DEFSTAN 00-970(PT0)/12(2014) : 2014
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Available format(s)
Hardcopy , PDF
Superseded date
11-07-2014
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
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Preface
Section One - General
0 Introduction
1 Scope
2 Warning
3 Normative References
4 Definitions
Section Two - Format of 00-970
Section Three - Use of 00-970
Section Four - Qualification of Equipment for Use on Aircraft
Section Five - Amendment Procedure
Section Six - Status of Issue
Annex A - Table of Contents
Annex B - Applicable NATO Standardization Agreements (STANAGs)
Annex C - Applicable UK Defence Standards
Annex D - US Military Specifications
Annex E - Other Related Specifications
Annex F - Definitions
Annex G - Suspect Text Reporting
Specifies guidance and content information, together with definitions of the terms used throughout this document.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT0)/11(2013). (02/2014)
|
| DocumentType |
Standard
|
| Pages |
85
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-F-5504 Revision B:1958 | Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type |
| MIL-STD-850 Revision B:1970 | AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT |
| DEFSTAN 47-25/1(1982) : 1982 | PIPELINES AND PIPE COUPLINGS FOR AIRCRAFT FLUID SYSTEMS (METRIC) |
| SAE AS50571B | Lights, Instrument, Individual, General Specification For |
| MIL-T-5522 Revision D:1975 | 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 |
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| BS 6221-20:1984 | Printed wiring boards Guide for the assembly of printed wiring boards |
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| BS 7867:1997 | Specification for portable fire extinguishers for use in aircraft |
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| DEFSTAN 17-3/1(1972) : 1972 | ADAPTORS, AIRCRAFT JACKING POINTS (DETACHABLE JACKING PADS) |
| STANAG 3456 : 0 | AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
| MIL-STD-13231 Base Document:1999 | MARKING OF ELECTRONIC ITEMS |
| MIL-I-6115 Revision A:1951 | 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 Normalized steel cylinders |
| 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 Base Document:1954 | TEST REQUIREMENTS, GROUND HELICOPTER |
| DEFSTAN 03-11/5(2008) : 2008 | PHOSPHATE TREATMENT OF IRON AND STEEL |
| MIL-HDBK-505 Base Document:1998 | Definitions of Item Levels, Item Exchangeability, Models, and Related Terms |
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| SAE AMSA21180B | Aluminum-Alloy Castings, High Strength |
| STANAG 4671 : 2017 | UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS (USAR) |
| STANAG 3558 : 2002 | LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES |
| MIL-HDBK-965 Base Document:1996 | ACQUISITION PRACTICES FOR PARTS MANAGEMENT |
| MIL-A-25175 Revision C:1976 | 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 Revision A:1969 | DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
| MIL-HDBK-729 Base Document:1983 | 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 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| STANAG 3368 : 2014 | INTERNAL AIRCRAFT ENGINE STARTING SYSTEM |
| SAE AS8090A | 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 Revision R:2014 | Military Marking for Shipment and Storage |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| MIL-A-46146 Revision B:1990 | ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
| MIL-HDBK-273 Base Document:1983 | SURVIVABILITY ENHANCEMENT, AIRCRAFT NUCLEAR WEAPON THREAT, DESIGN AND EVALUATION GUIDELINES |
| SAE ARP1179D | 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 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MIL-F-25381 Revision A:1972 | 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 |
| MIL-HDBK-173 Revision A:1973 | 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 |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-HDBK-241 Revision B:1983 | 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 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL-STD-1555 Base Document:1973 | AIRCREW STATION DISPLAYS AND ASSOCIATED EQUIPMENT, DEFINITIONS OF |
| SAE AS18607 | THERMAL ANTI-ICING EQUIPMENT, WING AND EMPENNAGE |
| 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 Base Document:1997 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-STD-101 Revision C:2014 | COLOR CODE FOR PIPELINES AND FOR COMPRESSED GAS CYLINDERS |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL-E-22285 Base Document:1959 | EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
