|
MIL F 5504 : B
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC MICRONIC TYPE |
|
BS 381C:1996
|
Specification for colours for identification, coding and special purposes |
|
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 |
|
DEFSTAN 66-6/4(1993) : 1993
|
OHMMETER, SAFETY, MULTI-RANGE, BATTERY POWERED SET |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
STANAG 3370 : 2004
|
AIRCREW STATION ALERTING SYSTEMS |
|
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 |
|
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 47-23/1(1980) : 1980
|
BEAD PROFILE FOR AIRCRAFT PIPING AND DUCTING (FLEXIBLE CONNECTIONS) |
|
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
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 |
|
DEFSTAN 59-113/2(2012) : 2012
|
LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT |
|
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 |
|
DEFSTAN 81-24/5(2004) : 2004
|
IDENTIFICATION MARKING OF TRANSPORTABLE CONTAINERS, COMPRESSED GAS |
|
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) |
|
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 |
|
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 |
|
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 |
|
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 |
|
STANAG 3643 : 0
|
COATING REFLECTION REDUCING FOR GLASS ELEMENTS USED IN AIRCREW STATION DISPLAYS |
|
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 |
|
DEFSTAN 81-14/7(2012) : 2012
|
CASES, WOOD (BATTEN AND BOARD CONSTRUCTION) |
|
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 |
|
BS EN ISO 9241-1:1997
|
ERGONOMIC REQUIREMENTS FOR OFFICE WORK WITH VISUAL DISPLAY TERMINAL (VDTS) - GENERAL INTRODUCTION |
|
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 2127:1992
|
AEROSPACE SERIES - ALUMINIUM ALLOY AL-P7075-T73511 - EXTRUDED BARS AND SECTIONS A OR D <= 100 MM |
|
DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991
|
PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS |
|
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 |
|
BS G 262:1998
|
AIRCRAFT - DECLARATION OF DESIGN AND PERFORMANCE FOR AIRCRAFT EQUIPMENT - STANDARD FORM |
|
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 |
|
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 |
|
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 |
|
MIL P 15024 : E
|
PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
|
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 |
|
BS EN ISO 14001:2015
|
Environmental management systems. Requirements with guidance for use |
|
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 |
|
NFPA 326 : 2015
|
SAFEGUARDING OF TANKS AND CONTAINERS FOR ENTRY, CLEANING, OR REPAIR |
|
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 |
|
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 |
|
DEFSTAN 61-17/5(2009) : 2009
|
THE SELECTION AND INTRODUCTION OF BATTERIES AND FUEL CELLS FOR SERVICE USE |
|
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] |
|
DEFSTAN 05-10/4(1990) : 1990
|
DRAWING PROCEDURE |
|
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 |
|
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 |
|
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 |
|
BS ISO 10074:2010
|
ANODIZING OF ALUMINIUM AND ITS ALLOYS - SPECIFICATION FOR HARD ANODIC OXIDATION COATINGS ON ALUMINIUM AND ITS ALLOYS |
|
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 |
|
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 |
|
BS ISO 461-1:2003
|
AIRCRAFT - CONNECTORS FOR GROUND ELECTRICAL SUPPLIES - PART 1: DESIGN, PERFORMANCE AND TEST REQUIREMENTS |
|
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 |
|
BS EN 971-1:1996
|
PAINTS AND VARNISHES - TERMS AND DEFINITIONS FOR COATING MATERIALS - GENERAL TERMS |
|
SAE AS 18012 : 1998
|
MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
|
BS 5852-1:1979
|
Fire tests for furniture Methods of test for the ignitability by smokers\' materials of upholstered composites for seating |
|
STANAG 3447 : 2016
|
AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
|
BS SP115-117(1956) : 1956
|
SPECIFICATIONS FOR HYDRAULIC SURFACE-CHECK TYPE LUBRICATING NIPPLES FOR AIRCRAFT |
|
MIL F 23447 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
|
DEFSTAN 80-161/2(2002) : 2002
|
PAINT, FINISHING, SPRAYING, EPOXY, MULTI-PACK |
|
DEFSTAN 59-31/2 : LATEST
|
LIGHTING PROTECTION |
|
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 |
|
DEFSTAN 80-214/3(2009) : 2009
|
PAINT, FINISH, SELECTIVELY STRIPPABLE, ACRYLIC - TYPES: BRUSHING, SPRAYING |
|
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 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 |
|
STANAG 3436 : 0
|
COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
|
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 |
|
BS 2X 32:1998
|
SPECIFICATION FOR PRE-TREATMENT ETCH PRIMER FOR AEROSPACE PURPOSES |
|
MIL STD 2161 : C
|
PAINT SCHEMES AND EXTERIOR MARKINGS FOR U.S. NAVY AND MARINE CORPS AIRCRAFT |
|
DEFSTAN 61-6/3(1989) : 1989
|
AIRCRAFT ELECTRICAL CIRCUIT IDENTIFICATION |
|
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 |
|
SAE AS 8045 : 2011
|
MINIMUM PERFORMANCE STANDARD FOR UNDERWATER LOCATING DEVICES (ACOUSTIC) (SELF-POWERED) |
|
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 |
|
SAE AS 6254 : 2015
|
MINIMUM PERFORMANCE STANDARD FOR LOW FREQUENCY UNDERWATER LOCATING DEVICES (ACOUSTIC) (SELF-POWERED) |
|
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 |
|
DEFSTAN 00-80/1(2012) : 2012
|
SOLAR HEAT REFLECTANCE REQUIREMENTS OF PAINTS FOR MILITARY EQUIPMENT |
|
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 |