|
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 |
|
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 |
|
MIL PRF 83870 : C
|
FILTER ELEMENT, DISPOSABLE, 20 MICRON ABSOLUTE, CONSTANT SPEED DRIVE, AIRCRAFT |
|
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) |
|
ASTM B 80 : 2015 : REDLINE
|
Standard Specification for Magnesium-Alloy Sand Castings |
|
DEFSTAN 08-11/1(2000) : 2000
|
NBC PROTECTION FOR AIR PLATFORMS |
|
DEFSTAN 03-11/5(2008) : 2008
|
PHOSPHATE TREATMENT OF IRON AND STEEL |
|
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 |
|
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 |
|
DEFSTAN 00-00/2(2014) : 2014
|
A STANDARD FOR DEFENCE STANDARDS: MANAGEMENT AND PRODUCTION |
|
BS 2087-1:1992
|
PRESERVATIVE TEXTILE TREATMENTS - SPECIFICATION FOR TREATMENTS |
|
MIL-STD-1365 Revision C:2010
|
GENERAL DESIGN CRITERIA FOR HANDLING EQUIPMENT ASSOCIATED WITH WEAPONS AND RELATED ITEMS |
|
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 |
|
MIL STD 1530 : D
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
|
STANAG 3368 : 2014
|
INTERNAL AIRCRAFT ENGINE STARTING SYSTEM |
|
DEFSTAN 05-61/1(1983) : 1983
|
QUALITY ASSURANCE PROCEDURAL REQUIREMENTS |
|
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) |
|
MIL HDBK 273 : 0
|
SURVIVABILITY ENHANCEMENT, AIRCRAFT NUCLEAR WEAPON THREAT, DESIGN AND EVALUATION GUIDELINES |
|
SAE ARP 1179 : 2011
|
AIRCRAFT GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT |
|
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 |
|
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 |
|
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 |
|
DEFSTAN 03-36/2(2010) : 2010
|
GUIDANCE TO THE USE OF CADMIUM ALTERNATIVES IN THE PROTECTIVE COATING OF DEFENCE EQUIPMENT |
|
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 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 E 22285 : 0
|
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
|
AECTP-400 : 2006
|
MECHANICAL ENVIRONMENTAL TESTS |
|
SAE J 1966 : 2011
|
LUBRICATING OILS, AIRCRAFT PISTON ENGINE (NON-DISPERSANT MINERAL OIL) |
|
MIL I 18373 : B
|
INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
|
DEFSTAN 59-113/2(2012) : 2012
|
LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT |
|
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 P 46111 : C
|
PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
|
MIL-HDBK-728-4 Revision A:1993
|
MAGNETIC PARTICLE TESTING |
|
DEFSTAN 00-10/3(1986) : 1986 AMD 2 1993
|
GENERAL DESIGN AND MANUFACTURING REQUIREMENTS FOR SERVICE ELECTRONIC EQUIPMENT |
|
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 |
|
DEFSTAN 03-14/4(2008) : 2008
|
ELECTRODEPOSITION OF CHROMIUM FOR ENGINEERING PURPOSES |
|
MIL D 23222 : A
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
|
MIL PRF 83860 : D
|
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE |
|
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 |
|
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 |
|
DEFSTAN 61-7(PT2)/3(1991) : 1991
|
IDENTIFICATION OF ELECTRICAL AND ELECTRONIC SYSTEMS, WIRING AND COMPONENTS - PART 2: MARKING CODE FOR ELECTRICAL AND ELECTRONIC EQUIPMENT |
|
SAE ARP 4418 : 2008
|
PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES |
|
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
|
MIL PRF 27210 : J
|
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
|
DEFSTAN 03-4/6(2011) : 2011
|
THE PRE-TREATMENT AND PROTECTION OF STEEL ITEMS OF SPECIFIED MAXIMUM TENSILE STRENGTH EXCEEDING 1450 MPA |
|
SAE ARP 8615 : 2011
|
FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR |
|
STANAG 3315 : 1998
|
AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS |
|
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 00-600/3(2014) : 2014
|
INTEGRATED LOGISTIC SUPPORT - REQUIREMENTS FOR MOD PROJECTS |
|
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 |
|
STANAG 3542 : 2011
|
TECHNICAL CRITERIA FOR THE TRANSPORT OF CARGO BY HELICOPTER |
|
STANAG 3701 : 0
|
AIRCRAFT INTERIOR COLOUR SCHEMES |
|
MIL HDBK 725 : 0
|
ADHESIVES - A GUIDE TO THEIR PROPERTIES AND USES AS DESCRIBED BY FEDERAL AND MILITARY SPECIFICATIONS |
|
DEFSTAN 81-14/8(2013) : 2013
|
CASES, WOOD (BATTEN AND BOARD CONSTRUCTION) |
|
MIL A 87229 : 0
|
AUXILIARY POWER SYSTEMS, AIRBORNE |
|
MIL E 85583 : A
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
|
DEFSTAN 00-3/4(2011) : 2011
|
DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
|
MIL STD 2073/1 : E
|
STANDARD PRACTICE FOR MILITARY PACKAGING |
|
BS EN ISO 4618:2014
|
Paints and varnishes. Terms and definitions |
|
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 |
|
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 |
|
STANAG 3312 : 0
|
PROFILE DIMENSIONS OF FLANGES FOR V-BAND COUPLINGS FOR PIPING AND DUCTING |
|
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 |
|
MIL STD 8651 : 0
|
INSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT) |
|
DEFSTAN 07-55(PT1)/1(1975) : 1975 AMD 3 1983
|
ENVIRONMENTAL TESTING OF SERVICE MATERIAL - PART 1: GENERAL REQUIREMENTS |
|
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
|
|
|
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-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 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 |
|
STANAG 3372 : 2014
|
LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
|
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 |
|
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
|
DEFSTAN 59-71/1(1988) : 1988 AMD 1 1990
|
CRIMPED ELECTRICAL CONNECTIONS FOR COPPER CONDUCTORS - GENERIC SPECIFICATION |
|
ASTM D 6576 : 2013 : REDLINE
|
Standard Specification for Flexible Cellular Rubber Chemically Blown |
|
JSSG 2000 : B
|
AIR SYSTEM |
|
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 03-24/5(2008) : 2008
|
CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
|
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 15-2/1(1987) : 1987
|
FLEXIBLE TANKS FOR USE IN AIRCRAFT FUEL AND METHANOL/WATER SYSTEMS |
|
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 |
|
MIL-DTL-23227 Revision F:1997
|
TUBE AND PIPE, NICKEL-CHROMIUM-IRON ALLOY (UNS N06600) |
|
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 |
|
DEFSTAN 00-44/2(2012) : 2012
|
RELIABILITY AND MAINTAINABILITY DATA COLLECTION AND CLASSIFICATION |
|
BS 7863:2009
|
RECOMMENDATIONS FOR COLOUR CODING TO INDICATE THE EXTINGUISHING MEDIA CONTAINED IN PORTABLE FIRE EXTINGUISHERS |
|
DEFSTAN 03-3/5(2011) : 2011
|
PROTECTION OF ALUMINIUM ALLOYS BY SPRAYED METAL COATINGS |
|
STANAG 3525 : 0
|
SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
|
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 |
|
BS 2C7(1984) : 1984
|
SPECIFICATION FOR AIRCRAFT TYRE VALVES: INTERCHANGEABILITY DIMENSIONS |
|
STANAG 3302 : 81 AMD 5
|
CONNECTORS FOR 28 VOLT "DC" SERVICING POWER |
|
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 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 |
|
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
|
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 |
|
MIL STD 1760 : E
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
|
DEFSTAN 17-4/3(1986) : 1986
|
PICKETING (TIE-DOWN) FITTINGS FOR SHIPBORNE AIRCRAFT (INCLUDING HELICOPTERS) |
|
MIL HDBK 2089 : 0
|
AIRCRAFT SURVIVABILITY TERMS |
|
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-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-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-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 |
|
NASM 25049 : REV 1
|
KNOBS, CONTROL, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
|
STANAG 3416 : 0
|
METHANOL/WATER AND DEMINERALIZED WATER REPLENISHMENT |
|
AECTP-500 : 2016
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
|
DEFSTAN 03-8/2(1992) : 1992
|
ELECTRO-DEPOSITION OF TIN |
|
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
MIL STD 889 : C
|
DISSIMILAR METALS |
|
DEFSTAN 16-23/2(1982) : 1982
|
FLOOR FITTINGS FOR CARGO TRANSPORT AIRCRAFT APERTURES FOR TIE-DOWN POINTS |
|
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-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 |
|
STANAG 3237 : 1997
|
APERTURE OF TERMINAL RING OR LINK OF AIRCRAFT LIFTING SLINGS |
|
BS EN ISO 14001:2015
|
Environmental management systems. Requirements with guidance for use |
|
MIL HDBK 728/2 : 0
|
EDDY CURRENT TESTING |
|
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 |
|
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 |
|
STANAG 3334 : 96 AMD 1
|
DEFUELLING OF AIRCRAFT |
|
MIL P 9400 : C
|
PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
|
SAE ARP 492 : 2014
|
AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST |
|
SAE AMS A 25463 : 2013
|
ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
|
DEFSTAN 47-12/4(1987) : 1987
|
POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES (WIRE REINFORCED) FOR MEDIUM AND HIGH PRESSURE FLUID SYSTEMS IN AIRCRAFT |
|
IEC TS 62239-1:2015
|
Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan |
|
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 |
|
DEFSTAN 15-3 : LATEST
|
TRANSPARENT GLAZING MATERIALS AND ACCESSORIES FOR AEROSPACE APPLICATIONS |
|
STANAG 3647 : 0
|
NOMENCLATURE IN AIRCREW STATIONS |
|
DEFSTAN 81-46/3(2005) : 2005
|
BOARD, CORRUGATED, DOUBLE-FACED (TYPES A, B AND C) |
|
SAE ARP 4761 : 1996
|
GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
|
ASTM D 3983 : 1998
|
Standard Test Method for Measuring Strength and Shear Modulus of Nonrigid Adhesives by the Thick-Adherend Tensile-Lap Specimen |
|
MIL STD 464 : C
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
|
SAE AMS P 83310 : 2016
|
PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
|
STANAG 2133 : 2004
|
VULNERABILITY ANALYSIS OF CHEMICAL AND BIOLOGICAL HAZARDS |
|
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
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 08-5/1(1984) : 1984 ADDENDUM 1998
|
DESIGN REQUIREMENTS FOR WEAPON SYSTEMS (GUIDED WEAPONS, TORPEDOES AND AIRBORNE ARMAMENT STORES) |
|
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
STANAG 3230 : 2007
|
EMERGENCY MARKINGS ON AIRCRAFT |
|
DEFSTAN 80-143/2(2006) : 2006
|
CORROSION PREVENTIVE, AUTOMOTIVE, UNDERBODY AND HOLLOW SECTION: JOINT SERVICE DESIGNATION: PX-28 |
|
MIL PRF 27260 : D
|
TIE DOWN, CARGO, AIRCRAFT CGU-1/B |
|
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 |
|
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 |
|
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 00-971/1(1987) : 1987
|
GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
|
DEFSTAN 05-10/4(1990) : 1990
|
DRAWING PROCEDURE |
|
DEFSTAN 03-7/1(1973) : 1973
|
PAINTING OF METAL AND WOOD |
|
STANAG 3611 : 73 AMD 4
|
CHARACTERISTICS OF COMPRESSED BREATHING AIR FOR AIRCRAFT USE |
|
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-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 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. |
|
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 |
|
ASTM D 4529 : 2017 : REDLINE
|
Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
|
MIL HDBK 336/2 : 0
|
SURVIVABILITY, AIRCRAFT, NONNUCLEAR, AIRFRAME - VOLUME 2 |
|
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 |
|
STANAG 3575 : 0
|
AIRCRAFT STORES EJECTOR RACKS |
|
MIL L 8552 : C
|
LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
|
IPC 2221B:2012
|
GENERIC STANDARD ON PRINTED BOARD DESIGN |
|
DEFSTAN 61-7(PT1)/6(1990) : 1990
|
IDENTIFICATION OF ELECTRICAL AND ELECTRONIC SYSTEMS, WIRING AND COMPONENTS - PART 1: COLOUR CODING AND MARKING FOR POLARITY AND PHASE DISTINCTION IN ELECTRICAL SYSTEMS |
|
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 |
|
STANAG 3224 : 2005
|
AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
|
DEFSTAN 66-7(PT1)/3(1983) : 1983 AMD 1 1985
|
INSTRUMENTS, ELECTRICAL INDICATING (SEALED) 50 MM TO 100 MM - PART 1: SPECIFICATION |
|
AFGS-87154 Revision A:1992
|
FUEL SYSTEMS, GENERAL DESIGN SPECIFICATION FOR |
|
BS 5X 17(1998) : 1998
|
SPECIFICATION FOR OLEORESINOUS VARNISH FOR AEROSPACE PURPOSES |
|
JSSG 2001 : B
|
AIR VEHICLE |
|
MIL STD 1290 : A
|
LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
|
MIL PRF 32070 : A
|
TEST PROGRAM SETS |
|
DEFSTAN 03-18/5(2012) : 2012
|
CHROMATE CONVERSION COATINGS (CHROMATE FILMING TREATMENTS) GRADES: STANDARD AND BRUSHING FOR ALUMINIUM AND ALUMINIUM ALLOYS |
|
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 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 |
|
STANAG 4327 : 0
|
LIGHTNING, MUNITION ASSESSMENT AND TEST PROCEDURES |
|
BS 3G 230:2000
|
Specification for general requirements for aircraft electrical cables (second series) |
|
MIL-M-8609 Revision B:1965
|
MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
|
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 |
|
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 |
|
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) |
|
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-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-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 |
|
BS 4M 45-1:1998
|
AIRCRAFT TYRES AND RIMS - SPECIFICATIONS |
|
MIL F 25173 : A
|
FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT |
|
DEFSTAN 61-10/4(1984) : 1984
|
GENERATOR SETS (GROUND, ENGINE DRIVEN) |
|
MIL HDBK 728/3 : 0
|
LIQUID PENETRANT TESTING |
|
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 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 |
|
BS 4C 14:1991
|
SPECIFICATION FOR AIRCRAFT PRESSURE REFUELLING CONNECTORS |
|
STANAG 4155 : 0
|
NCB PROTECTIVE MASK AND FILTER CANNISTER SCREW THREADS |
|
ASTM E 2375 : 2016 : REDLINE
|
Standard Practice for Ultrasonic Testing of Wrought Products |
|
MIL HDBK 728/6 : 0
|
ULTRASONIC TESTING |
|
ASTM E 1444 : 2005
|
Standard Practice for Magnetic Particle Testing |
|
STANAG 4702 : 2016
|
ROTARY WING UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS |
|
MIL A 8867 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
|
SAE AS 18276 : 2014
|
LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
|
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 |
|
STANAG 4703 : 2016
|
LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQURIEMENTS |
|
MIL PRF 5041 : K
|
TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT |
|
MIL A 8861 : B
|
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
|
SAE AS 5604 : 2012
|
COMPASS: MAGNETIC, PILOT'S STANDBY |
|
DEFSTAN 16-24/1(1983) : 1983
|
SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
|
STANAG 3766 : 2017
|
GREASE NIPPLES |
|
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 |
|
DEFSTAN 05-65/1(1984) : 1984
|
RADIOGRAPHIC INSPECTION |
|
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 |
|
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 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 |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
JSSG 2009 : A
|
AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE) |
|
MIL STD 1472 : G
|
HUMAN ENGINEERING |
|
MIL PRF 25690 : B
|
PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
|
DEFSTAN 00-55(PT1)/3(2014) : 2014
|
REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
|
DEFSTAN 00-49/3(2014) : 2014
|
MOD GUIDE TO R&M TERMINOLOGY USED IN REQUIREMENTS |
|
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 STD 1366 : E
|
INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
|
STANAG 3359 : 85 AMD 4
|
LOCATION AND ARRANGEMENT OF ENGINE DISPLAYS IN AIRCRAFT |
|
MIL W 6729 : C
|
WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR |
|
STANAG 3705 : 0
|
HUMAN ENGINEERING DESIGN CRITERIA FOR CONTROLS AND DISPLAYS IN AIRCREW STATIONS |
|
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 |
|
MIL HDBK 728/1 : 0
|
NONDESTRUCTIVE TESTING |
|
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
|
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 |
|
BS ISO 3324-1:2013
|
AIRCRAFT TYRES AND RIMS - PART 1: SPECIFICATIONS |
|
MIL-DTL-18307 Revision H:2006
|
NOMENCLATURE AND IDENTIFICATION FOR AERONAUTICAL SYSTEMS INCLUDING JOINT ELECTRONICS TYPE DESIGNATED SYSTEMS AND ASSOCIATED SUPPORT SYSTEMS |
|
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 P 15024/5 : 0
|
PLATE, IDENTIFICATION |
|
DEFSTAN 00-55(PT2)/2(1997) : 1997 ERRATUM 1997
|
REQUIREMENTS FOR SAFETY RELATED SOFTWARE IN DEFENCE EQUIPMENT - PART 2: GUIDANCE |
|
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-HDBK-728-5 Revision A:1994
|
RADIOGRAPHIC TESTING - VOLUME 5 |
|
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
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 |
|
BS 6221-25:2000
|
PRINTED WIRING BOARDS - GUIDE TO THE REWORK AND REPAIR OF SOLDERED SURFACE MOUNTED PRINTED BOARD ASSEMBLIES |
|
AECTP-300 : 2006
|
CLIMATIC ENVIRONMENTAL TESTS |
|
DEFSTAN 16-1/3(1992) : 1992 CORR 1997
|
OXYGEN; LIQUID AND GASEOUS (BREATHING) FOR AIRCRAFT SYSTEMS |
|
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 |
|
STANAG 3258 : 0
|
POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
|
STANAG 3687 : 90 AMD 2
|
CAMOUFLAGE OF AIRCRAFT |
|
STANAG 3576 : 2016
|
ELECTRICAL CONNECTOR FOR DISPENSERS AND INTERNAL INTERVALOMETER TYPE ROCKET LAUNCHERS FOR AIRCRAFT |
|
BS EN ISO 17834:2003
|
Thermal spraying. Coatings for protection against corrosion and oxidation at elevated temperatures |
|
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-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 |
|
DEFSTAN 16-17/2(1983) : 1983
|
AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
|
MIL STD 1285 : D
|
MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
|
MIL HDBK 691 : B
|
ADHESIVE BONDING |
|
MIL HDBK 336/1 : 0
|
SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA - VOLUME 1 |
|
DEFSTAN 08-41(PT1)/1(1997) : 1997
|
CHEMICAL AND BIOLOGICAL HARDENING OF MILITARY EQUIPMENT - PART 1: GENERAL REQUIREMENTS ASSESSMENT AND TESTING |
|
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 |
|
DEFSTAN 00-970/1(1983) : 1983
|
DESIGN REQUIREMENTS FOR SERVICE AIRCRAFT |
|
MIL STD 22 : D
|
WELDED JOINT DESIGN |
|
STANAG 3436 : 0
|
COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
|
DEFSTAN 05-57/6(2014) : 2014
|
CONFIGURATION MANAGEMENT OF DEFENCE MATERIEL |
|
DEFSTAN 03-33/1(1993) : 1993
|
CHROMATE PASSIVATION OF CADMIUM AND ZINC SURFACES |
|
STANAG 7140 : 0
|
AIRCRAFT FLIGHT INSTRUMENTS - LAYOUT AND DISPLAY |
|
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-DTL-26499 Revision E:2006
|
HOSE ASSEMBLY, METAL, FLEXIBLE, BREATHING OXYGEN |
|
A-A-59166 Revision A:2014
|
COATING COMPOUND, NONSLIP (FOR WALKWAYS) |
|
MIL DTL 27422 : F
|
TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
|
MIL L 25467 : D
|
LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
|
MIL HDBK 336/3 : 0
|
SURVIVABILITY, AIRCRAFT, NONNUCLEAR, ENGINE - VOLUME 3 |
|
MIL-HDBK-705 Revision C:1987
|
GENERATOR SETS, ELECTRICAL, MEASUREMENTS AND INSTRUMENTATIONS |
|
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-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 HDBK 2069 : 0
|
AIRCRAFT SURVIVABILITY |
|
MIL D 1000/1 : LATEST
|
DRAWING, ENGINEERING & ASSOCIATED DATA |
|
STANAG 3225 : 75 AMD 7
|
LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS FOR ROTARY WING AIRCRAFT |
|
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 |
|
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) |
|
DEFSTAN 91-4/9(2013) : 2013
|
FUEL, NAVAL, DISTILLATE NATO CODE: F-76 JOINT SERVICE DESIGNATION DIESO F-76 |
|
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL W 5088 : L
|
WIRING, AEROSPACE VEHICLE |
|
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 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 |
|
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 |
|
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 |
|
MIL DTL 83413 : C
|
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-35/2(1996) : 1996 AMD 1 1997
|
ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL |
|
MIL A 19736 : A
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
|
BS EN 10203:1991
|
COLD REDUCED ELECTROLYTIC TINPLATE |
|
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 |
|
DEFSTAN 07-55(PT2)SEC6/1(1976) : 1976 AMD 1 1983
|
ENVIRONMENTAL TESTING OF SERVICE MATERIAL - PART 2: TESTS - SECTION 6: FIRE AND EXPLOSION |
|
BS ISO 7295 : 1988
|
AEROSPACE SERIES - TYRE VALVES FOR AIRCRAFT - INTERCHANGEABILITY DIMENSIONS |
|
STANAG 3950 : 0
|
HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
|
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 |
|
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 |
|
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 |
|
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 |
|
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 |
|
MIL-C-81774A:1973
|
CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
MIL-STD-961 Revision E:2003
|
DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
|
DEFSTAN 00-52/4(2014) : 2014
|
THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |
|
DEFSTAN 66-7(PT2)/1(1971) : AMD 6
|
INSTRUMENTS, ELECTRICAL INDICATING (SEALED) - PART 2: LIST OF INSTRUMENTS |