| MIL-M-46062 Revision C:1985 | MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH |
| AECTP-400 : 2006 | MECHANICAL ENVIRONMENTAL TESTS |
| SAE J1966_201108 | 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 Revision A:1981 | 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 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL STD 2084 : 0 | GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
| MIL-P-46111 Revision C:1978 | PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
| MIL-P-8686 Base Document:1955 | 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 Revision B:1991 | TEST PROGRAM SETS GENERAL REQUIREMENTS FOR |
| 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 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| MIL-W-5044 Revision C:1970 | WALKWAY COMPOUND, NONSLIP AND WALKWAY MATTING, NONSLIP |
| DEFSTAN 03-14/4(2008) : 2008 | ELECTRODEPOSITION OF CHROMIUM FOR ENGINEERING PURPOSES |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| MIL-D-23222 Revision A:1971 | DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
| MIL-PRF-83860 Revision D:2013 | 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 |
| MIL-HDBK-46855 Revision A:1999 | HUMAN ENGINEERING PROGRAM - PROCESS AND PROCEDURES |
| 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 ARP4418A | Procedure for Sampling and Measurement of Engine and APU Generated Contaminants in Bleed Air Supplies from Aircraft Engines |
| MIL-C-7762 Revision A:1967 | 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-PRF-27210 Revision J:2013 | 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 |
| SAE AS6625A | Spray Equipment, Aircraft Windshield, Anti-Icing |
| MIL-T-81571 Base Document:1967 | THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, 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 |
| MIL-I-7028 Base Document:1950 | INSTRUMENT AND INSTRUMENT BOARDS, AIRCRAFT, INSTALLATION OF |
| MIL-M-3171 Revision C:1966 | MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION |
| 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 Quenched and tempered steel cylinders with tensile strength less than 1100 MPa |
| STANAG 3542 : 2011 | TECHNICAL CRITERIA FOR THE TRANSPORT OF CARGO BY HELICOPTER |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| STANAG 3701 : 0 | AIRCRAFT INTERIOR COLOUR SCHEMES |
| MIL-HDBK-725 Base Document:1972 | ADHESIVES - A GUIDE TO THEIR PROPERTIES AND USES AS DESCRIBED BY FEDERAL AND MILITARY SPECIFICATIONS |
| MIL-A-87229 Base Document:1985 | 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 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| MIL E 21981B:1986 | ELECTRONICS EQUIPMENT, NOMENCLATURE, SERIAL NUMBERS AND IDENTIFICATION PLATES: REQUIREMENTS FOR |
| DEFSTAN 00-14/2(1987) : LATEST | THE USE OF ATLAS IN THE DEFENCE INDUSTRY |
| DEFSTAN 00-3/4(2011) : 2011 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| MIL-T-81259 Revision B:1991 | TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
| MIL-PRF-5425 Revision E:1998 | PLASTIC SHEET, ACRYLIC, HEAT RESISTANT |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL-P-46112 Revision B:1977 | 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 Revision B:1987 | 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 Revision F:1993 | 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 Base Document:1997 | INSTALLATION OF IDENTIFICATION AND MODIFICATION PLATES (FOR AIRCRAFT) |
| MIL-STD-2218 Base Document:1992 | 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 AMSR83283A | Rubber Silicone, High Strength, Cabin Pressure Seal Material, Diaphragm Type |
| MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-DTL-83054 Revision C:2003 | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| AFGS-87139 Revision B:2013 | LANDING GEAR SYSTEMS |
| MIL-C-18244 Revision A:1962 | 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) |
| BS EN 22063:1994 | Metallic and other inorganic coatings. Thermal spraying. Zinc, aluminium and their alloys |
| SAE AS25050B | 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 |
| STANAG 3372 : 2014 | LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
| MIL-M-18012 Revision B:1964 | MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
| MIL-B-8584 Revision C:1970 | BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
| MIL-STD-31000 Revision A:2013 | 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 |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-G-25871 Revision B:1978 | GLASS, LAMINATED, AIRCRAFT GLAZING |
