MIL F 5504 : B
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC MICRONIC TYPE |
MIL STD 850 : B
|
AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT |
DEFSTAN 47-25/1(1982) : 1982
|
PIPELINES AND PIPE COUPLINGS FOR AIRCRAFT FLUID SYSTEMS (METRIC) |
SAE AS 50571 B : 2016
|
LIGHTS, INSTRUMENT, INDIVIDUAL, GENERAL SPECIFICATION FOR |
MIL T 5522 : D
|
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS |
BS EN 10202:2001
|
Cold reduced tinmill products. Electrolytic tinplate and electrolytic chromium/chromium oxide coated steel |
SAE AMS I 7171 : 2011
|
INSULATION BLANKET, THERMAL ACOUSTICAL |
BS 6221-20:1984
|
PRINTED WIRING BOARDS - GUIDE FOR THE ASSEMBLY OF PRINTED WIRING BOARDS |
MIL A 8865 : B
|
AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
ASTM D 3701 : 2017 : REDLINE
|
Standard Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nuclear Magnetic Resonance Spectrometry |
BS 7867:1997
|
SPECIFICATION FOR PORTABLE FIRE EXTINGUISHERS FOR USE IN AIRCRAFT |
DEFSTAN 00-44/1(2007) : 2007
|
RELIABILITY AND MAINTAINABILITY DATA COLLECTION AND CLASSIFICATION |
MIL PRF 83870 : C
|
FILTER ELEMENT, DISPOSABLE, 20 MICRON ABSOLUTE, CONSTANT SPEED DRIVE, AIRCRAFT |
MIL HDBK 5 : G_VOL2
|
METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
STANAG 3370 : 2004
|
AIRCREW STATION ALERTING SYSTEMS |
MIL HDBK 17-5 : 0
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 5: CERAMIC MATRIX COMPOSITES |
DEFSTAN 17-3/1(1972) : 1972
|
ADAPTORS, AIRCRAFT JACKING POINTS (DETACHABLE JACKING PADS) |
STANAG 3456 : 0
|
AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
MIL STD 13231 : 0
|
MARKING OF ELECTRONIC ITEMS |
MIL I 6115 : A
|
INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF |
BS EN ISO 9809-3:2010
|
GAS CYLINDERS - REFILLABLE SEAMLESS STEEL GAS CYLINDERS - DESIGN, CONSTRUCTION AND TESTING - PART 3: NORMALIZED STEEL CYLINDERS (ISO 9809-3:2010) |
DEFSTAN 00-49/2(2008) : 2008
|
MOD GUIDE TO R&M TERMINOLOGY USED IN REQUIREMENTS |
ASTM B 80 : 2015 : REDLINE
|
Standard Specification for Magnesium-Alloy Sand Castings |
DEFSTAN 08-11/1(2000) : 2000
|
NBC PROTECTION FOR AIR PLATFORMS |
MIL T 8679 : 0
|
TEST REQUIREMENTS, GROUND HELICOPTER |
DEFSTAN 03-11/5(2008) : 2008
|
PHOSPHATE TREATMENT OF IRON AND STEEL |
DEFSTAN 05-37/2(1989) : 1989
|
THE POLICY FOR THE PROCUREMENT OF ELECTRONIC COMPONENTS |
STANAG 3303 : 86 AMD 5
|
CONNECTORS FOR 115/200 VOLTS, 400 HERTZ, 3 PHASE, AC SERVICING POWER |
MIL HDBK 505 : 0
|
DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
STANAG 3217 : 2006
|
OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
SAE AMS A 21180 : 2011
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
STANAG 4671 : 2017
|
UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS (USAR) |
STANAG 3558 : 2002
|
LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES |
STANAG 3341 : 72 AMD 6
|
EMERGENCY CONTROL COLOUR SCHEMES |
MIL HDBK 965 : 0
|
ACQUISITION PRACTICES FOR PARTS MANAGEMENT |
BS 2087-1:1992
|
PRESERVATIVE TEXTILE TREATMENTS - SPECIFICATION FOR TREATMENTS |
MIL A 25175 : C
|
AIR TRANSPORT, NONTACTICAL, PACKING FOR |
MIL-STD-1365 Revision C:2010
|
GENERAL DESIGN CRITERIA FOR HANDLING EQUIPMENT ASSOCIATED WITH WEAPONS AND RELATED ITEMS |
MIL STD 280 : A
|
DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
MIL HDBK 729 : 0
|
CORROSION & CORROSION PREVENTION METALS |
MIL-I-8500 Revision D:1980
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
BS 4921:1988
|
SPECIFICATION FOR SHERARDIZED COATINGS ON IRON OR STEEL |
DEFSTAN 17-1/2(1984) : 1984
|
AIRCRAFT LIFTING SLINGS, APERTURE OF TERMINAL RING OR LINK |
MIL STD 1530 : D
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
STANAG 3368 : 2014
|
INTERNAL AIRCRAFT ENGINE STARTING SYSTEM |
SAE AS 8090 : 2016
|
MOBILITY, TOWED AEROSPACE GROUND EQUIPMENT, GENERAL REQUIREMENTS FOR |
DEFSTAN 00-16/1(1984) : 1984
|
GUIDE TO THE ACHIEVEMENT OF QUALITY IN SOFTWARE |
STANAG 3605 : 0
|
COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
MIL STD 129 : R
|
MILITARY MARKING FOR SHIPMENT AND STORAGE |
DEFSTAN 03-5/3(1995) : 1995
|
AUTOCATALYTIC (ELECTROLESS) NICKEL COATING OF METALS |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL A 46146 : B
|
ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
DEFSTAN 05-124/1(1992) : 1992
|
PROCEDURES FOR THE PROCUREMENT OF AIRCRAFT ENGINES AND THEIR ACCESSORIES |
MIL HDBK 273 : 0
|
SURVIVABILITY ENHANCEMENT, AIRCRAFT NUCLEAR WEAPON THREAT, DESIGN AND EVALUATION GUIDELINES |
DEFSTAN 00-13/3(1994) : 1994
|
REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT |
DEFSTAN 61-17/4(2001) : 2001
|
THE SELECTION AND INTRODUCTION OF BATTERIES FOR SERVICE USE |
SAE ARP 1179 : 2011
|
AIRCRAFT GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT |
DEFSTAN 47-19/1(1977) : 1977 AMD 2
|
AIRCRAFT PIPE FITTINGS (INCH SERIES) - SCREW THREADS, HEXAGON SIZES, TAPPED HOLES, AND 'O' RING SEALS |
BS X 31:1967
|
SPECIFICATION FOR LOW TEMPERATURE STOVING SCHEME FOR AERONAUTICAL PURPOSES |
MIL-C-16310 Revision D:1991
|
CYLINDER, COMPRESSED GAS (COMPRESSED AIR AND CARBON DIOXIDE, NONSHATTERABLE AND NONMAGNETIC) |
MIL F 8785 : C
|
FLYING QUALITIES OF PILOTED AIRPLANES |
MIL F 25381 : A
|
FLIGHT TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR |
DEFSTAN 16-26/1(1983) : 1983
|
CHARGING VALVES FOR AIRCRAFT HIGH PRESSURE NITROGEN AND HYDRAULIC FLUID SYSTEMS |
RTCA DO 178 : C2011
|
SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
BS G 175:1959
|
Aircraft fuel nozzle grounding plugs and sockets |
MIL HDBK 173 : A
|
AUDIO EQUIPMENT |
DEFSTAN 81-124/3(2007) : 2007
|
EXPANDED POLYETHYLENE SHEET AND MOULDINGS, TYPE QX |
DEFSTAN 47-23/1(1980) : 1980
|
BEAD PROFILE FOR AIRCRAFT PIPING AND DUCTING (FLEXIBLE CONNECTIONS) |
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MIL STD 970 : 0
|
STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
STANAG 3153 : 0
|
AIRCRAFT NAVIGATION AND ANTI-COLLISION LIGHTS |
MIL STD 130 : N
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
MIL HDBK 241 : B
|
DESIGN GUIDE FOR EMI REDUCTION IN POWER SUPPLIES |
DEFSTAN 03-36/2(2010) : 2010
|
GUIDANCE TO THE USE OF CADMIUM ALTERNATIVES IN THE PROTECTIVE COATING OF DEFENCE EQUIPMENT |
MIL H 8890 : 0
|
HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
MIL STD 1555 : 0
|
AIRCREW STATION DISPLAYS AND ASSOCIATED EQUIPMENT, DEFINITIONS OF |
SAE AS 18607 : 1997
|
THERMAL ANTI-ICING EQUIPMENT, WING AND EMPENNAGE |
STANAG 3319 : 83 AMD 6
|
DIMENSIONS FOR CASES OF CONTROL BOXES, INSTRUMENTS AND PANEL MOUNTED EQUIPMENT |
STANAG 3659 : 2002
|
ELECTRICAL BONDING REQUIREMENTS FOR METALLIC AIRCRAFT SYSTEMS |
MIL P 87141 : A NOTICE 1
|
PARACHUTES REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL HDBK 1512 : 0
|
ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
MIL STD 101 : C
|
COLOR CODE FOR PIPELINES AND FOR COMPRESSED GAS CYLINDERS |
MIL A 8863 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
MIL T 5578 : C
|
TANK, FUEL, AIRCRAFT, SELF-SEALING |
MIL E 22285 : 0
|
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
MIL M 46062 : C
|
MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH |
MIL B 83054 : B
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
AECTP-400 : 2006
|
MECHANICAL ENVIRONMENTAL TESTS |
SAE J 1966 : 2011
|
LUBRICATING OILS, AIRCRAFT PISTON ENGINE (NON-DISPERSANT MINERAL OIL) |
MIL E 87219 : 0
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
MIL STD 1186 : A
|
CUSHIONING, ANCHORING, BRACING, BLOCKING, AND WATERPROOFING, WITH APPROPRIATE TEST METHODS |
