|
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 |