| MIL-I-18259 Base Document:1954 | INSTALLATION OF WINDOW ANTI ICING, DEGREASING AND WASHING SYSTEMS (GENERAL SPECIFICATION FOR) |
| MIL-P-8045 Revision B:1964 | 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 Revision C:1987 | 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 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
| DEFSTAN 81-14/7(2012) : 2012 | CASES, WOOD (BATTEN AND BOARD CONSTRUCTION) |
| MIL-STD-2076 Base Document:1978 | 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 |
| 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 |
| DEFSTAN 91-30/1(1977) : 1977 | LUBRICATING OIL, COLLOIDAL GRAPHITE OX-320 O-218 |
| MIL-A-8869 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS |
| BS EN ISO 9241-1:1997 | Ergonomic requirements for office work with visual display terminals (VDTs) General introduction |
| MIL-PRF-83861 Revision D:2013 | FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| MIL M 8090 : F | MOBILITY, TOWED AEROSPACE GROUND EQUIPMENT, GENERAL REQUIREMENTS FOR |
| MIL-P-5238 Revision C:1974 | 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 AS8804A | Deicing System, Pneumatic Boot, Aircraft, General Specification for |
| 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 |
| MIL-C-25050 Revision A:1963 | COLORS, AERONAUTICAL LIGHTS AND LIGHTING EQUIPMENT, GENERAL REQUIREMENTS FOR |
| DEFSTAN 03-3/5(2011) : 2011 | PROTECTION OF ALUMINIUM ALLOYS BY SPRAYED METAL COATINGS |
| STANAG 3525 : 0 | SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
| MIL-A-9067 Revision C:1961 | ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| STANAG 3639 : 2004 | AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
| BS EN 1803:2002 | Transportable gas cylinders. Periodic inspection and testing of welded carbon steel gas cylinders |
| JSSG-2010 Base Document: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 |
| 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 4324 : 2007 | ELECTROMAGNETIC RADIATION HAZARD ASSESSMENT AND TESTING OF MUNITIONS AND ASSOCIATED SYSTEMS |
| MIL-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-HDBK-2164 Revision A:1996 | 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 |
| MIL-STD-469 Revision B:1996 | INTERFACE STANDARD FOR RADAR ENGINEERING INTERFACE REQUIREMENTS, ELECTROMAGNETIC COMPATIBILITY |
| SAE AS18802 | 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 AS6144A | Sound and Thermal Insulation for Aircraft, General Specification for the Installation of |
| MIL-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-HDBK-723 Revision A:1970 | STEEL AND IRON WROUGHT PRODUCTS |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-T-85075 Revision A:1985 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| DEFSTAN 17-4/3(1986) : 1986 | PICKETING (TIE-DOWN) FITTINGS FOR SHIPBORNE AIRCRAFT (INCLUDING HELICOPTERS) |
| MIL-HDBK-2089 Base Document:1997 | AIRCRAFT SURVIVABILITY TERMS |
| MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
| MIL-HDBK-2173 Base Document:1998 | RELIABILITY-CENTERED MAINTENANCE REQUIREMENTS FOR NAVAL AIRCRAFT, WEAPONS SYSTEMS & SUPPORT EQUIPMENT |
| MIL-G-5485 Revision D:1993 | GLASS; LAMINATED, FLAT, BULLET RESISTANT |
| MIL-HDBK-781 Revision A:1996 | 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 AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| MIL-S-27174 Revision B:1985 | |
| DEFSTAN 00-45(PT1)/3(2012) : 2012 | USING RELIABILITY CENTRED MAINTENANCE TO MANAGE ENGINEERING FAILURES - PART 1: REQUIREMENTS FOR THE APPLICATION OF RELIABILITY CENTRED MAINTENANCE |
| MIL-A-19531 Revision B:1958 | AIRCRAFT, MAINTENANCE AND ENGINEERING INSPECTION REQUIREMENTS |
| MIL-HDBK-253 Base Document:1978 | 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 Revision A:1966 | 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 Base Document:1961 | 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 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL-S-58095 Revision A:1986 | 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 Base Document:2005 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
| SAE ARP1256D | Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-P-6997 Revision B:1953 | 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 Base Document:1985 | SURVIVAL AND FLOTATION SYSTEM, AIRBORNE |
| MIL-L-8937 Revision D:1982 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, [NATO CODE NUMBER S 1738] |
| MIL-E-25499 Revision C:1970 | ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS 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 |
