel, Military Aircraft |
| MIL-HDBK-1587 Base Document:1996 | 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 Revision A:2006 | LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
| SAE ARP1070D | Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility |
| MIL-HDBK-6870 Revision B:2012 | 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 Revision D:2017 | FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
| MIL-STD-2161 Revision C:2014 | 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 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| MIL-HDBK-704-7 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 270 VDC (Part 7 of 8 Parts) |
| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| FED-STD-595 Revision C:2008 | 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 Revision D:2003 | AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
| MIL-PRF-7115-4 Revision A:2014 | 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 Revision A:1960 | 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 Base Document:1965 | 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<br> |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| FAA AC 25.869-1 : 2007 | FIRE PROTECTION: SYSTEMS |
| MIL-HDBK-419 Revision A:1987 | 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 Base Document:1995 | 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 AIR4845 | THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT |
| SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
| MIL-STD-1425 Revision A:1991 | SAFETY DESIGN REQUIREMENTS FOR MILITARY LASERS AND ASSOCIATED SUPPORT EQUIPMENT |
| MIL-HDBK-704-3 Base Document:2004 | 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 Revision E:2003 | 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 |
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