MIL I 18373 : B
|
INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
MIL-STD-1789 Revision A:1988
|
SOUND PRESSURE LEVELS IN AIRCRAFT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
BS 2X 34:1998
|
Specification for two component polyurethane finish for aerospace purposes |
MIL-S-22885-1 Revision J:2010
|
SWITCH, PUSH BUTTON, ILLUMINATED LENSES (SCREW-IN, T-1-3/4 MFB LAMP) |
DEFSTAN 13-8/4(1978) : 1978
|
DIMENSIONAL REQUIREMENTS FOR AIRBORNE STORES, ASSOCIATED SUSPENSION AND RELEASE SYSTEMS AND ELECTRICAL CONTROL CONNECTIONS |
MIL HDBK 1763 : 0
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
MIL C 5604 : B
|
COMPASS, MAGNETIC, PILOTS STANDBY |
MIL STD 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
MIL P 46111 : C
|
PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
MIL P 8686 : 0
|
POWER UNITS, AIRCRAFT AUXILIARY, GAS-TURBINE TYPE GENERAL SPECIFICATION FOR [ASG] |
MIL-L-6503 Revision H:1975
|
LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
MIL STD 2077 : B
|
TEST PROGRAM SETS GENERAL REQUIREMENTS FOR |
BS 2C 13:1988
|
SPECIFICATION FOR SIZES OF AIRCRAFT GRAVITY FILLING ORIFICES AND ASSOCIATED REPLENISHMENT NOZZLES (METRIC SERIES) |
AFGS 87219 : B
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT |
MIL W 5044 : C
|
WALKWAY COMPOUND, NONSLIP AND WALKWAY MATTING, NONSLIP |
DEFSTAN 03-14/4(2008) : 2008
|
ELECTRODEPOSITION OF CHROMIUM FOR ENGINEERING PURPOSES |
MIL A 83377 : B
|
ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
MIL D 23222 : A
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
MIL PRF 83860 : D
|
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE |
MIL I 7032 : G
|
INVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
BS 5M 23:1987
|
SPECIFICATION FOR AN IDENTIFICATION SCHEME FOR PIPELINES |
DEFSTAN 05-18/5(2007) : 2007
|
SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS |
DEFSTAN 00-26/2(1988) : 1988
|
GUIDE TO THE EVALUATION AND EXPRESSION OF THE UNCERTAINTIES ASSOCIATED WITH THE RESULTS OF ELECTRICAL MEASUREMENTS |
MIL HDBK 46855 : A
|
HUMAN ENGINEERING PROGRAM - PROCESS AND PROCEDURES |
STANAG 2402 : 0
|
DANGER AREAS FOR LAND LAUNCHED UNMANNED AERIAL VEHICLES FOR USE BY NATO FORCES OPERATING IN A GROUND ENVIRONMENT ON MILITARY RANGES |
STANAG 3104 : 2015
|
IDENTIFICATION OF AIRCRAFT AND MISSILE PIPELINES AND ELECTRICAL CONDUITS |
MIL-STD-878 Revision B:2006
|
METHOD OF DIMENSIONING AND DETERMINING CLEARANCE FOR AIRCRAFT TIRES AND RIMS |
SAE ARP 4418 : 2008
|
PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES |
ARMP-7 : 2008
|
NATO R&M TERMINOLOGY APPLICABLE TO ARMPS |
MIL C 7762 : A
|
COMPASS, INSTALLATION OF |
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
MIL L 23699 : E
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
MIL A 8591 : H
|
AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
DEFSTAN 61-5(PT1)/4(2006) : 2006
|
LOW VOLTAGE ELECTRICAL POWER SUPPLY SYSTEMS - PART 1: TERMINOLOGY AND DEFINITIONS |
MIL PRF 27210 : J
|
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
MIL C 25427 : A
|
COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
DEFSTAN 03-4/6(2011) : 2011
|
THE PRE-TREATMENT AND PROTECTION OF STEEL ITEMS OF SPECIFIED MAXIMUM TENSILE STRENGTH EXCEEDING 1450 MPA |
MIL O 27210 : F
|
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
DEFSTAN 05-19/1(1972) : 1972
|
LIMITS AND FITS FOR ENGINEERING |
SAE AS 6625 : 1997
|
SPRAY EQUIPMENT, AIRCRAFT WINDSHIELD, ANTI-ICING |
MIL T 81571 : 0
|
THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, GENERAL SPECIFICATION FOR |
STANAG 3315 : 1998
|
AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS |
DEFSTAN 59-97/3(1990) : AMD 1
|
HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL |
DEFSTAN 05-42/2(1982) : 1982
|
PARTICULATE CONTAMINATION CLASSES FOR FLUIDS IN HYDRAULIC SYSTEMS |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
DEFSTAN 53-9/1 : LATEST
|
BOLTS, MACHINE SCREWS, AND NUTS FOR AEROSPACE VEHICLES |
MIL I 7028 : 0
|
INSTRUMENT AND INSTRUMENT BOARDS, AIRCRAFT, INSTALLATION OF |
MIL M 3171 : C
|
MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION |
BS EN ISO 9809-1:2010
|
GAS CYLINDERS - REFILLABLE SEAMLESS STEEL GAS CYLINDERS - DESIGN, CONSTRUCTION AND TESTING - PART 1: QUENCHED AND TEMPERED STEEL CYLINDERS WITH TENSILE STRENGTH LESS THAN 1100 MPA |
MIL H 8891 : A
|
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
MIL HDBK 725 : 0
|
ADHESIVES - A GUIDE TO THEIR PROPERTIES AND USES AS DESCRIBED BY FEDERAL AND MILITARY SPECIFICATIONS |
MIL A 87229 : 0
|
AUXILIARY POWER SYSTEMS, AIRBORNE |
DEFSTAN 59-76/1(1981) : 1981
|
TRANSFORMERS AND INDUCTORS - GENERAL REQUIREMENTS FOR THE PROCUREMENT OF TRANSFORMERS AND INDUCTORS - CAPABILITY APPROVAL |
MIL E 85583 : A
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 17-10/2(1984) : 1984
|
TOWING ATTACHMENTS AND TOWING/STEERING EQUIPMENT FOR AIRCRAFT |
SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
MIL P 26292 : C
|
PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
MIL E 21981B:1986
|
ELECTRONICS EQUIPMENT, NOMENCLATURE, SERIAL NUMBERS AND IDENTIFICATION PLATES: REQUIREMENTS FOR |
DEFSTAN 00-3/4(2011) : 2011
|
DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
MIL T 81259 : B
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
MIL PRF 5425 : E
|
PLASTIC SHEET, ACRYLIC, HEAT RESISTANT |
MIL HDBK 244 : A
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
MIL P 46112 : B
|
PLASTIC SHEET & STRIP, POLYMIDE |
DEFSTAN 00-34/1(1986) : 1986 AMD 1 1990
|
STANDARD SYMBOLOGY FOR AUTOMATIC IDENTIFICATION MARKING - BAR CODE 39 |
DEFSTAN 03-10/2(1987) : 1987
|
ELECTRO-DEPOSITION OF NICKEL AND CHROMIUM |
MIL STD 1333 : B
|
AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
STANAG 3312 : 0
|
PROFILE DIMENSIONS OF FLANGES FOR V-BAND COUPLINGS FOR PIPING AND DUCTING |
MIL G 21480 : A
|
GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
BS 4F 68:2002
|
Controlled storage of vulcanized rubbers for use in aerospace applications |
NF EN 1803 : 2002
|
TRANSPORTABLE GAS CYLINDERS - PERIODIC INSPECTION AND TESTING OF WELDED CARBON STEEL GAS CYLINDERS |
MIL T 7743 : F
|
TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR |
BS 4N 100-5:1999
|
AIRCRAFT OXYGEN SYSTEMS AND EQUIPMENT - GUIDE TO FIRE AND EXPLOSION HAZARDS ASSOCIATED WITH OXYGEN |
MIL STD 8651 : 0
|
INSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT) |
MIL STD 2218 : 0
|
THERMAL DESIGN, ANALYSIS & TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT |
MIL A 5498 : D
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
MIL S 25073 : 0
|
|
MIL STD 273 : B NOTICE 2
|
GAGE - PLUG, THREAD SETTING, CLASS W, FOR GO GAGES UNIFIED STANDARD CLASSES 2A AND 3A AND AMERICAN NATIONAL STANDARD CLASS 3 EXTERNAL THREADS |
DEFSTAN 03-13/1(1977) : 1977
|
GUIDE FOR THE PREVENTION OF CORROSION OF METAL CAUSED BY VAPOUR FROM ORGANIC MATERIALS |
STANAG 3278 : 2014
|
AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
SAE AMS R 83283 : 2014
|
RUBBER SILICONE, HIGH STRENGTH, CABIN PRESSURE SEAL MATERIAL, DIAPHRAGM TYPE |
MIL F 87154 : 0
|
FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-DTL-83054 Revision C:2003
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
AFGS-87139 Revision B:2013
|
LANDING GEAR SYSTEMS |
MIL C 18244 : A
|
CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 01-5/17(2011) : 2011
|
FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
DEFSTAN 47-21/1(1979) : 1979
|
FLEXIBLE HOSE ASSEMBLIES FOR PITOT AND STATIC SYSTEMS IN AIRCRAFT (METRIC) |
DEFSTAN 49-2/2(1975) : 1975 AMD 3
|
LUBRICATING GUNS, HAND AND GUNS, FLUID, DIRECT DELIVERY |
BS EN 22063:1994
|
METALLIC AND OTHER INORGANIC COATINGS - THERMAL SPRAYING - ZINC, ALUMINIUM AND THEIR ALLOYS |
SAE AS 25050B : 2017
|
COLORS, AERONAUTICAL LIGHTS AND LIGHTING EQUIPMENT, GENERAL REQUIREMENTS FOR |
DEFSTAN 00-29/1(1982) : 1982
|
FUNGAL CONTAMINATION AFFECTING THE DESIGN OF MILITARY MATERIAL |
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
MIL M 18012 : B
|
MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
MIL B 8584 : C
|
BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
MIL STD 31000 : A
|
TECHNICAL DATA PACKAGES |
DEFSTAN 05-43/1(1977) : 1977
|
STANDARD PROCEDURES FOR TAKING SAMPLES OF HYDRAULIC FLUIDS FOR EVALUATION OF PARTICULATE CONTAMINATION |
DEFSTAN 05-17/2(191980) : 1980
|
ELECTROTECHNICAL TERMS AND GRAPHICAL SYMBOLS |
DEFSTAN 59-42(PT1)/1(1990) : 1990
|
HEAT SHRINK SOLDER SHEATHS - PART 1: REQUIREMENTS AND TEST METHODS FOR CAPABILITY APPROVAL |
DEFSTAN 05-34/2(1984) : 1984
|
MARKING OF SERVICE MATERIAL |
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
MIL G 25871 : B
|
GLASS, LAMINATED, AIRCRAFT GLAZING |
MIL I 18259 : 0
|
INSTALLATION OF WINDOW ANTI ICING, DEGREASING AND WASHING SYSTEMS (GENERAL SPECIFICATION FOR) |
MIL P 8045 : B
|
PLASTIC SELF-SEALING AND NON SELF-SEALING TANK BACKING MATERIAL |
ASTM D 6576 : 2013 : REDLINE
|
Standard Specification for Flexible Cellular Rubber Chemically Blown |
MIL L 6723 : C
|
LIGHT, AIRCRAFT, GENERAL SPECIFICATION FOR |
STANAG 3492 : 0
|
CLAMPS, MOUNTING (IMPERIAL AND METRIC) FOR AIRCRAFT INSTRUMENTS |
MIL P 85573 : 0
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
DEFSTAN 05-21/1(1973) : 1973
|
QUALITY CONTROL SYSTEM REQUIREMENTS FOR INDUSTRY |
MIL STD 2076 : 0
|
UNIT UNDER TEST COMPATIBILITY WITH AUTOMATIC TEST EQUIPMENT GENERAL REQUIREMENTS FOR |
DEFSTAN 03-24/5(2008) : 2008
|
CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
IEC TS 62239:2008
|
Process management for avionics - Preparation of an electronic components management plan |
DEFSTAN 05-56/1(1980) : 1980
|
GRAPHICAL SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
JSSG-2007 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
DEFSTAN 53-88/1(1979) : 1979
|
WASHERS, LOCK, KEY (TAB) AND SPRING TENSION (CRINKLE), INCH SERIES, FOR AEROSPACE APPLICATIONS |
DEFSTAN 15-2/1(1987) : 1987
|
FLEXIBLE TANKS FOR USE IN AIRCRAFT FUEL AND METHANOL/WATER SYSTEMS |
DEFSTAN 91-30/1(1977) : 1977
|
LUBRICATING OIL, COLLOIDAL GRAPHITE OX-320 O-218 |
MIL A 8869 : B
|
AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS |
MIL PRF 83861 : D
|
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE |
STANAG 3218 : 86 AMD 2
|
LOCATION, ACTUATION AND SHAPE OF ENGINE CONTROLS AND SWITCHES |
MIL C 38373 : B
|
CAP, FLUID TANK FILLER |
MIL M 8090 : F
|
MOBILITY, TOWED AEROSPACE GROUND EQUIPMENT, GENERAL REQUIREMENTS FOR |
MIL P 5238 : C
|
PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 16-10/3(1983) : 1983 AMD 1
|
LOW PRESSURE AIR STARTING OF AIRCRAFT ENGINES |
MIL-DTL-23227 Revision F:1997
|
TUBE AND PIPE, NICKEL-CHROMIUM-IRON ALLOY (UNS N06600) |
MIL-STD-1791 Revision C:2017
|
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
BS 7195(1989) : 1989
|
GUIDE FOR PREVENTION OF CORROSION OF METALS CAUSED BY VAPOURS FROM ORGANIC MATERIALS |
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 AS 8804 : 1997
|
DEICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
BS 7863:2009
|
RECOMMENDATIONS FOR COLOUR CODING TO INDICATE THE EXTINGUISHING MEDIA CONTAINED IN PORTABLE FIRE EXTINGUISHERS |
MIL C 25050 : A
|
COLORS, AERONAUTICAL LIGHTS AND LIGHTING EQUIPMENT, GENERAL REQUIREMENTS FOR |
DEFSTAN 03-3/5(2011) : 2011
|
PROTECTION OF ALUMINIUM ALLOYS BY SPRAYED METAL COATINGS |
MIL A 9067 : C
|
ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR |
MIL-E-6051 Revision D:1967
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
STANAG 3639 : 2004
|
AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
BS EN 1803:2002
|
TRANSPORTABLE GAS CYLINDERS - PERIODIC INSPECTION AND TESTING OF WELDED CARBON STEEL GAS CYLINDERS |
JSSG 2010 : 1998
|
CREW SYSTEMS |
DEFSTAN 59-56(PT1)/2(1995) : 1995 AMD 3 1996
|
PLUGS AND SOCKETS, ELECTRICAL - LIST OF ITEMS APPROVED TO BS CECC 75201.001 ISSUE 2 (FORMERLY PATTERN 602) - PART 1: STANDARD AND MAINTENANCE RANGES |
STANAG 3302 : 81 AMD 5
|
CONNECTORS FOR 28 VOLT "DC" SERVICING POWER |
MIL P 7788 : F
|
PANEL, INFORMATION INTEGRALLY ILLUMINATED |
MIL-M-25500 Revision B:1969
|
MOCKUP TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR |
STANAG 3220 : 74 AMD 6
|
LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS FOR FIXED WING AIRCRAFT |
STANAG 4324 : 2007
|
ELECTROMAGNETIC RADIATION HAZARD ASSESSMENT AND TESTING OF MUNITIONS AND ASSOCIATED SYSTEMS |
MIL D 8181 : B
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
MIL HDBK 2164 : A
|
ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
STANAG 4360 : 2012
|
SPECIFICATION FOR PAINT SYSTEMS, RESISTANT TO CHEMICAL AGENTS AND DECONTAMINANTS, FOR THE PROTECTION OF LAND MILITARY EQUIPMENT |
ASTM B 584 : 2014 : REDLINE
|
Standard Specification for Copper Alloy Sand Castings for General Applications |
DEFSTAN 81-26/1(1974) : 1974
|
CYLINDERS, COMPRESSED GAS FOR AIRCRAFT |
MIL STD 469 : B
|
INTERFACE STANDARD FOR RADAR ENGINEERING INTERFACE REQUIREMENTS, ELECTROMAGNETIC COMPATIBILITY |
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
DEFSTAN 91-2 : LATEST
|
PETROLEUM FUELS |
STANAG 3865 : 2009
|
PHYSIOLOGICAL REQUIREMENTS FOR AIRCRAFT MOLECULAR SIEVE OXYGEN CONCENTRATING SYSTEMS |
SAE AS 6144 : 2011
|
SOUND AND THERMAL INSULATION FOR AIRCRAFT - GENERAL SPECIFICATION FOR THE INSTALLATION OF |
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
DEFSTAN 05-2/2(1972) : AMD 2
|
CODIFICATION OF EQUIPMENT |
MIL STD 1760 : E
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL HDBK 723 : A
|
STEEL AND IRON WROUGHT PRODUCTS |
MIL S 5002 : D
|
SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
MIL T 85075 : A
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
MIL HDBK 2089 : 0
|
AIRCRAFT SURVIVABILITY TERMS |
MIL STD 1353 : C
|
ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
DEFSTAN 00-600/2(2011) : 2011
|
INTEGRATED LOGISTIC SUPPORT - REQUIREMENTS FOR MOD PROJECTS |
MIL HDBK 2173 : 0
|
RELIABILITY-CENTERED MAINTENANCE REQUIREMENTS FOR NAVAL AIRCRAFT, WEAPONS SYSTEMS & SUPPORT EQUIPMENT |
MIL G 5485 : D
|
GLASS; LAMINATED, FLAT, BULLET RESISTANT |
MIL HDBK 781 : A
|
RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
MIL-I-8672 Revision B:1969
|
INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
BS 2C 4:1973
|
SPECIFICATION FOR COUPLING DIMENSIONS FOR AERO-ENGINE REFRIGERANT PRESSURE REPLENISHMENT CONNECTIONS |
SAE AS 5440 : 2011
|
HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-S-27174 Revision B:1985
|
|
MIL A 19531 : B
|
AIRCRAFT, MAINTENANCE AND ENGINEERING INSPECTION REQUIREMENTS |
MIL HDBK 253 : 0
|
GUIDANCE FOR THE DESIGN AND TEST OF SYSTEMS PROTECTED AGAINST THE EFFECTS OF ELECTROMAGNETIC ENERGY |
MIL-STD-2175 Revision A:1993
|
CASTING, CLASSIFICATION AND INSPECTION OF |
DEFSTAN 25-8/2(1971) : 1971
|
CABLE ASSEMBLIES, INTERVEHICLE, ELECTRICAL FOR STARTING PURPOSES |
MIL A 8806 : A
|
ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-DTL-7905 Revision H:2003
|