| 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 Base Document:1977 | 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 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| DEFSTAN 16-23/2(1982) : 1982 | FLOOR FITTINGS FOR CARGO TRANSPORT AIRCRAFT APERTURES FOR TIE-DOWN POINTS |
| MIL-STD-417 Revision A:1976 | 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 |
| MIL-E-5627 Revision B:1965 | EXTINGUISHERS, FIRE, CARBON DIOXIDE, PORTABLE |
| MIL-STD-1367 Revision A:1989 | 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 |
| STANAG 3237 : 1997 | APERTURE OF TERMINAL RING OR LINK OF AIRCRAFT LIFTING SLINGS |
| 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 Revision A:1974 | TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| SAE ARP1533C | Procedure for the Analysis and Evaluation of Gaseous Emissions from Aircraft Engines |
| MIL-HDBK-1791 Base Document:1997 | 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 AS1933A | 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 |
| MIL-P-9400 Revision C:1991 | PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
| 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 Revision C:1981 | 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 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-L-18276 Revision C:1964 | LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
| MIL-STD-2074 Base Document:1978 | FAILURE CLASSIFICATION FOR RELIABILITY TESTING |
| 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 Revision A:1987 | WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-PRF-5480 Revision H:2015 | DATA, ENGINEERING AND TECHNICAL: REPRODUCTION |
| MIL-A-25463 Revision B:1982 | 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 Base Document:1985 | INSPECTION, LIQUID PENETRANT |
| MIL-STD-453 Revision C:1984 | INSPECTION, RADIOGRAPHIC |
| MIL-F-7190 Revision B:1985 | FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AMSP83310A | 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) |
| A-A-59124 Base Document:1997 | DECK COVERING, LIGHTWEIGHT, NONSLIP |
| MIL-E-18927 Revision E:1983 | 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 Revision D:2013 | TIE DOWN, CARGO, AIRCRAFT CGU-1/B |
| MIL-STD-2154 Base Document:1982 | 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 ARP5316D | 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 AS8181A | 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 Base Document:2000 | 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 Base Document:1965 | ASBESTOS FELT OR MAT, RESIN IMPREGNATED |
| DEFSTAN 00-971/1(1987) : 1987 | GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
| MIL-E-8593 Revision A:1975 | ENGINE, AIRCRAFT, TURBOPROP, GENERAL SPECIFICATION FOR [ASG] |
| MIL-L-5057 Revision F:1981 | 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 AMSSTD2175 | Castings, Classification and Inspection of |
| MIL-H-18325 Revision B:1959 | HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-722 Base Document:1969 | 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 Base Document:1982 | ADHESIVE BONDED AEROSPACE STRUCTURE REPAIR |
| MIL-I-8651 Revision C:1992 | 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 Base Document:1997 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for |
| SAE AS18259 | Installation of Window Anti-Icing, De-Greasing, and Washing Systems (General Specification For) |
| MIL-F-26301 Revision H:2014 | FLASHER, SOLID STATE, AIRCRAFT NAVIGATIONAL LIGHT, GENERAL SPECIFICATION FOR |
| SAE AS7788 | Panels, Information, Integrally Illuminated |
| MIL-HDBK-1812 Base Document:1997 | TYPE DESIGNATION, ASSIGNMENT AND METHOD FOR OBTAINING |
| MIL-F-17874 Revision B:1965 | FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF |
| DEFSTAN 03-26/2(1988) : 1988 | HARD ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
| MIL-T-5842 Revision B:1985 | 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 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| 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 Revision C:1976 | ANTENNA SUBSYSTEMS FOR AIRBORNE IDENTIFICATION AND NAVIGATION EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-STD-1757 Revision A:1983 | 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 Revision D:1990 | 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 Base Document:1950 | PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER |
| STANAG 3575 : 0 | AIRCRAFT STORES EJECTOR RACKS |
| MIL-L-8552 Revision C:1965 | LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
| MIL-STD-809 Revision B:1986 | ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
| IPC 2221B:2012 | GENERIC STANDARD ON PRINTED BOARD DESIGN |
| MIL-E-5007 Revision D:1973 | 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 Base Document:1951 | Compasses, Pilot\'s Standby, Installation of |
| AFGS-87154 Revision A:1992 | FUEL SYSTEMS, GENERAL DESIGN SPECIFICATION FOR |
| MIL-R-83283 Revision A:1991 | RUBBER, SILICONE, HIGH STRENGTH, CABIN PRESSURE SEAL MATERIAL, DIAPHRAGM TYPE |
| MIL-STD-2124 Revision A:1984 | 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 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL-PRF-32070 Revision A:2012 | TEST PROGRAM SETS |
| DEFSTAN 03-18/5(2012) : 2012 | CHROMATE CONVERSION COATINGS (CHROMATE FILMING TREATMENTS) GRADES: STANDARD AND BRUSHING FOR ALUMINIUM AND ALUMINIUM ALLOYS |
| 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 |
| MIL-L-81174 Revision A:1993 | LIGHT LANDING, AIRCRAFT RETRACTABLE |
| MIL H 5364 : D | HARNESS, SHOULDER SAFETY, GENERAL SPECIFICATION FOR |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-C-8779 Revision E:1988 | COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
| MIL-H-5484 Revision C:1964 | Heater, Aircraft, Combustion Type |
| SAE AS 5778 : 1997 | COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
| MIL-STD-872 Base Document:1966 | 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 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-HDBK-2165 Base Document:1995 | Testability Program for Systems and Equipments |
| MIL-I-83456 Base Document:1974 | 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 AS7413A | Coupling Assemblies, Quick Disconnect, Automatic Shutoff |
| MIL-HDBK-268 Base Document:1982 | SURVIVABILITY ENHANCEMENT, AIRCRAFT CONVENTIONAL WEAPON THREATS, DESIGN & EVALUATION GUIDELINES |
| MIL-STD-783 Revision D:1984 | 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 2G 199:1984 | 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 Revision F:1995 | REEL, SHOULDER HARNESS, INERTIA LOCK |
| MIL-STD-12 Revision D:1981 | 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 Revision D:1992 | COVER, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
| 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 Revision A:1956 | 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 Base Document:1972 | Display, Head-up, General Specification for |
| MIL-HDBK-131 Revision A:1966 | 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 |
| DEFSTAN 03-25/5(2008) : 2008 | SULFURIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
| STANAG 3208 : 2009 | AIR CONDITIONING CONNECTIONS |
| SAE AMSG25871A | Glass, Laminated, Aircraft Glazing |
| MIL-C-8678 Base Document:1984 | COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-STD-1523 Revision A:1984 | AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL |
| 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 |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-STD-471 Revision A:1973 | 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 Revision C:1977 | Tests, Impact, Shock Absorber Landing Gear, Aircraft |
| BS ISO 461-1:2003 | Aircraft. Connectors for ground electrical supplies Design, performance and test requirements |
| STANAG 3198 : 2017 | FUNCTIONAL REQUIREMENTS OF AIRCRAFT OXYGEN EQUIPMENT AND PRESSURE SUITS |
| MIL-A-21180 Revision D:1984 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL PRF 5041 : K | TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| SAE AS5604A | Compass; Magnetic, Pilot\'s Standby |
| BS 4G 173-1:1985 | Connectors for ground electrical supplies for aircraft Specification for design, performance and test requirements |
| MIL STD 1288 : NOTICE 4 | AIRCREW PROTECTION REQUIREMENTS NONNUCLEAR WEAPONS THREAT |
| STANAG 3766 : 2017 | GREASE NIPPLES |
| MIL-R-6130 Revision C:1980 | RUBBER, CELLULAR, CHEMICALLY BROWN |
| 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 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| 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 Base Document:1981 | AIRCRAFT NONNUCLEAR SURVIVABILITY TERMS |
| MIL-STD-250 Revision D:1974 | 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 AS18012 | 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 Base Document:1962 | 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 AS35411C | Fittings, Lubrication |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-S-8512 Revision D:1974 | 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 Revision C:1964 | RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE |
| MIL-D-18300 Revision H:1993 | DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
| SAE AS50881F | 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 Revision D:1969 | ARRESTER, LIGHTNING, GENERAL SPECIFICATION FOR |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-PRF-25690 Revision B:1993 | PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
| DEFSTAN 05-10(PT0)/6(2013) : 2013 | PRODUCT DEFINITION INFORMATION - PART 0: GENERAL INTRODUCTION TO PRODUCT DEFINITION INFORMATION |
| BS 2G 219:1983 | Specification for general requirements for ground support electrical supplies for aircraft |
| MIL-M-8650 Revision C:1976 | Mockups, Aircraft, General Specification for |
| 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 Base Document:1949 | TRANSMISSION, POWER, CONSTANT RATIO, GENERAL SPECIFICATION [AIRCRAFT USE] |
| MIL-STD-1366 Revision E:2006 | INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
| MIL-S-81771 Revision A:1975 | 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] |
| MIL-W-6729 Revision C:1993 | WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-490 Revision A:1985 | SPECIFICATION PRACTICES |
| 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 AMSF7190B | Forging, Steel, For Aircraft/Aerospace Equipment and Special Ordnance Applications |
| MIL-Q-9858 Revision A:1963 | QUALITY PROGRAM REQUIREMENTS |
| BS 2G 135:1967 | Specification for electrically-heated pitot and pitotstatic pressure heads |
| MIL-HDBK-838 Base Document:1997 | 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 Revision C:1980 | CASTINGS, PRECISION, NONFERROUS |
| MIL B 81757 : C | BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-C-7413 Revision B:1970 | 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 Base Document:1997 | 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 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| MIL-STD-805 Revision B:1987 | 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 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 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| MIL-D-8708 Revision C:1991 | 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 |
| MIL-H-46855 Revision B:1979 | 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 |
| 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 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| MIL-T-18606 Base Document:1955 | 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 |
| ASTM D 1322 : 2015-06 | TEST METHOD FOR SMOKE POINT OF KEROSINE AND AVIATION TURBINE FUEL |
| MIL-STD-2164 Base Document:1985 | ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
| MIL L 6484 : C | LIGHT, COCKPIT UTILITY, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-F-83860-1 Revision A:1977 | FILTER ELEMENT, FLUID PRESSURE, HYDRAULIC, AIRCRAFT, DISPOSABLE, 5 MICRON ABSOLUTE |
| STANAG 3576 : 2016 | ELECTRICAL CONNECTOR FOR DISPENSERS AND INTERNAL INTERVALOMETER TYPE ROCKET LAUNCHERS FOR AIRCRAFT |
| MIL-S-7470 Revision A:1975 | 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 Base Document:1978 | FASTENING DEVICES PREFERRED FOR DESIGN, LISTING OF |
| MIL-PRF-38214 Revision 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 Revision A:1994 | 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 Revision D:2004 | MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
| MIL-HDBK-691 Revision B:1987 | 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 Revision A:1992 | INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
| MIL-P-83310 Base Document:1971 | PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
| MIL-R-23761 Revision B:1975 | 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 Base Document:1979 | LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-STD-22 Revision D:1979 | 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 Base Document:1954 | ANTI-ICING EQUIPMENT FOR AIRCRAFT HEATED SURFACE TYPE, GENERAL SPECIFICATION FOR |
| STANAG 3105 : 2014 | PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
| MIL-STD-331 Revision D:2017 | FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
| MIL-H-8501 Revision A:1961 | 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 Revision A:1953 | 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 Revision F:2014 | TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
| MIL-L-25467 Revision D:1977 | LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
| 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 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 Revision B:1968 | 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 Revision C:2014 | 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 Base Document:1967 | ENGINE AND RELATED PROPULSION AND POWER EQUIPMENT, AIRCRAFT, ACCEPTANCE TESTS OF, SAMPLING PLAN FOR, STATISTICAL |
| MIL-HDBK-2069 Base Document:1997 | AIRCRAFT SURVIVABILITY |
| MIL-STD-2173 Base Document:1986 | 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 |
| MIL-L-16462 Revision B:1960 | LITTER, FOLDING, RIGID POLE |
| STANAG 3329 : 0 | NUMERALS AND LETTERS IN AIRCREW STATIONS |
| SAE AS8045A | Minimum Performance Standard for Underwater Locating Devices (Acoustic) (Self-Powered) |
| MIL-S-416 Revision D:1979 | STRAINER, WELL, WATER, WIRE WOUND |
| MIL-DTL-9129 Revision G:2014 | Discharges, 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 AS6254A | Minimum Performance Standard for Low Frequency Underwater Locating Devices (Acoustic) (Self-Powered) |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| DEFSTAN 61-1 : LATEST | MOTORS, ELECTRIC |
| MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-S-8698 Base Document:1954 | 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-HDBK-274 Revision A:2011 | 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 Revision A:1984 | 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 Revision C:1970 | 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 |
| MIL R 81589 : NOTICE 1 | RAIN REPELLENT FLUID APPLICATION SYSTEM AIRCRAFT WINDSHIELD |
| MIL-DTL-83413 Revision C:2012 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-P-87210 Base Document:1984 | 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 Revision D:1974 | BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
| MIL-S-6144 Revision A:1966 | SOUND AND THERMAL INSULATION FOR AIRCRAFT GENERAL SPECIFICATION FOR THE INSTALLATION OF |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| DEFSTAN 53-70/2(1976) : 1976 AMD 2 | DIMENSIONS OF ELASTOMERIC TOROIDAL SEALING RINGS (INCH SERIES) FOR AIRCRAFT PURPOSES |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| BS EN 10203:1991 | Specification for cold reduced electrolytic tinplate |
| MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| DEFSTAN 80-15/2(1990) : 1990 | PAINT, PRE-TREATMENT PRIMER (ETCHING PRIMER) - TYPES: BRUSHING (BASE AND ACID COMPONENT), SPRAYING (BASE AND ACID COMPONENT) |
| SAE AMS M 3171 : 1998 | MAGNESIUM ALLOY, PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION ON |
| MIL-S-6904 Revision B:1965 | 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 Revision A:1987 | 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 Revision B:1987 | 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 |
| MIL-PRF-46010 Revision H:2013 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
| MIL-STD-705 Revision D:2016 | 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 Revision D:2013 | SYSTEMS, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
| MIL-HDBK-2084 Base Document:1995 | 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 <i>R</i><sub>m</sub> value of less than 1 100 MPa |
| MIL-M-13231 Revision C:1988 | MARKING OF ELECTRONIC ITEMS |
| BS EN 60893-2:2004 | Insulating materials. Industrial rigid laminated sheets based on thermosetting resins for electrical purposes Methods of test |
| DEFSTAN 03-20/3(2005) : 2005 | ELECTRO-DEPOSITION OF ZINC |
| DEFSTAN 03-19/4(2010) : 2010 | ELECTRO-DEPOSITION OF CADMIUM |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
| MIL-HDBK-17-2 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 2: POLYMER MATRIX COMPOSITES MATERIALS PROPERTIES |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
| MIL-STD-765 Revision A:1967 | COMPASS SWINGING, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| DEFSTAN 91-19/1(1973) : 1973 | LUBRICANT, SOLID FILM; HEAT CURED NATO CODE NO; S-1738 JOINT SERVICE DESIGNATION; ZX-34 |
| DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984 | V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC) |
| DEFSTAN 91-101/3(2001) : 2001 AMD 1 2002 | LUBRICATING OIL, GAS TURBINE ENGINE, SYNTHETIC GRADE 5 CST NATO CODE: O-156 JOINT SERVICE DESIGNATION: OX-27 AND OX-28 |
| DEFSTAN 17-5/2(1986) : 1986 | POWER DRIVEN HYDRAULIC GROUND SERVICING EQUIPMENT FOR AIRCRAFT |
| MIL T 31000 : 0 | TECHNICAL DATA PACKAGES - GENERAL SPECIFICATION FOR |
| MIL-C-104 Revision C:1992 | CRATES, WOOD: LUMBER AND PLYWOOD SHEATHED, NAILED, AND BOLTED |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
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