Source: https://infostore.saiglobal.com/en-us/Standards/MIL-HDBK-516-C-705318_SAIG_MIL_MIL_1630051/
Timestamp: 2020-02-26 23:07:06
Document Index: 522840971

Matched Legal Cases: ['ART 6', 'ART 1', 'ART 23', 'ART 5', 'ART 1', 'ART 8', 'ART 2', 'ART 23', 'ART 4', 'ART 3', 'ART 7']

MIL HDBK 516 : C | AIRWORTHINESS CERTIFICATION CRITERIA | SAI Global
MIL HDBK 516 : C
AIRWORTHINESS CERTIFICATION CRITERIA
6. FLIGHT TECHNOLOGY
7. PROPULSION AND PROPULSION INSTALLATIONS
8. AIR VEHICLE SUBSYSTEMS
9. CREW SYSTEMS
10. DIAGNOSTICS SYSTEMS
13. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E[3])
15. COMPUTER SYSTEMS AND SOFTWARE
17. ARMAMENTS AND STORES INTEGRATION
18. PASSENGER SAFETY
20. AIR TRANSPORTABILITY, AIRDROP, MISSION/TEST
EQUIPMENT AND CARGO/PAYLOAD SAFETY
APPENDIX A - AIRWORTHINESS CERTIFICATION CRITERIA
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
MIL HDBK 525 : 0 ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM
MIL STD 1798 : C MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
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
MIL STD 961 : E DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
MIL STD 1568 : D MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
ASTM D 2247 : 2015 : REDLINE Standard Practice for Testing Water Resistance of Coatings in 100 % Relative Humidity
MIL STD 38784 : A GENERAL STYLE AND FORMAT REQUIREMENTS FOR TECHNICAL MANUALS
ASTM F 2156 : 2017 : REDLINE Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope
NASA STD 7009 : 2016 STANDARD FOR MODELS AND SIMULATIONS
FAA AC 25.963-1 : 0 FUEL TANK ACCESS COVERS
FAA AC 25.994-1 : 0 DESIGN CONSIDERATIONS TO PROTECT FUEL SYSTEMS DURING A WHEELS-UP LANDING
MIL STD 1399/390 : 0 INTERFACE STANDARD FOR SHIPBOARD SYSTEMS - ELECTRIC POWER, DIRECT CURRENT, (OTHER THAN SHIP'S BATTERY) FOR SUBMARINES (METRIC)
RTCA DO 255 : 2000 REQUIREMENTS SPECIFICATION FOR AVIONICS COMPUTER RESOURCE (ACR)
SAE AS 1831 : 1997 ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
RTCA DO 297 : 2005
JSSG 2010 10 : 0 CREW SYSTEMS OXYGEN SYSTEMS HANDBOOK
ASTM F 330 : 2016 : REDLINE Standard Test Method for Bird Impact Testing of Aerospace Transparent Enclosures
MIL STD 27733 : 0 MODIFICATION AND MARKING REQUIREMENTS FOR TEST EQUIPMENT IN AEROSPACE VEHICLES AND RELATED SUPPORT EQUIPMENT
MIL PRF 27260 : D TIE DOWN, CARGO, AIRCRAFT CGU-1/B
FAA AC 33-5 : 0 TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 25.869-1 : 2007 FIRE PROTECTION: SYSTEMS
FAA AC 33.76-1 : 2009 BIRD INGESTION CERTIFICATION STANDARDS
MIL HDBK 1599 : A BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
SAE AS 5726 : 2013 INTERFACE STANDARD, INTERFACE FOR MICRO MUNITIONS
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)
ASTM F 735 : 2017 : REDLINE Standard Test Method for Abrasion Resistance of Transparent Plastics and Coatings Using the Oscillating Sand Method
MIL STD 1796 : A AVIONICS INTEGRITY PROGRAM (AVIP)
STANAG 4101 : 0 TOWING ATTACHMENTS
MIL E 22285 : 0 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
FAA AC 20-145 : 2003 GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS
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 8091 : 2014 AIRCRAFT JACKING PADS ADAPTERS AND SOCKETS DESIGN AND INSTALLATION OF
STANAG 3899 : 0 GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES
MIL STD 1425 : A SAFETY DESIGN REQUIREMENTS FOR MILITARY LASERS AND ASSOCIATED SUPPORT EQUIPMENT
FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
MIL HDBK 419 : A GROUNDING, BONDING, AND SHIELDING FOR ELECTRONIC EQUIPMENTS AND FACILITIES - VOLUME 1: BASIC THEORY & VOLUME 2: APPLICATIONS
MIL T 81259 : B TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
STANAG 3098 : 2014 AIRCRAFT JACKING
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
STANAG 3447 : 2016 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