CYLINDERS, STEEL, COMPRESSED GAS, NON-SHATTERABLE, SEAMLESS, 1800 PSI AND 2100 PSI |
SAE AS 8091 : 2014
|
AIRCRAFT JACKING PADS ADAPTERS AND SOCKETS DESIGN AND INSTALLATION OF |
MIL STD 2069 : 0
|
REQUIREMENTS FOR AIRCRAFT NONNUCLEAR SURVIVABILITY PROGRAM |
DEFSTAN 81-14/6(2004) : 2004
|
CASES, WOOD (BATTEN AND BOARD CONSTRUCTION) |
MIL-HDBK-275 Revision A:1976
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
MIL S 58095 : A
|
SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
MIL-STD-411 Revision F:1997
|
AIRCREW STATION ALERTING SYSTEMS |
STANAG 4236 : 2007
|
LIGHTNING ENVIRONMENT |
MIL STD 8591 : 0
|
AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
SAE ARP 1256 : 2011
|
PROCEDURE FOR THE CONTINUOUS SAMPLING AND MEASUREMENT OF GASEOUS EMISSIONS FROM AIRCRAFT TURBINE ENGINES |
BS 5852:2006
|
Methods of test for assessment of the ignitability of upholstered seating by smouldering and flaming ignition sources |
MIL DTL 6162 : C
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL P 6997 : B
|
PLASTIC, WORKING AND INSTALLATION OF TRANSPARENT SHEET, GENERAL SPECIFICATION FOR [ASG] |
MIL STD 470 : B
|
MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
MIL S 87238 : 0
|
SURVIVAL AND FLOTATION SYSTEM, AIRBORNE |
MIL L 8937 : D
|
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, [NATO CODE NUMBER S 1738] |
MIL E 25499 : C
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
NASM 25049 : REV 1
|
KNOBS, CONTROL, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
AECTP-500 : 2016
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
DEFSTAN 03-8/2(1992) : 1992
|
ELECTRO-DEPOSITION OF TIN |
MIL STD 2072 : 0
|
SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR |
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
MIL I 23659 : C
|
INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
MIL P 81655 : 0
|
PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
MIL STD 889 : C
|
DISSIMILAR METALS |
DEFSTAN 16-23/2(1982) : 1982
|
FLOOR FITTINGS FOR CARGO TRANSPORT AIRCRAFT APERTURES FOR TIE-DOWN POINTS |
MIL STD 417 : A
|
CLASSIFICATION SYSTEM AND TESTS FOR SOLID ELASTOMERIC MATERIALS |
DEFSTAN 53-94/1(1983) : 1983
|
PROTECTIVE CAPS AND PLUGS FOR AIRCRAFT PIPELINES |
STANAG 3400 : 2010
|
RESTRAINT OF CARGO IN FIXED WING AIRCRAFT |
MIL-STD-1788 Revision A:1985
|
AVIONICS INTERFACE DESIGN STANDARD |
BS G 212:1971
|
SPECIFICATION FOR GENERAL REQUIREMENTS FOR AIRCRAFT ELECTRICAL CABLES |
MIL-E-5627 Revision B:1965
|
EXTINGUISHERS, FIRE, CARBON DIOXIDE, PORTABLE |
MIL STD 1367 : A
|
PACKAGING, HANDLING, STORAGE, AND TRANSPORTABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
MIL-D-21625 Revision G:1993
|
DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
BS 5045-7:2000
|
Transportable gas containers Specification for seamless steel gas containers of water capacity 0.5 L up to 15 L for special portable applications |
MIL E 5400 : T
|
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
MIL E 24021 : J NOTICE 1
|
ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
MIL STD 1843 : 0
|
RELIABILITY-CENTERED MAINTENANCE FOR AIRCRAFT, ENGINES AND EQUIPMENT |
MIL STD 875 : A
|
TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT |
MIL STD 7080 : 0
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
SAE ARP 1533 : 2016
|
PROCEDURE FOR THE ANALYSIS AND EVALUATION OF GASEOUS EMISSIONS FROM AIRCRAFT ENGINES |
MIL HDBK 1791 : 0
|
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
DEFSTAN 53-32/2(1980) : 1980 CORR 1981
|
GUIDE TO THE METHODS OF LOCKING SCREWED FASTENERS |
SAE AS 1933 : 2013
|
AGE CONTROLS FOR HOSE CONTAINING AGE-SENSITIVE ELASTOMERIC MATERIAL |
STANAG 3800 : 2001
|
NIGHT VISION IMAGING SYSTEM (NVIS) INTERIOR LIGHTING COMPATIBILITY DESIGN CRITERIA |
MIL T 25959 : C NOTICE 1
|
TIE DOWN, CARGO, AIRCRAFT |
STANAG 3334 : 96 AMD 1
|
DEFUELLING OF AIRCRAFT |
MIL P 9400 : C
|
PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
STANAG 3216 : 84 AMD 4
|
LAYOUT OF FLIGHT DATA IN PILOTS DISPLAYS |
SAE ARP 492 : 2014
|
AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST |
SAE AMS A 25463 : 2013
|
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
MIL G 6162/1 : C
|
STARTER GENERATOR, 30 VOLT, DIRECT CURRENT 400 AMPERE, AIRCRAFT ENGINE DRIVEN |
MIL C 83413 : A
|
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
DEFSTAN 47-12/4(1987) : 1987
|
POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES (WIRE REINFORCED) FOR MEDIUM AND HIGH PRESSURE FLUID SYSTEMS IN AIRCRAFT |
MIL STD 1512 : 0
|
ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
MIL L 18276 : C
|
LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
MIL STD 2074 : 0
|
FAILURE CLASSIFICATION FOR RELIABILITY TESTING |
MIL-I-8671 Revision D:1994
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
STANAG 3323 : 0
|
PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC) |
MIL W 81752 : A
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
MIL-PRF-5480 Revision H:2015
|
DATA, ENGINEERING AND TECHNICAL: REPRODUCTION |
MIL A 25463 : B
|
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
DEFSTAN 15-3 : LATEST
|
TRANSPARENT GLAZING MATERIALS AND ACCESSORIES FOR AEROSPACE APPLICATIONS |
STANAG 3647 : 0
|
NOMENCLATURE IN AIRCREW STATIONS |
MIL STD 6866 : 0
|
INSPECTION, LIQUID PENETRANT |
MIL STD 453 : C
|
INSPECTION, RADIOGRAPHIC |
MIL F 7190 : B
|
FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL P 85034 : 0
|
POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
MIL STD 838 : C
|
LUBRICATION OF MILITARY EQUIPMENT |
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 |
MIL-HDBK-17-3 Revision F:2002
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 3: POLYMER MATRIX COMPOSITES MATERIALS USAGE, DESIGN, AND ANALYSIS |
SAE AMS P 83310 : 2016
|
PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
DEFSTAN 53-1/3(1981) : 1981 AMD 1 1984
|
USE OF UNIFIED SCREW THREADS |
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 05-28/1(1980) : 1980
|
NATO GUIDE TO THE PREPARATION OF SPECIFICATIONS FOR THE PROCUREMENT OF DEFENCE MATERIAL |
MIL-DTL-23659 Revision F:2010
|
INITIATORS, ELECTRIC, GENERAL DESIGN SPECIFICATION FOR |
DEFSTAN 00-41/3(1993) : 1993
|
RELIABILITY AND MAINTAINABILITY MOD GUIDE TO PRACTICES AND PROCEDURES |
DEFSTAN 00-31/1(1987) : 1987
|
THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
DEFSTAN 05-91/2(1995) : 1995
|
QUALITY SYSTEM REQUIREMENTS FOR DESIGN/DEVELOPMENT, PRODUCTION, INSTALLATION AND SERVICING |
A A 59124 : 0
|
DECK COVERING, LIGHTWEIGHT, NONSLIP |
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
STANAG 3230 : 2007
|
EMERGENCY MARKINGS ON AIRCRAFT |
MIL PRF 27260 : D
|
TIE DOWN, CARGO, AIRCRAFT CGU-1/B |
MIL STD 2154 : 0
|
INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS FOR |
SAE AS 85075 : 2000
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
BS 5599:1993
|
SPECIFICATION FOR HARD ANODIC OXIDATION COATINGS ON ALUMINIUM AND ITS ALLOYS FOR ENGINEERING PURPOSES |
MIL-I-7171 Revision D:1993
|
INSULATION BLANKET, THERMAL ACOUSTICAL |
SAE ARP 5316 : 2014
|
STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
AECTP-100 : 2016
|
ENVIRONMENTAL GUIDELINES FOR DEFENCE MATERIEL |
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
MIL T 6396 : E
|
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
MIL-STD-965 Revision B:1993
|
PARTS CONTROL PROGRAM |
DEFSTAN 66-27/1(1978) : 1978 AMD 1
|
PRESSURE CONNECTIONS ON AIRCRAFT INSTRUMENTS AND ASSOCIATED EQUIPMENT |
STANAG 7187 : 2015
|
