MIL HDBK 516 : C

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AIRWORTHINESS CERTIFICATION CRITERIA

Available format(s): Hardcopy, PDF

Language(s): English

Published date:

Publisher: US Military Specs/Standards/Handbooks

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
ISBN
Pages
Published
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
(INACTIVE RECORD)RTCA DO 160 : G2010 CHG 1 2014	ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT
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 ARP 1870 : 2012	AEROSPACE SYSTEMS ELECTRICAL BONDING AND GROUNDING FOR ELECTROMAGNETIC COMPATIBILITY AND SAFETY
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
ARINC 667 : 2002 SUPP 2	GUIDANCE FOR THE MANAGEMENT OF FIELD LOADABLE SOFTWARE
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
(INACTIVE RECORD)IEEE 1228 : 1994	IEEE Standard for Software Safety Plans.
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
EIA 649 : 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

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MIL HDBK 516 : C

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