FAA AC 33.4-2 : 0 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY
MIL STD 1683 : B CONNECTORS AND JACKETED CABLE, ELECTRIC, SELECTION STANDARD FOR SHIPBOARD USE
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)
FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
FAA AC 33-3 : 0 TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
ASTM G 85 : 2011 : REDLINE Standard Practice for Modified Salt Spray (Fog) Testing
SAE AS 1426 : 1980 STANDARD GALLEY SYSTEM SPECIFICATION, PART 1, PERFORMANCE, DESIGN DEVELOPMENT
MIL STD 188/181 : C CHANGE 3 INTEROPERABILITY STANDARD FOR ACCESS TO 5-KHZ AND 25-KHZ UHF SATELLITE COMMUNICATIONS CHANNELS
FAA AC 20-128 : 0 DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
MIL STD 8591 : 0 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE)
SAE AS 8049 : 2015 PERFORMANCE STANDARD FOR SEATS IN CIVIL ROTORCRAFT, TRANSPORT AIRCRAFT, AND GENERAL AVIATION AIRCRAFT
MIL PRF 5041 : K TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT
MIL PRF 7032 : H INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR
FAA AC 33-4 : 0 DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES
MIL PRF 63029 : J MANUALS, TECHNICAL: REQUIREMENTS FOR OPERATOR'S MANUALS AND CHECKLISTS FOR MANNED AND UNMANNED AIRCRAFT SYSTEMS
FAA AC 25.981-1 : 2008 FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
STANAG 7191 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
MIL PRF 5920 : F MANUALS, TECHNICAL - SAMPLE BASIC WEIGHT CHECKLISTS AND LOADING DATA
FAA AC 120-42 : 2008 EXTENDED OPERATIONS (ETOPS AND POLAR OPERATIONS)
SAE ARP 5583 : 2010 GUIDE TO CERTIFICATION OF AIRCRAFT IN A HIGH-INTENSITY RADIATED FIELD (HIRF) ENVIRONMENT
RTCA DO 333 : 2011 FORMAL METHODS SUPPLEMENT TO DO-178C AND DO-278A
MIL DTL 85025 : B NATOPS PROGRAM TECHNICAL PUBLICATIONS AND PRODUCTS - STYLE, FORMAT, AND COMMON TECHNICAL CONTENT
MIL HDBK 61 : A CONFIGURATION MANAGEMENT GUIDANCE
FAA AC 33-1 : 0 TURBINE ENGINE FOREIGN OBJECT INGESTION AND ROTOR BLADE CONTAINMENT TYPE CERTIFICATION PROCEDURES
SAE ARP 5089 : 1996 COMPOSITE REPAIR NDT/NDI HANDBOOK
FAA AC 91-85 : 2016 AUTHORIZATION OF AIRCRAFT AND OPERATORS FOR FLIGHT IN REDUCED VERTICAL SEPARATION MINIMUM (RVSM) AIRSPACE
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)
ATP 56 : B AIR TO AIR REFUELLING
SAE AS 8584 : 2013 BRAKE SYSTEMS, WHEEL, MILITARY AIRCRAFT
ASTM D 2803 : 2009 GUIDE FOR TESTING FILIFORM CORROSION RESISTANCE OF ORGANIC COATINGS ON METAL
MIL HDBK 299 : 0 CABLE COMPARISON HANDBOOK DATA PERTAINING TO ELECTRIC SHIPBOARD CABLE
FAA AC 20-30 : 0 AIRCRAFT POSITION LIGHT AND ANTICOLLISION LIGHT INSTALLATIONS
RTCA DO 212 : 1992 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE AUTOMATIC DEPENDENT SURVEILLANCE (ADS) EQUIPMENT
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)
SAE AIR 5826 : 2017 DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
SAE AIR 4845 : 1993 THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT
JSSG 2007 : 0 JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE
MIL STD 1530 : D AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
STANAG 3971 : 2013 AIR-TO-AIR REFUELLING - ATP-56
FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
JSSG 2010 13 : 1998 CREW SYSTEMS SURVIVAL, SEARCH, AND RESCUE (SSAR) HANDBOOK
SAE ARP 1538 : 2013 ARRESTING HOOK INSTALLATION, LAND-BASED AIRCRAFT
FAA AC 43.13-1 : 0 ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
MIL STD 1290 : A LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE
FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
MIL DTL 25959 : H TIE DOWN, TENSIONERS, CARGO, AIRCRAFT
RTCA DO 332 : 2011 OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A
MIL STD 188/242 : 0 INTEROPERABILITY AND PERFORMANCE STANDARDS FOR TACTICAL SINGLE CHANNEL VERY HIGH FREQUENCY (VHF) RADIO EQUIPMENT
FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
RTCA DO 200B : 2015 STANDARDS FOR PROCESSING AERONAUTICAL DATA
SAE ARP 1420 : 2002 GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
MIL HDBK 1763 : 0 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
STANAG 3278 : 2014 AIRCRAFT TOWING ATTACHMENTS AND DEVICES
SAE ARP 1834 : 1997 FAULT/FAILURE ANALYSIS FOR DIGITAL SYSTEMS AND EQUIPMENT
MIL STD 331 : D FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR
NASA STD 8719.13 : 2013 SOFTWARE SAFETY STANDARD
FAA AC 20-29 : 0 USE OF AIRCRAFT FUEL ANTI-ICING ADDITIVES
SAE ARP 1493 : 2013 WHEEL AND BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT
FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
SAE ARP 1870 : 2012 AEROSPACE SYSTEMS ELECTRICAL BONDING AND GROUNDING FOR ELECTROMAGNETIC COMPATIBILITY AND SAFETY
STANAG 3230 : 2007 EMERGENCY MARKINGS ON AIRCRAFT
ATP 3.3.4.2 : 2013 AIR TO AIR REFUELLING
AOP 52 : 2016 GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS
EIA SEB6 : A1990 SYSTEM SAFETY ENGINEERING IN SOFTWARE DEVELOPMENT
RTCA DO 186 : B2005 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE RADIO COMMUNICATIONS EQUIPMENT
SAE AS 1055 : 2013 FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS
FAA AC 20-42 : 2011 HAND FIRE EXTINGUISHERS FOR USE IN AIRCRAFT
STANAG 4671 : 2017 UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS (USAR)
MIL HDBK 1760 : A AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
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)
MIL HDBK 221 : 0 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
ARINC 667 : 2002 SUPP 2 GUIDANCE FOR THE MANAGEMENT OF FIELD LOADABLE SOFTWARE
ASTM F 733 : 2009 PRACTICE FOR OPTICAL DISTORTION AND DEVIATION OF TRANSPARENT PARTS USING THE DOUBLE-EXPOSURE METHOD
FAA AC 20-170 : 2010 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
SAE AIR 1419 : 2013 INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES
RTCA DO 236 : C2013 CHG 1 2014 MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION
ARINC 653 : 1997 SUPP 1 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE
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)
JSSG 2010/9 : 1998 CREW SYSTEMS PERSONAL PROTECTION EQUIPMENT HANDBOOK
ARINC 609 : 1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS
RTCA DO 330 : 2011 SOFTWARE TOOL QUALIFICATION CONSIDERATIONS
FAA AC 20-148 : 2004 REUSABLE SOFTWARE COMPONENTS
FAA AC 25-9 : 0 SMOKE DETECTION, PENETRATION AND EVACUATION TESTS AND RELATED FLIGHT MANUAL EMERGENCY PROCEDURES
FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
FAA AC 25-17 : 2009 TRANSPORT AIRPLANE CABIN INTERIORS CRASHWORTHINESS HANDBOOK
MIL STD 188 243 : A TACTICAL SINGLE CHANNEL ULTRA HIGH FREQUENCY (UHF) RADIO COMMUNICATIONS
SAE AMS 3694 : 2012 AERODYNAMIC SMOOTHING COMPOUND, FLEXIBLE, -55 DEGREES TO +130 DEGREES C (-65 DEGREES TO +270 DEGREES F)
FAA AC 20-119 : 1983 FUEL DRAIN VALVES
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 L 8552 : C LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
RTCA DO 278 : A2011 SOFTWARE INTEGRITY ASSURANCE CONSIDERATIONS FOR COMMUNICATION, NAVIGATION, SURVEILLANCE AND AIR TRAFFIC MANAGEMENT (CNS/ATM) SYSTEMS
MIL T 6053 : C TEST, IMPACT, SHOCK ABSORBER, LANDING GEAR, AIRCRAFT
MIL HDBK 2165 : 0 TESTABILITY PROGRAM FOR SYSTEMS AND EQUIPMENTS
MIL STD 1399/300 : B ELECTRIC POWER, ALTERNATING CURRENT
RTCA DO 219 : 1993 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR ATC TWO-WAY DATA LINK COMMUNICATIONS
JSSG 2010 14 : 1998 CREW SYSTEMS AIRCRAFT WINDSHIELD/CANOPY SYSTEMS AND TRANSPARENT ENCLOSURES HANDBOOK
MIL PRF 21480 : B GENERATOR SYSTEM, ELECTRIC POWER, 400 HERTZ, ALTERNATING CURRENT, AIRCRAFT - GENERAL SPECIFICATION FOR
MIL HDBK 1587 : 0 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
RTCA DO 331 : 2011 MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A