ON BOARD OXYGEN GENERATING SYSTEMS (OBOGS) PERFORMANCE STANDARDS |
MIL HDBK 2124 : 0
|
FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
MIL A 81264 : 0
|
ASBESTOS FELT OR MAT, RESIN IMPREGNATED |
DEFSTAN 00-971/1(1987) : 1987
|
GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
MIL E 8593 : A
|
ENGINE, AIRCRAFT, TURBOPROP, GENERAL SPECIFICATION FOR [ASG] |
MIL L 5057 : F
|
LIGHT, INSTRUMENT, INDIVIDUAL, GENERAL SPECIFICATION FOR |
MIL I 6870 : E
|
INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
DEFSTAN 03-7/1(1973) : 1973
|
PAINTING OF METAL AND WOOD |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE AMS STD 2175 : 1998
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
MIL H 18325 : B
|
HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
STANAG 3611 : 73 AMD 4
|
CHARACTERISTICS OF COMPRESSED BREATHING AIR FOR AIRCRAFT USE |
MIL HDBK 722 : 0
|
GLASS |
STANAG 4235 : 0
|
ELECTROSTATIC ENVIRONMENTAL CONDITIONS AFFECTING THE DESIGN OF MATERIEL FOR USE BY NATO FORCES |
STANAG 3499 : 0
|
CHARACTERISTICS OF SUPPLY EQUIPMENT FOR LIQUID OXYGEN |
MIL HDBK 337 : 0
|
ADHESIVE BONDED AEROSPACE STRUCTURE REPAIR |
MIL I 8651 : C
|
IDENTIFICATION AND MODIFICATION [FOR AIRCRAFT] INSTALLATION OF |
MIL-PRF-8184 Revision F:1998
|
PLASTIC SHEET, ACRYLIC MODIFIED |
BS EN 1968:2002
|
TRANSPORTABLE GAS CYLINDERS - PERIODIC INSPECTION AND TESTING OF SEAMLESS STEEL GAS CYLINDERS |
MIL-HDBK-83377 : 1997
|
ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
SAE AS 18259 : 1997
|
INSTALLATION OF WINDOW ANTI-ICING, DE-GREASING AND WASHING SYSTEMS (GENERAL SPECIFICATION FOR) |
STANAG 3692 : 76 AMD 4
|
LOCATION AND ACTUATION OF THRUST VECTOR CONTROLS FOR VSTOL AIRCRAFT OTHER THAN ROTARY WING AIRCRAFT |
MIL-F-26301 Revision H:2014
|
FLASHER, SOLID STATE, AIRCRAFT NAVIGATIONAL LIGHT, GENERAL SPECIFICATION FOR |
SAE AS 7788 : 1999
|
PANELS, INFORMATION, INTEGRALLY ILLUMINATED |
MIL HDBK 1812 : 0
|
TYPE DESIGNATION, ASSIGNMENT AND METHOD FOR OBTAINING |
MIL F 17874 : B
|
FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF |
DEFSTAN 03-26/2(1988) : 1988
|
HARD ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
MIL T 5842 : B
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
MIL-PRF-28800 Revision F:1996
|
TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL PRF 5503 : G
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
BS 2569-2:1965
|
Specification for sprayed metal coatings Protection of iron and steel against corrosion and oxidation at elevated temperatures. |
STANAG 3593 : 1997
|
NUMBERING OF ENGINES AND THEIR ASSOCIATED CONTROLS AND DISPLAYS IN AIRCRAFT |
MIL-PRF-23699 Revision G:2014
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, AND O-167 |
MIL A 25730 : C
|
ANTENNA SUBSYSTEMS FOR AIRBORNE IDENTIFICATION AND NAVIGATION EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL STD 1757 : A
|
LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE |
MIL-L-27160 Revision C:1972
|
LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR |
MIL M 6857 : D
|
MAGNESIUM ALLOY CASTINGS, HEAT TREATMENT OF |
BS 5760-0:1986
|
RELIABILITY OF SYSTEMS, EQUIPMENT AND COMPONENTS - INTRODUCTORY GUIDE TO RELIABILITY |
ASTM D 4529 : 2017 : REDLINE
|
Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
MIL P 8184 : E
|
PLASTIC SHEET, ACRYLIC, MODIFIED |
MIL C 7115 : F
|
CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 16-21/2(1986) : 1986 AMD 1 1986
|
MARKING OF AIRCRAFT HYDRAULIC COMPONENTS |
MIL P 6992 : 0
|
PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER |
MIL L 8552 : C
|
LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
MIL STD 809 : B
|
ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
IPC 2221B:2012
|
GENERIC STANDARD ON PRINTED BOARD DESIGN |
MIL E 5007 : D
|
ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
MIL HDBK 17-4 : A
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 4: METAL MATRIX COMPOSITES |
DEFSTAN 05-10(PT0)/5(2006) : 2006
|
PRODUCT DEFINITION INFORMATION - PART 0: GENERAL INTRODUCTION TO PRODUCT DEFINITION INFORMATION |
STANAG 3224 : 2005
|
AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
MIL-STD-1812 Base Document:1997
|
TYPE DESIGNATION, ASSIGNMENT AND METHOD FOR OBTAINING |
MIL STD 680 : B NOTICE 1
|
CONTRACTOR STANDARDIZATION PROGRAM REQUIREMENTS |
MIL-DTL-6484 Revision D:2007
|
LIGHTS, COCKPIT UTILITY, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL C 7188 : 0
|
COMPASS, PILOTS STANDBY, INSTALLATION OF |
AFGS-87154 Revision A:1992
|
FUEL SYSTEMS, GENERAL DESIGN SPECIFICATION FOR |
MIL R 83283 : A
|
RUBBER, SILICONE, HIGH STRENGTH, CABIN PRESSURE SEAL MATERIAL, DIAPHRAGM TYPE |
MIL STD 2124 : A
|
FLIGHT INCIDENT RECORDER/CRASH POSITION LOCATOR, MINIMUM PERFORMANCE STANDARDS FOR |
BS 5X 17(1998) : 1998
|
SPECIFICATION FOR OLEORESINOUS VARNISH FOR AEROSPACE PURPOSES |
MIL STD 1290 : A
|
LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
MIL PRF 32070 : A
|
TEST PROGRAM SETS |
DEFSTAN 00-17/1(1985) : 1985
|
MODULAR APPROACH TO SOFTWARE CONSTRUCTION, OPERATION AND TEST - MASCOT |
DEFSTAN 17-2/3(1989) : 1989
|
REPLENISHMENT EQUIPMENT FOR AERO ENGINE THRUST AUGMENTATION (REFRIGERANT INJECTION) SYSTEMS |
STANAG 3221 : 77 AMD 7
|
AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) IN AIRCRAFT DESIGN STANDARDS AND LOCATION OF CONTROLS |
MIL L 81174 : A
|
LIGHT LANDING, AIRCRAFT RETRACTABLE |
MIL H 5364 : D
|
HARNESS, SHOULDER SAFETY, GENERAL SPECIFICATION FOR |
MIL S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
MIL STD 882 : E
|
STANDARD PRACTICE FOR SYSTEM SAFETY |
MIL C 8779 : E
|
COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
MIL H 5484 : C
|
HEATER, AIRCRAFT, COMBUSTION TYPE |
SAE AS 5778 : 1997
|
COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
MIL STD 872 : 0
|
TEST REQUIREMENTS AND PROCEDURES FOR AIRCRAFT EMERGENCY GROUND AND DITCH ESCAPE PROVISIONS |
STANAG 4327 : 0
|
LIGHTNING, MUNITION ASSESSMENT AND TEST PROCEDURES |
BS 3G 230:2000
|
Specification for general requirements for aircraft electrical cables (second series) |
MIL-F-83861-1 Revision A:1977
|
FILTER ELEMENT, FLUID PRESSURE, HYDRAULIC, AIRCRAFT, DISPOSABLE, 5 MICRON ABSOLUTE |
MIL-M-8609 Revision B:1965
|
MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 91-4/8(2008) : 2008
|
FUEL, NAVAL DISTILLATE, NATO CODE: F-76, JOINT SERVICE DESIGNATION: DIESO F-76 |
BS EN 1802:2002
|
TRANSPORTABLE GAS CYLINDERS - PERIODIC INSPECTION AND TESTING OF SEAMLESS ALUMINIUM ALLOY GAS CYLINDERS |
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 |
MIL I 83456 : 0
|
INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR |
STANAG 4145 : 1991
|
NUCLEAR SURVIVABILITY CRITERIA FOR ARMED FORCES MATERIEL AND INSTALLATIONS - AEP-4 |
SAE AS 7413 : 2001(S2019)
|
COUPLING ASSEMBLIES, QUICK DISCONNECT, AUTOMATIC SHUTOFF |
MIL HDBK 268 : 0
|
SURVIVABILITY ENHANCEMENT, AIRCRAFT CONVENTIONAL WEAPON THREATS, DESIGN & EVALUATION GUIDELINES |
MIL STD 783 : D
|
LEGENDS FOR USE IN AIRCREW STATIONS AND ON AIRBORNE EQUIPMENT |
STANAG 3747 : 2016
|
GUIDE SPECIFICATIONS (MINIMUM QUALITY STANDARDS) FOR AVIATION TURBINE FUELS (F-24, F-27, F-34, F-35, F-37, F-40 AND F-44) |
MIL A 8897 : A
|
ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS |
BS 2G199(1984) : 1984 AMD 4901
|
SCHEDULE FOR TABLES RELATING TO ALTITUDES, AIRSPEED AND MACH NUMBERS FOR USE IN AERONAUTICAL INSTRUMENT DESIGN AND CALIBRATION |
DEFSTAN 68-284/3(2009) : 2009
|
COMPRESSED BREATHING GASES FOR AIRCRAFT, DIVING AND MARINE LIFE-SUPPORT APPLICATIONS |
MIL R 8236 : F
|
REEL, SHOULDER HARNESS, INERTIA LOCK |
MIL STD 12 : D
|
ABBREVIATIONS FOR USE ON DRAWINGS, SPECIFICATIONS FOR STANDARDS AND IN TECHNICAL DOCUMENTS |
MIL-A-83376 Revision A:1978
|
ADHESIVE BONDED METAL FACED, SANDWICH STRUCTURES, ACCEPTANCE CRITERIA |
MIL-DTL-5578 Revision D:2008
|
TANKS, FUEL, AIRCRAFT, SELF-SEALING |
STANAG 7139 : 0
|
AIRCRAFT ENGINE CONTROLS, SWITCHES, DISPLAYS, INDICATORS, GAUGES AND ARRANGEMENTS |
DEFSTAN 95-7/2(2004) : 2004
|
WIRE FOR LOCKING PURPOSES AND WIRE LOCKING PRACTICE FOR AEROSPACE USE |
DEFSTAN 03-2/6(2011) : 2011
|
CLEANING AND PREPARATION OF METAL SURFACES |
MIL C 5778 : D
|
COVER, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
DEFSTAN 59-36/5(1995) : 1995
|
SELECTION OF ELECTRONIC AND ELECTRICAL COMPONENTS FOR USE IN DEFENCE EQUIPMENT |
BS 3C7(1989) : 1989
|
SPECIFICATION FOR AIRCRAFT TYRE VALVES: INTERCHANGEABILITY DIMENSIONS |
MIL-HDBK-87213 Revision A:2005
|
ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
MIL T 5041 : J
|
TIRE, PNEUMATIC, AIRCRAFT |
MIL-PRF-24021 Revision K:1998
|
ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
AECTP-200 : 2009
|
ENVIRONMENTAL CONDITIONS |
MIL F 25173 : A
|
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT |
DEFSTAN 61-10/4(1984) : 1984
|
GENERATOR SETS (GROUND, ENGINE DRIVEN) |
DEFSTAN 05-13/2(1991) : 1991
|
MARKS IDENTIFYING METRIC FEATURES OF EQUIPMENT AND PARTS |
MIL-DTL-6396 Revision F:2008
|
TANKS, FUEL, OIL, COOLING FLUIDS, INTERNAL, REMOVABLE NON-SELF-SEALING |
MIL S 38039 : B
|
SYSTEM, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
MIL D 81641 : 0
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
MIL HDBK 131 : A
|
IDENTIFICATION MARKINGS FOR FASTENERS |
STANAG 3317 : 71 AMD 8
|
AIRCRAFT ELECTRICAL CABLES |
DEFSTAN 03-25/5(2008) : 2008
|
SULFURIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
STANAG 3208 : 2009
|
AIR CONDITIONING CONNECTIONS |
SAE AMS G 25871 : 2016
|
GLASS, LAMINATED, AIRCRAFT GLAZING |
ISO 14001:2015
|
Environmental management systems — Requirements with guidance for use |
MIL C 8678 : 0
|
COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS |
MIL STD 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL STD 1523 : A
|
AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL |
BS 4C 14:1991
|
SPECIFICATION FOR AIRCRAFT PRESSURE REFUELLING CONNECTORS |
DEFSTAN 03-18/4(2008) : 2008
|
CHROMATE CONVERSION COATINGS (CHROMATE FILMING TREATMENTS) GRADES: STANDARD AND BRUSHING FOR ALUMINIUM AND ALUMINIUM ALLOYS |
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
STANAG 4155 : 0
|
NCB PROTECTIVE MASK AND FILTER CANNISTER SCREW THREADS |
ASTM E 2375 : 2016 : REDLINE
|
Standard Practice for Ultrasonic Testing of Wrought Products |
ASTM E 1444 : 2005
|
Standard Practice for Magnetic Particle Testing |
MIL A 8867 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
MIL STD 471 : A
|
MAINTAINABILITY DEMONSTRATION |
SAE AS 18276 : 2014
|
LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
MIL-D-8804 Revision B:1993
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL B 8565 : J
|
BATTERY AND CELL, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL T 6053 : C
|
TEST, IMPACT, SHOCK ABSORBER, LANDING GEAR, AIRCRAFT |
STANAG 3198 : 2017
|
FUNCTIONAL REQUIREMENTS OF AIRCRAFT OXYGEN EQUIPMENT AND PRESSURE SUITS |
MIL A 21180 : D
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
MIL PRF 5041 : K
|
TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT |
MIL STD 794 : E
|
PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
MIL A 8861 : B
|
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
SAE AS 5604 : 2012
|
COMPASS: MAGNETIC, PILOT'S STANDBY |
BS 4G 173-1:1985
|
CONNECTORS FOR GROUND ELECTRICAL SUPPLIES FOR AIRCRAFT - SPECIFICATION FOR DESIGN, PERFORMANCE AND TEST REQUIREMENTS |
DEFSTAN 16-24/1(1983) : 1983
|
SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
MIL STD 1288 : NOTICE 4
|
AIRCREW PROTECTION REQUIREMENTS NONNUCLEAR WEAPONS THREAT |
STANAG 3766 : 2017
|
GREASE NIPPLES |
MIL R 6130 : C
|
RUBBER, CELLULAR, CHEMICALLY BROWN |
MIL D 87213 : 0
|
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
DEFSTAN 61-11(PT1)/1(1969) : 1969
|
CABLES, CORDS AND WIRES, ELECTRICAL CABLES, RADIO FREQUENCY |
STANAG 3632 : 0
|
AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL STD 7179 : A
|
FINISHES, COATINGS, AND SEALANTS, FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEMS |
MIL-PRF-22885 Revision J:2016
|
SWITCHES, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR |
SAE AS 8775 : 1998
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
MIL STD 2089 : 0
|
AIRCRAFT NONNUCLEAR SURVIVABILITY TERMS |
MIL STD 250 : D
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT |
SAE AS 18012 : 1998
|
MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
STANAG 3447 : 2016
|
AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
MIL F 23447 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
DEFSTAN 59-31/2 : LATEST
|
LIGHTING PROTECTION |
DEFSTAN 53-20/1(1970) : 1970
|
RINGS, RETAINING (CIRCLIPS) |
SAE AS 35411 : 2010
|
FITTINGS, LUBRICATION |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
STANAG 4270 : 0
|
AVIATION FUEL DESIGN PARAMETER FOR FUTURE NATO LAND BASED TURBINE POWERED MILITARY AIRCRAFT |
MIL R 5520 : C
|
RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
MIL F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 16-6/2(1991) : 1991
|
CHARGING VALVE FOR AIRCRAFT LIQUID SPRING UNDERCARRIAGE UNITS |
MIL A 9094 : D
|
ARRESTER, LIGHTNING, GENERAL SPECIFICATION FOR |
MIL P 116 : J
|
PRESERVATION, METHODS OF |
STANAG 3296 : 0
|
AIRCRAFT GASEOUS OXYGEN REPLENISHMENT COUPLINGS |
MIL O 19838 : 0
|
OIL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF |
MIL STD 1472 : G
|
HUMAN ENGINEERING |
MIL PRF 25690 : B
|
PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
BS 2G 219:1983
|
SPECIFICATION FOR GENERAL REQUIREMENTS FOR GROUND SUPPORT ELECTRICAL SUPPLIES FOR AIRCRAFT |
MIL M 8650 : C
|
MOCKUP, AIRCRAFT CONSTRUCTION OF |
STANAG 7106 : 2015
|
CHARACTERISTICS OF GASEOUS BREATHING OXYGEN, LIQUID BREATHING OXYGEN AND SUPPLY PRESSURES, HOSES AND REPLENISHMENT COUPLINGS |
MIL-STD-322 Revision B:1984
|
EXPLOSIVE COMPONENTS, ELECTRICALLY INITIATED BASIC EVALUATION TESTS FOR |
MIL T 5091 : 0
|
TRANSMISSION, POWER, CONSTANT RATIO, GENERAL SPECIFICATION [AIRCRAFT USE] |
MIL STD 1366 : E
|
INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
STANAG 3824 : 77 AMD 5
|
GUIDANCE SPECIFICATION (MINIMUM QUALITY STANDARDS) FOR AVIATION GASOLINE (F-18) |
STANAG 3359 : 85 AMD 4
|
LOCATION AND ARRANGEMENT OF ENGINE DISPLAYS IN AIRCRAFT |
MIL S 81771 : A
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
MIL-L-5667 Revision B:1964
|
LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
DEFSTAN 61-3/5(1992) : INTERIM
|
GENERIC SPECIFICATION FOR BATTERIES, NON RECHARGEABLE, PRIMARY |
MIL W 6729 : C
|
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL STD 490 : A
|
SPECIFICATION PRACTICES |
DEFSTAN 08-46/2(2002) : 2002 AMD 2 2004
|
THE ELECTRIC, MAGNETIC AND ELECTROMAGNETIC ENVIRONMENT |
STANAG 3705 : 0
|
HUMAN ENGINEERING DESIGN CRITERIA FOR CONTROLS AND DISPLAYS IN AIRCREW STATIONS |
BS EN 60684-2:2011
|
Flexible insulating sleeving Methods of test |
MIL F 8815 : D
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
MIL-STD-962 Revision D:2003
|
DEFENSE STANDARDS FORMAT AND CONTENT |
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL Q 9858 : A
|
QUALITY PROGRAM REQUIREMENTS |
BS 2G 135:1967
|
SPECIFICATION FOR ELECTRICALLY-HEATED PITOT AND PITOTSTATIC PRESSURE HEADS |
MIL HDBK 838 : 0
|
LUBRICATION OF MILITARY EQUIPMENT |
DEFSTAN 13-91/2(1981) : 1981 AMD 2
|
MECHANICAL ARMING WIRE CONNECTIONS BETWEEN AIRBORNE ARMAMENT STORES AND ASSOCIATED SUSPENSION EQUIPMENT |
MIL-DTL-18307 Revision H:2006
|
NOMENCLATURE AND IDENTIFICATION FOR AERONAUTICAL SYSTEMS INCLUDING JOINT ELECTRONICS TYPE DESIGNATED SYSTEMS AND ASSOCIATED SUPPORT SYSTEMS |
MIL-V-25023 Revision B:1967
|
VALVE, FUEL DRAIN, SELF-LOCKING |
MIL C 11866 : C
|
CASTINGS, PRECISION, NONFERROUS |
MIL B 81757 : C
|
BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL C 7413 : B
|
COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
MIL-STD-1474 Revision E:2015
|
NOISE LIMITS |
STANAG 3441 : 2007
|
DESIGN OF AIRCRAFT STORES |
MIL HDBK 310 : 0
|
DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
MIL R 7726 : H SUPP 1
|
REPAIR AND REBUILDING OF USED AIRCRAFT PNEUMATIC TIRES |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
MIL P 15024/5 : 0
|
PLATE, IDENTIFICATION |
MIL STD 805 : B
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
BS 2M 41:1977
|
METHODS OF NUMBERING PROPULSION UNITS AND COMPONENTS AND DESCRIBING THEIR DIRECTION OF ROTATION |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL STD 1776 : 0
|
AIRCREW STATIONS AND PASSENGER ACCOMMODATION (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL I 18802 : A
|
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
DEFSTAN 05-126/2(1994) : 1994
|
THE CONTRACTORS REPAIR SUPPLY PROCEDURE |
DEFSTAN 47-17/1(1978) : 1978
|
ADAPTORS AND SEALS FOR PIPE CONNECTIONS TO AIRCRAFT PITOT/STATIC INSTRUMENTS AND ASSOCIATED EQUIPMENT |
STANAG 4670 : 2016
|
GUIDANCE FOR THE TRAINING OF UNMANNED AIRCRAFT SYSTEMS (UAS) OPERATORS |
MIL H 46855 : B
|
HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT & FACILITIES |
BS 6221-25:2000
|
PRINTED WIRING BOARDS - GUIDE TO THE REWORK AND REPAIR OF SOLDERED SURFACE MOUNTED PRINTED BOARD ASSEMBLIES |
DEFSTAN 00-14/3(1997) : 1997
|
THE USE OF ATLAS IN THE DEFENCE INDUSTRY |
MIL F 8490 : A NOTICE 1
|
FASTENER, CASE FOR EQUIPMENT RACK SYSTEM IN AIRCRAFT |
AECTP-300 : 2006
|
CLIMATIC ENVIRONMENTAL TESTS |
DEFSTAN 16-1/3(1992) : 1992 CORR 1997
|
OXYGEN; LIQUID AND GASEOUS (BREATHING) FOR AIRCRAFT SYSTEMS |
MIL STD 462 : D
|
MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
MIL HDBK 470 : A
|
DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1 |
MIL T 18606 : 0
|
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
DEFSTAN 81-121/3(2004) : 2004
|
RECONDITIONING OF AIRBORNE HIGH PRESSURE SEAMLESS STEEL GAS CONTAINERS |
MIL A 46108 : B
|
ARMOR, TRANSPARENT, GLASS; GLASS/PLASTIC; PLASTIC LAMINATES (GENERAL SPECIFICATION) |
BS 2X 26:2001
|
DOPING AND FINISHING SCHEMES FOR FABRIC COVERED AIRCRAFT |
DEFSTAN 05-57/5(2005) : 2005
|
CONFIGURATION MANAGEMENT OF DEFENCE MATERIEL |
STANAG 3258 : 0
|
POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
DEFSTAN 16-13/3(1989) : 1989
|
RECEPTION COUPLINGS AND NOZZLES FOR IN-FLIGHT REFUELLING OF AIRCRAFT |
STANAG 3687 : 90 AMD 2
|
CAMOUFLAGE OF AIRCRAFT |
MIL STD 2164 : 0
|
ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
MIL L 6484 : C
|
LIGHT, COCKPIT UTILITY, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL F 83860/1 : A
|
FILTER ELEMENT, FLUID PRESSURE, HYDRAULIC, AIRCRAFT, DISPOSABLE, 5 MICRON ABSOLUTE |
MIL S 7470 : A
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
STANAG 3219 : 0
|
LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
STANAG 4234 : 0
|
ELECTROMAGNETIC RADIATION (RADIO FREQUENCY) - 200 KHz TO 40 GHz ENVIRONMENT - AFFECTING THE DESIGN OF MATERIEL FOR USE BY NATO FORCES |
MIL D 9129 : D
|
DISCHARGERS, ELECTROSTATIC - GENERAL SPECIFICATION FOR |
MIL STD 1754 : 0
|
FASTENING DEVICES PREFERRED FOR DESIGN, LISTING OF |
MIL-PRF-38214 D:2008
|
COMPASS, MAGNETIC, MOUNTED |
MIL-HDBK-237 Revision D:2005
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS AND SPECTRUM SUPPORTABILITY GUIDANCE FOR THE ACQUISITION PROCESS |
DEFSTAN 47-22/1(1979) : 1979
|
END FITTINGS FOR FLEXIBLE HOSE ASSEMBLIES FOR AIRCRAFT - METRIC |
MIL R 8931 : A
|
RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
DEFSTAN 16-17/2(1983) : 1983
|
AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
DEFSTAN 00-1/2(1977) : 1977
|
EXTREME CLIMATIC CONDITIONS GOVERNING EQUIPMENT DESIGN |
MIL STD 1285 : D
|
MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
MIL STD 1629 : A
|
PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
MIL HDBK 691 : B
|
ADHESIVE BONDING |
MIL-DTL-5498 Revision G:2013
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
MIL-HDBK-6870 Revision B:2012
|
NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
MIL I 85071 : A
|
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
MIL P 83310 : 0
|
PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
MIL R 23761 : B
|
REGULATORS, VOLTAGE, AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
DEFSTAN 10-21/1(1976) : 1976 AMD 2
|
AIRCRAFT EJECTOR RELEASE UNITS FOR CONVENTIONAL MUNITIONS |
MIL T 28800 : E
|
TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
MIL L 87139 : 0
|
LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL STD 22 : D
|
WELDED JOINT DESIGN |
DEFSTAN 03-33/1(1993) : 1993
|
CHROMATE PASSIVATION OF CADMIUM AND ZINC SURFACES |
STANAG 7140 : 0
|
AIRCRAFT FLIGHT INSTRUMENTS - LAYOUT AND DISPLAY |
MIL A 9482 : 0
|
ANTI-ICING EQUIPMENT FOR AIRCRAFT HEATED SURFACE TYPE, GENERAL SPECIFICATION FOR |
STANAG 3105 : 2014
|
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
MIL STD 331 : D
|
FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
MIL H 8501 : A
|
HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (AF USE MIL F 83300) |
MIL-DTL-26499 Revision E:2006
|
HOSE ASSEMBLY, METAL, FLEXIBLE, BREATHING OXYGEN |
MIL S 6625 : A
|
SPRAY EQUIPMENT, AIRCRAFT WINDSHIELD, ANTI ICING |
A-A-59166 Revision A:2014
|
COATING COMPOUND, NONSLIP (FOR WALKWAYS) |
MIL F 18372 : 0
|
FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR) |
MIL DTL 27422 : F
|
TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
MIL L 25467 : D
|
LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
DEFSTAN 05-122/3(2006) : 2006
|
PROCEDURES FOR THE MILITARY REGISTRATION OF CIVIL-OWNED AIRCRAFT |
BS 3G 100-2.3.5:1972
|
SPECIFICATION FOR GENERAL REQUIREMENTS FOR EQUIPMENT FOR USE IN AIRCRAFT - ALL EQUIPMENT - ENVIRONMENTAL CONDITIONS - EXPLOSION-PROOFNESS |
MIL-HDBK-705 Revision C:1987
|
GENERATOR SETS, ELECTRICAL, MEASUREMENTS AND INSTRUMENTATIONS |
DEFSTAN 00-37/1(1988) : INTERIM
|
GUIDE TO THE PROCUREMENT OF A COMPUTER AIDED DESIGN [CAD] SYSTEM |
DEFSTAN 91-48/2(1997) : 1997
|
HYDRAULIC FLUID, PETROLEUM: SUPERCLEAN NATO CODE: H-515 JOINT SERVICE DESIGNATION: OM-15 HYDRAULIC FLUID, PETROLEUM: NORMAL NATO CODE: H-520 JOINT SERVICE DESIGNATION: OM-18 |
MIL T 9166 : B
|
TIE DOWN, CARGO, AIRCRAFT, CABLE NET 10,000 LB CAPACITY TYPE A 2 |
MIL-I-8670 Revision B:1993
|
INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
MIL STD 2161 : C
|
PAINT SCHEMES AND EXTERIOR MARKINGS FOR U.S. NAVY AND MARINE CORPS AIRCRAFT |
MIL E 8970 : 0
|
ENGINE AND RELATED PROPULSION AND POWER EQUIPMENT, AIRCRAFT, ACCEPTANCE TESTS OF, SAMPLING PLAN FOR, STATISTICAL |
MIL HDBK 2069 : 0
|
AIRCRAFT SURVIVABILITY |
MIL STD 2173 : 0
|
RELIABILITY-CENTERED MAINTENANCE REQUIREMENTS FOR NAVAL AIRCRAFT, WEAPONS SYSTEMS AND SUPPORT EQUIPMENT |
MIL-STD-1247 Revision D:2009
|
MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS |
MIL D 1000/1 : LATEST
|
DRAWING, ENGINEERING & ASSOCIATED DATA |
STANAG 1095 : 86 AMD 1
|
TIE-DOWN FITTINGS ON SHIPBOARD AIRCRAFT |
MIL L 16462 : B
|
LITTER, FOLDING, RIGID POLE |
STANAG 3329 : 0
|
NUMERALS AND LETTERS IN AIRCREW STATIONS |
MIL-S-416 Revision D:1979
|
STRAINER, WELL, WATER, WIRE WOUND |
MIL DTL 9129 : G
|
DISCHARGERS, ELECTROSTATIC, GENERAL SPECIFICATION FOR |
MIL-P-8564 Revision D:1970
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
STANAG 3462 : 0
|
AVAILABILITY OF WEIGHT AND BALANCE REQUIREMENTS AND LOADING CRITERIA FOR TRANSPORT AIRCRAFT |
DEFSTAN 59-113/1(2006) : 2006
|
LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT |
MIL B 5087 : B
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
DEFSTAN 61-1 : LATEST
|
MOTORS, ELECTRIC |
DEFSTAN 05-100/4(2009) : 2009
|
MINISTRY OF DEFENCE REQUIREMENTS FOR AIRCRAFT FLIGHT AND GROUND RUNNING |
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL W 5088 : L
|
WIRING, AEROSPACE VEHICLE |
MIL S 8698 : 0
|
STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS [ASG] |
DEFSTAN 00-50/1(1982) : 1982
|
GUIDE TO CHEMICAL ENVIRONMENTAL CONTAMINANTS AND CORROSION AFFECTING THE DESIGN OF MILITARY MATERIAL |
MIL-DTL-25427 Revision B:2009
|
COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL HDBK 274 : A
|
ELECTRICAL GROUNDING FOR AIRCRAFT SAFETY |
MIL PRF 7726 : K
|
RETREAD TIRES, RIBBED TREAD, PNEUMATIC AIRCRAFT |
BS 2X 33:1998
|
Specification for two component epoxy primer for aerospace purposes |
MIL HDBK 132 : A
|
PROTECTIVE FINISHES FOR METAL AND WOOD SURFACES |
BS 2C 12:1980
|
SPECIFICATION FOR JACKING PADS FOR AIRCRAFT |
MIL-HDBK-17-1 Revision F:2002
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 1: POLYMER MATRIX COMPOSITES GUIDELINES FOR CHARACTERIZATION OF STRUCTURAL MATERIALS |
MIL L 46010 : D
|
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
MIL-F-3541 Revision C:1989
|
FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
MIL T 5955 : C
|
TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
DEFSTAN 00-72/2(2005) : 2005
|
CHEMICAL AGENT RESISTANCE REQUIREMENTS FOR COATINGS APPLIED TO MILITARY EQUIPMENT |
MIL-STD-1289 Revision D:2003
|
AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
DEFSTAN 05-59/2(1988) : 1988
|
MAINTENANCE DATA AND DEFECT REPORTING IN THE ROYAL NAVY, THE ARMY AND THE ROYAL AIR FORCE |
MIL R 81589 : NOTICE 1
|
RAIN REPELLENT FLUID APPLICATION SYSTEM AIRCRAFT WINDSHIELD |
MIL-T-23103 Revision A:1971
|
THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
MIL DTL 83413 : C
|
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
MIL E 7080 : B
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
MIL P 87210 : 0
|
PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
MIL STD 2073 : 1978
|
DOD MATERIEL, PROCEDURES FOR DEVELOPMENT AND APPLICATION OF PACKAGING REQUIREMENTS |
MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL B 26220 : D
|
BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
MIL S 6144 : A
|
SOUND AND THERMAL INSULATION FOR AIRCRAFT GENERAL SPECIFICATION FOR THE INSTALLATION OF |
MIL S 85510 : 0
|
|
DEFSTAN 53-70/2(1976) : 1976 AMD 2
|
DIMENSIONS OF ELASTOMERIC TOROIDAL SEALING RINGS (INCH SERIES) FOR AIRCRAFT PURPOSES |
MIL A 19736 : A
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
BS EN 10203:1991
|
COLD REDUCED ELECTROLYTIC TINPLATE |
DEFSTAN 05-53/1(1981) : 1981
|
IDENTIFICATION OF DRAWINGS FOR THEIR RETRIEVAL |
MIL STD 781 : D
|
RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
MIL F 83870 : A
|
FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
DEFSTAN 59-15/1(1988) : INTERIM
|
ELASTOMERIC INSULATING MATERIALS & POLYTETRAFLUOROETHYLENE (PTFE) SLEEVING IN CONTINUOUS LENGTHS SLEEVES FOR BINDING AND/OR IDENTIFICATION PURPOSES APPROVAL |
DEFSTAN 80-15/2(1990) : 1990
|
PAINT, PRE-TREATMENT PRIMER (ETCHING PRIMER) - TYPES: BRUSHING (BASE AND ACID COMPONENT), SPRAYING (BASE AND ACID COMPONENT) |
MIL HDBK 221 : 0
|
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
SAE AMS M 3171 : 1998
|
MAGNESIUM ALLOY, PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION ON |
MIL S 6904 : B
|
SIGNAL, EMERGENCY WARNING, GENERAL SPECIFICATION FOR |
MIL P 5425 : D
|
PLASTIC, SHEET, ACRYLIC, HEAT RESISTANT |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
STANAG 3950 : 0
|
HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
DEFSTAN 16-7/3(1990) : 1990
|
COMPRESSED AIR, CHARACTERISTICS, SUPPLY, PRESSURE AND HOSES FOR TECHNICAL PURPOSES |
MIL HDBK 419 : A
|
GROUNDING, BONDING, AND SHIELDING FOR ELECTRONIC EQUIPMENTS AND FACILITIES - VOLUME 1: BASIC THEORY & VOLUME 2: APPLICATIONS |
STANAG 3209 : 2014
|
TYRE VALVE COUPLINGS |
MIL A 8860 : B
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
DEFSTAN 66-16/1(1975) : 1975
|
TEST SET, SAFETY, VOLTAGE DETECTION |
MIL C 7905 : G
|
CYLINDERS, STEEL COMPRESSED GAS, NONSHATTERABLE, SEAMLESS 1800 PSI AND 2100 PSI |
BS EN ISO 2063:2005
|
THERMAL SPRAYING - METALLIC AND OTHER INORGANIC COATINGS - ZINC, ALUMINIUM AND THEIR ALLOYS |
STANAG 3622 : 73 AMD 7
|
EXTERNAL VISION FROM AIRCREW STATIONS |
MIL-PRF-46010 Revision H:2013
|
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
MIL STD 705 : D
|
MOBILE ELECTRIC POWER SYSTEMS |
DEFSTAN 25-7/1(1968) : 1968 AMD 1
|
HORNS, ELECTRICAL |
DEFSTAN 00-52/3(1991) : 1991
|
THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |
MIL PRF 38039 : D
|
SYSTEMS, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
MIL HDBK 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
MIL-STD-1553 Revision B:1978
|
DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
BS EN 1964-3:2000
|
Transportable gas cylinders. Specification for the design and construction of refillable transportable seamless steel gas cylinders of water capacities from 0,5 litre up to and including 150 litres Cylinders made of seamless stainless steel with an Rm value of less than 1 100 MPa |
MIL M 13231 : C
|
MARKING OF ELECTRONIC ITEMS |
BS EN 60893-2:2004
|
Insulating materials. Industrial rigid laminated sheets based on thermosetting resins for electrical purposes Methods of test |
DEFSTAN 03-20/3(2005) : 2005
|
ELECTRO-DEPOSITION OF ZINC |
DEFSTAN 03-19/4(2010) : 2010
|
ELECTRO-DEPOSITION OF CADMIUM |
STANAG 3212 : 2017
|
DIAMETERS FOR GRAVITY FILLING ORIFICES |
MIL HDBK 17/2 : F
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 2: POLYMER MATRIX COMPOSITES MATERIALS PROPERTIES |
MIL STD 877 : 0
|
ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
MIL STD 765 : A
|
COMPASS SWINGING, AIRCRAFT, GENERAL REQUIREMENTS FOR |
DEFSTAN 91-19/1(1973) : 1973
|
LUBRICANT, SOLID FILM; HEAT CURED NATO CODE NO; S-1738 JOINT SERVICE DESIGNATION; ZX-34 |
DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984
|
V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC) |
DEFSTAN 91-101/3(2001) : 2001 AMD 1 2002
|
LUBRICATING OIL, GAS TURBINE ENGINE, SYNTHETIC GRADE 5 CST NATO CODE: O-156 JOINT SERVICE DESIGNATION: OX-27 AND OX-28 |
DEFSTAN 17-5/2(1986) : 1986
|
POWER DRIVEN HYDRAULIC GROUND SERVICING EQUIPMENT FOR AIRCRAFT |
MIL T 31000 : 0
|
TECHNICAL DATA PACKAGES - GENERAL SPECIFICATION FOR |
MIL-C-104 Revision C:1992
|
CRATES, WOOD: LUMBER AND PLYWOOD SHEATHED, NAILED, AND BOLTED |
MIL-C-81774A:1973
|
CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
MIL-STD-961 Revision E:2003
|
DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |