|
ISO 2631:1978
|
Guide for the evaluation of human exposure to whole-body vibration |
|
STANAG 3370 : 2004
|
AIRCREW STATION ALERTING SYSTEMS |
|
DEFSTAN 17-3/1(1972) : 1972
|
ADAPTORS, AIRCRAFT JACKING POINTS (DETACHABLE JACKING PADS) |
|
DTD 925 D : JUL 69
|
THE FABRICATION OF ACRYLIC PANELS AND SHAPINGS |
|
STANAG 3217 : 2006
|
OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
|
BS G 230:1984
|
SPECIFICATION FOR GENERAL REQUIREMENTS FOR AIRCRAFT ELECTRICAL CABLES (SECOND SERIES) |
|
STANAG 3341 : 72 AMD 6
|
EMERGENCY CONTROL COLOUR SCHEMES |
|
DEFSTAN 17-1/2(1984) : 1984
|
AIRCRAFT LIFTING SLINGS, APERTURE OF TERMINAL RING OR LINK |
|
BS G 175:1959
|
Aircraft fuel nozzle grounding plugs and sockets |
|
DTD 5577 : NOV 65
|
HEAT STABLE STRUCTURAL ADHESIVES |
|
STANAG 3659 : 2002
|
ELECTRICAL BONDING REQUIREMENTS FOR METALLIC AIRCRAFT SYSTEMS |
|
FAA AC 20-53 : 2006
|
PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
|
MIL E 22285 : 0
|
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
|
MIL B 83054 : B
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
|
DEFSTAN 59-113/2(2012) : 2012
|
LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT |
|
DTD 775 : A
|
ADHESIVE SUITABLE FOR JOINING METALS |
|
MIL P 46111 : C
|
PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
|
BS C 6:1966
|
SPECIFICATION FOR AIRCRAFT ENGINE NACELLE FIRE EXTINGUISHER DOORS |
|
MIL A 83377 : B
|
ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
|
DEFSTAN 05-18/5(2007) : 2007
|
SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS |
|
MIL C 7762 : A
|
COMPASS, INSTALLATION OF |
|
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
|
SAE J 1013 : 1992
|
MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES |
|
MIL O 27210 : F
|
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
|
DEFSTAN 05-19/1(1972) : 1972
|
LIMITS AND FITS FOR ENGINEERING |
|
DEFSTAN 53-9/1 : LATEST
|
BOLTS, MACHINE SCREWS, AND NUTS FOR AEROSPACE VEHICLES |
|
MIL HDBK 725 : 0
|
ADHESIVES - A GUIDE TO THEIR PROPERTIES AND USES AS DESCRIBED BY FEDERAL AND MILITARY SPECIFICATIONS |
|
DEFSTAN 17-10/2(1984) : 1984
|
TOWING ATTACHMENTS AND TOWING/STEERING EQUIPMENT FOR AIRCRAFT |
|
SAE AS 401 : 1993
|
POWERPLANT FIRE DETECTION INSTRUMENTS - THERMAL AND FLAME CONTACT TYPES (RECIPROCATING ENGINE POWERED AIRCRAFT) |
|
STANAG 3278 : 2014
|
AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
|
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 |
|
DEFSTAN 00-29/1(1982) : 1982
|
FUNGAL CONTAMINATION AFFECTING THE DESIGN OF MILITARY MATERIAL |
|
DEFSTAN 05-34/2(1984) : 1984
|
MARKING OF SERVICE MATERIAL |
|
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
|
DEFSTAN 05-21/1(1973) : 1973
|
QUALITY CONTROL SYSTEM REQUIREMENTS FOR INDUSTRY |
|
DEFSTAN 03-24/5(2008) : 2008
|
CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
|
DEFSTAN 53-88/1(1979) : 1979
|
WASHERS, LOCK, KEY (TAB) AND SPRING TENSION (CRINKLE), INCH SERIES, FOR AEROSPACE APPLICATIONS |
|
STANAG 3218 : 86 AMD 2
|
LOCATION, ACTUATION AND SHAPE OF ENGINE CONTROLS AND SWITCHES |
|
MIL A 9067 : C
|
ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR |
|
STANAG 3639 : 2004
|
AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
|
DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991
|
PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS |
|
DEFSTAN 05-61(PT12)/1(1987) : 1987
|
QUALITY ASSURANCE PROCEDURAL REQUIREMENTS - PART 12: CONTROL OF WALL THICKNESS IN DESIGN AND MANUFACTURE OF FLYING CONTROL SYSTEMS |
|
MIL S 58095 : A
|
SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
|
BS SP 90:1961
|
SPECIFICATION FOR CORROSION-RESISTING STEEL SPLIT COTTER PINS FOR AIRCRAFT |
|
BS G 212:1971
|
SPECIFICATION FOR GENERAL REQUIREMENTS FOR AIRCRAFT ELECTRICAL CABLES |
|
MIL D 21625 : G
|
DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
|
DTD 761C : DEC 65
|
SAFETY GLASS WINDSCREEN, WEAPON SIGHTING QUALITY |
|
STANAG 3216 : 84 AMD 4
|
LAYOUT OF FLIGHT DATA IN PILOTS DISPLAYS |
|
FAA AC 20-100 : 1977
|
GENERAL GUIDELINES FOR MEASURING FIRE-EXTINGUISHING AGENT CONCENTRATIONS IN POWERPLANT COMPARTMENTS |
|
DTD 5548 : AMD 1
|
GLAZING COMPOUNDS |
|
DTD 5627 : APR 82
|
FIBROUS POLYAMIDE MATERIAL FOR USE AS AN EXPLOSION SUPPRESSANT AND AS A BAFFLE MATERIAL IN AIRCRAFT FUEL TANKS |
|
MIL W 81752 : A
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
|
ASTM D 1781 : 1998
|
Standard Test Method for Climbing Drum Peel for Adhesives |
|
DTD 5624 : MAR 81
|
FIBROUS POLYESTER MATERIAL FOR USE AS A FLAME AND FIRE SUPPRESSANT IN AIRCRAFT DRY BAYS |
|
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 |
|
DTD 861A : DEC 59
|
ADHESIVE FOR METAL (LOW PRESSURE TYPE) |
|
ASTM D 3983 : 1998
|
Standard Test Method for Measuring Strength and Shear Modulus of Nonrigid Adhesives by the Thick-Adherend Tensile-Lap Specimen |
|
DEFSTAN 53-1/3(1981) : 1981 AMD 1 1984
|
USE OF UNIFIED SCREW THREADS |
|
DTD 218D : SEP 66
|
LAMINATED SAFETY GLASS |
|
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
EN 2243-2:2005
|
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 2: Peel metal-metal |
|
EN 2243-1 : 2005
|
AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 1: SINGLE LAP SHEAR |
|
STANAG 3611 : 73 AMD 4
|
CHARACTERISTICS OF COMPRESSED BREATHING AIR FOR AIRCRAFT USE |
|
STANAG 3593 : 1997
|
NUMBERING OF ENGINES AND THEIR ASSOCIATED CONTROLS AND DISPLAYS IN AIRCRAFT |
|
MIL P 8184 : E
|
PLASTIC SHEET, ACRYLIC, MODIFIED |
|
MIL P 6992 : 0
|
PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER |
|
STANAG 3224 : 2005
|
AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
|
DEFSTAN 07-55(PT2)SEC4/1(1975) : 1975 AMD 3 1983
|
ENVIRONMENTAL TESTING OF SERVICE MATERIAL - PART 2: TESTS - SECTION 4: PENETRATION AND IMMERSION |
|
MIL STD 1290 : A
|
LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
|
STANAG 3221 : 77 AMD 7
|
AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) IN AIRCRAFT DESIGN STANDARDS AND LOCATION OF CONTROLS |
|
MIL H 5484 : C
|
HEATER, AIRCRAFT, COMBUSTION TYPE |
|
MIL M 8609 : B
|
MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
|
BS 5423:1987
|
SPECIFICATION FOR PORTABLE FIRE EXTINGUISHERS |
|
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 |
|
BS 3A125 TO 3A[...](1981) : 1981
|
AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
|
STANAG 3208 : 2009
|
AIR CONDITIONING CONNECTIONS |
|
DEFSTAN 16-24/1(1983) : 1983
|
SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
|
STANAG 3766 : 2017
|
GREASE NIPPLES |
|
MIL F 23447 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
|
BS C 15:1960
|
Specification for coupling dimensions for aircraft-to-tractor tow bar connections |
|
ASTM E 229 : 1997
|
Standard Test Method for Shear Strength and Shear Modulus of Structural Adhesives (Withdrawn 2003) |
|
PREN 2101 : 1987
|
CHROMIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS |
|
EN 2243-4:2005
|
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test |
|
MIL STD 1472 : G
|
HUMAN ENGINEERING |
|
DTD 5625 : JUN 80
|
STANDARD ANNEALED FLOAT GLASS FOR AIRCRAFT GLAZING |
|
STANAG 3359 : 85 AMD 4
|
LOCATION AND ARRANGEMENT OF ENGINE DISPLAYS IN AIRCRAFT |
|
BS 6F 100:1998
|
Procedure for inspection and testing of textiles for aerospace purposes |
|
DTD 5576A : JAN 66
|
LAMINATED SAFETY GLASS HEATED BY ELECTRICALLY CONDUCTING FILM(S) |
|
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
|
MIL T 18606 : 0
|
TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
|
STANAG 3258 : 0
|
POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
|
PD 6484:1979
|
Commentary on corrosion at bimetallic contacts and its alleviation |
|
STANAG 3219 : 0
|
LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
|
DTD 5592 : LATEST
|
ACRYLIC SHEETS FOR AIRCRAFT GLAZING |
|
DEFSTAN 16-17/2(1983) : 1983
|
AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
|
MIL HDBK 691 : B
|
ADHESIVE BONDING |
|
MIL P 83310 : 0
|
PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
|
STANAG 3436 : 0
|
COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
|
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 : B
|
INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
|
STANAG 3225 : 75 AMD 7
|
LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS FOR ROTARY WING AIRCRAFT |
|
EN 2243-3:2005
|
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb core |
|
DEFSTAN 00-50/1(1982) : 1982
|
GUIDE TO CHEMICAL ENVIRONMENTAL CONTAMINANTS AND CORROSION AFFECTING THE DESIGN OF MILITARY MATERIAL |
|
BS 2C 12:1980
|
SPECIFICATION FOR JACKING PADS FOR AIRCRAFT |
|
MIL STD 1294 : A
|
ACOUSTICAL NOISE LIMITS IN HELICOPTERS |
|
MIL T 23103 : A
|
THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
|
MIL E 7080 : B
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
|
MIL S 85510 : 0
|
|
|
DTD 869A : NOV 57
|
LAMINATED SAFETY GLASS, HIGH LIGHT TRANSMISSION |
|
SBAC TS 120 : 6
|
AGS2000 SERIES STIFFNUTS (INCLUDING CLINCH NUTS) BA & BSF THREADS FOR AIRCRAFT |
|
SAE ARP 1524 : 2013
|
SURFACE PREPARATION AND PRIMING OF ALUMINUM ALLOY PARTS FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
|
MIL HDBK 221 : 0
|
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
|
DEFSTAN 61-12(PT20)/1(1980) : 1980
|
WIRES, CORDS, AND CABLES, ELECTRICAL - METRIC UNITS - PART 20: BRAIDS, WIRE |
|
STANAG 3950 : 0
|
HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
|
STANAG 3209 : 2014
|
TYRE VALVE COUPLINGS |
|
DTD 5626 : JUN 80
|
HIGH LIGHT TRANSMISSION ANNEALED PLATE GLASS FOR AIRCRAFT GLAZING |
|
STANAG 3622 : 73 AMD 7
|
EXTERNAL VISION FROM AIRCREW STATIONS |
|
DEFSTAN 25-7/1(1968) : 1968 AMD 1
|
HORNS, ELECTRICAL |
|
BS C 10:1958
|
Coupling dimensions for aircraft ground air-conditioning connections |