MIL PRF 8565 : K BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL HDBK 2066 : 0 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
MIL W 5088 : L WIRING, AEROSPACE VEHICLE
FAA AC 25.853-1 : 0
MIL HDBK 828 : C RANGE LASER SAFETY
MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
MIL B 8584 : C BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
MIL L 85314 : A LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR
MIL STD 3022 : 0 DOCUMENTATION OF VERIFICATION, VALIDATION, AND ACCREDITATION (VV&A) FOR MODELS AND SIMULATIONS
ATP 3.3.4.5 : 2013 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS
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)
FAA AC 120-40 : 0 AIRPLANE SIMULATOR QUALIFICATION
MIL STD 1474 : E NOISE LIMITS
MIL A 8865 : B AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
MIL STD 464 : C ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
MIL STD 188/182 : B CHANGE 3 INTEROPERABILITY STANDARD FOR UHF SATCOM DAMA ORDERWIRE MESSAGES AND PROTOCOLS
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
JSSG 2010 3 : 1998 CREW SYSTEMS COCKPIT/CREW STATIONS/CABIN HANDBOOK
FAA AC 25.981-2 : 2008 FUEL TANK FLAMMABILITY REDUCTION MEANS
MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
FAA AC 120-63 : 0 HELICOPTER SIMULATOR QUALIFICATION
MIL STD 3024 : 0 PROPULSION SYSTEM INTEGRITY PROGRAM (PSIP)
JSSG 2000 : B AIR SYSTEM
MIL STD 805 : B TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
MIL PRF 29595 : A BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL PRF 81757 : D BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT - GENERAL SPECIFICATION FOR
MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
FAA AC 20-60 : 1968 ACCESSIBILITY TO EXCESS EMERGENCY EXITS
MIL DTL 7700 : H FLIGHT MANUAL, PERFORMANCE DATA APPENDIX, MISSION CREW MANUAL, SUPPLEMENTAL MANUAL, AND ABBREVIATED FLIGHT CREW CHECKLIST
MIL F 17874 : B FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
ASTM F 2316 : 2012 SPECIFICATION FOR AIRFRAME EMERGENCY PARACHUTES
RTCA DO 181 : E2011 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIR TRAFFIC CONTROL RADAR BEACON SYSTEM/MODE SELECT (ATCRBS/MODE S) AIRBORNE EQUIPMENT
RTCA DO 185 : B2008 CHG NOT 2 13 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 2 (TCAS 2)
RTCA DO 189 : 1985 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE DISTANCE MEASURING EQUIPMENT (DME) OPERATING WITHIN THE RADIO FREQUENCY RANGE OF 960-1215 MHZ
FAA AC 20-41 : A SUBSTITUTE TECHNICAL STANDARD ORDER (TSO) AIRCRAFT EQUIPMENT
FAA AC 25-16 : 0 ELECTRICAL FAULT AND FIRE PREVENTION AND PROTECTION
AFGS 87256 : (1) INTEGRATED DIAGNOSTICS
SAE AS 4273 : 2007 FIRE TESTING OF FLUID HANDLING COMPONENTS FOR AIRCRAFT ENGINES AND AIRCRAFT ENGINE INSTALLATIONS
MIL PRF 7115/4 : A CONVERTER, AIRCRAFT 300 AMPERE, TYPE 2, CLASS A, FAN COOLED
FAA AC 20-131 : 0 AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2) AND MODE S TRANSPONDERS
FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
JSSG 2010 1 : 1998 CREW SYSTEMS ENGINEERING HANDBOOK
MIL STD 1289 : D AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS
JSSG 2010 11 : 1998 CREW SYSTEMS EMERGENCY EGRESS HANDBOOK
MIL STD 1310 : H SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY
SAE ARP 8615 : 2011 FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
JSSG 2010 6 : 1998 CREW SYSTEMS SUBTENANCE AND WASTE MANAGEMENT HANDBOOK
SAE AS 8049/1 : 2016 PERFORMANCE STANDARDS FOR SIDE-FACING SEATS IN CIVIL ROTORCRAFT, TRANSPORT AIRCRAFT, AND GENERAL AVIATION AIRCRAFT
SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
MIL E 7016 : F ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
JSSG 2010 2 : 1998 CREW SYSTEMS CREW STATION AUTOMATION, INFORMATION AND CONTROL DISPLAY MANAGEMENT HANDBOOK
SAE ARP 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS