DEFSTAN 00-970(PT0)/17(2016) : 2016
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Superseded date
28-09-2017
Superseded by
Published date
24-01-2017
Publisher
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Preface
Section One - General
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
Gives guidance and content information, together with definitions of the terms used throughout this document.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT0)/16(2015). (01/2017)
|
| DocumentType |
Standard
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| PublisherName |
UK Ministry of Defence Standards
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| DEFSTAN 00-003/6(2017) : 2017 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| BS 381C:1996 | Specification for colours for identification, coding and special purposes |
| 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 |
| BS EN 10202:2001 | Cold reduced tinmill products. Electrolytic tinplate and electrolytic chromium/chromium oxide coated steel |
| SAE AMSI7171A | Insulation Blanket, Thermal-Acoustical |
| BS 6221-20:1984 | Printed wiring boards Guide for the assembly of printed wiring boards |
| MIL-A-8865 Revision B:1987 | 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 Revision C:2008 | 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 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 |
| 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 |
| MIL-HDBK-505 Base Document:1998 | 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 |
| 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 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 |
| DEFSTAN 05-61/1(1983) : 1983 | QUALITY ASSURANCE PROCEDURAL REQUIREMENTS |
| 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 |
| DEFSTAN 03-5/3(1995) : 1995 | AUTOCATALYTIC (ELECTROLESS) NICKEL COATING OF METALS |
| 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 |
| TIA/EIA 422 : B1994(R2014) | ELECTRICAL CHARACTERISTICS OF BALANCED VOLTAGE DIGITAL INTERFACE CIRCUITS |
| SAE ARP1179D | 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 Revision C:1980 | 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 Revision A:1973 | AUDIO EQUIPMENT |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| STANAG 3153 : 0 | AIRCRAFT NAVIGATION AND ANTI-COLLISION LIGHTS |
| MIL-STD-130 Revision N:2007 | 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 3659 : 2002 | ELECTRICAL BONDING REQUIREMENTS FOR METALLIC AIRCRAFT SYSTEMS |
| 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-E-22285 Base Document:1959 | EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
| AECTP-400 : 2006 | MECHANICAL ENVIRONMENTAL TESTS |
| SAE J1966_201108 | 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 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| MIL-P-46111 Revision C:1978 | 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) |
| AECTP-250 : 2014 | ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
| AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| DEFSTAN 03-14/4(2008) : 2008 | ELECTRODEPOSITION OF CHROMIUM FOR ENGINEERING PURPOSES |
| 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 |
| 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 ARP4418A | 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 Revision J:2013 | 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 ARP8615 | 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 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 Base Document:1972 | 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 Base Document:1985 | AUXILIARY POWER SYSTEMS, AIRBORNE |
| 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 |
| DEFSTAN 00-3/4(2011) : 2011 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| BS EN ISO 4618:2014 | Paints and varnishes. Terms and definitions |
| 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 |
| 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 |
| MIL-T-7743 Revision F:1993 | TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-STD-8651 Base Document:1997 | 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 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 | |
| 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-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 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 AS25050B | 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 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 |
| MIL-B-81365 Base Document:1966 | 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 Revision B:2004 | AIR SYSTEM |
| 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 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 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-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 | 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 Base Document:1998 | Crew Systems |
| BS 2C 7:1984 | Specification for aircraft tyre valves: interchangeability dimensions |
| 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 |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
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| SAE AS6144A | 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 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| 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-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-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 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
| 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 |
| BS 5852:2006 | Methods of test for assessment of the ignitability of upholstered seating by smouldering and flaming ignition sources |
| MIL-DTL-6162 Revision C:2000 | 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 Revision C:2016 | 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 Base Document:1985 | EDDY CURRENT TESTING |
| 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 |
| AECTP-600 : 2007 | THE TEN STEP METHOD FOR EVALUATING THE ABILITY OF MATERIEL TO MEET EXTENDED LIFE REQUIREMENTS AND ROLE AND DEPLOYMENT CHANGES |
| 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-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 |
| 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 Revision A:1987 | 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 ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING 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 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) |
| 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 |
| 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 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 |
| 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 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 3499 : 0 | CHARACTERISTICS OF SUPPLY EQUIPMENT FOR LIQUID OXYGEN |
| AECTP-240 : 2009 | MECHANICAL CONDITIONS |
| MIL-HDBK-337 Base Document:1982 | 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 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-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 |
| 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 Base Document:1983 | SURVIVABILITY, AIRCRAFT, NONNUCLEAR, AIRFRAME - VOLUME 2 |
| 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] |
| 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 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 |
| 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 Revision B:2004 | Air Vehicle |
| 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 |
| MIL-L-81174 Revision A:1993 | LIGHT LANDING, AIRCRAFT RETRACTABLE |
| 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 |
| 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 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 |
| 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 |
| 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 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-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 Revision A:1956 | FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT |
| DEFSTAN 61-10/4(1984) : 1984 | GENERATOR SETS (GROUND, ENGINE DRIVEN) |
| MIL-HDBK-728-3 Base Document:1985 | 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 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 |
| 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 Base Document:1985 | 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 Revision C:1987 | 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 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 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| SAE AS5604A | 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 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 |
| 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 AS18012 | 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 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-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 |
| SAE AS50881F | Wiring Aerospace Vehicle |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| 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 00-55(PT1)/3(2014) : 2014 | REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| ASTM A 148/A148M : 2015-09 | SPECIFICATION FOR STEEL CASTINGS, HIGH STRENGTH, FOR STRUCTURAL PURPOSES |
| 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 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-STD-1366 Revision E:2006 | INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
| MIL-W-6729 Revision C:1993 | 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 Base Document:1985 | NONDESTRUCTIVE TESTING |
| SAE AMSF7190B | 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 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 |
| BS ISO 3324-1:2013 | Aircraft tyres and rims 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 Base Document:1997 | DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
| MIL-P-15024-5 Base Document:1971 | 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 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-HDBK-728-5 Revision A:1994 | RADIOGRAPHIC TESTING - VOLUME 5 |
| 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 |
| 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 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 |
| 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 |
| 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 |
| 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 |
| DEFSTAN 16-17/2(1983) : 1983 | AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
| MIL-STD-1285 Revision D:2004 | MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
| MIL-HDBK-691 Revision B:1987 | Adhesive Bonding |
| MIL-HDBK-336-1 Base Document:1982 | 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 Revision D:1979 | 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 Revision D:2017 | 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 Revision F:2014 | TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
| MIL-L-25467 Revision D:1977 | LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-336-3 Base Document:1983 | 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 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-HDBK-2069 Base Document:1997 | AIRCRAFT SURVIVABILITY |
| MIL D 1000/1 : LATEST | DRAWING, ENGINEERING & ASSOCIATED DATA |
| 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 |
| 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) |
| 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 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| 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 |
| 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 Revision C:2012 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
| AECTP-230 : 2009 | CLIMATIC CONDITIONS |
| DEFSTAN 00-35/2(1996) : 1996 AMD 1 1997 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| BS EN 10203:1991 | Specification for 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 Base Document:1965 | 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 |
| 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 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 |
| 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 |
| 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 |
| 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 |
| 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-81774 Revision A: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 |
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