DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
Superseded date
26-07-2022
Superseded by
Published date
26-01-2016
Publisher
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| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015). (01/2016)
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| 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Superseded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 00-003/5(2016) : 2016 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| DEFSTAN 00-003/6(2017) : 2017 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| ISO 2631:1978 | Guide for the evaluation of human exposure to whole-body vibration |
| STANAG 3370 : 2004 | AIRCREW STATION ALERTING SYSTEMS |
| DEFSTAN 17-3/1(1972) : 1972 | ADAPTORS, AIRCRAFT JACKING POINTS (DETACHABLE JACKING PADS) |
| DTD 925 D : JUL 69 | THE FABRICATION OF ACRYLIC PANELS AND SHAPINGS |
| STANAG 3217 : 2006 | OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
| BS G 230:1984 | Specification for general requirements for aircraft electrical cables (second series) |
| STANAG 3341 : 72 AMD 6 | EMERGENCY CONTROL COLOUR SCHEMES |
| DEFSTAN 17-1/2(1984) : 1984 | AIRCRAFT LIFTING SLINGS, APERTURE OF TERMINAL RING OR LINK |
| BS G 175:1959 | Aircraft fuel nozzle grounding plugs and sockets |
| DTD 5577 : NOV 65 | HEAT STABLE STRUCTURAL ADHESIVES |
| STANAG 3659 : 2002 | ELECTRICAL BONDING REQUIREMENTS FOR METALLIC AIRCRAFT SYSTEMS |
| FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
| MIL-E-22285 Base Document:1959 | EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| DEFSTAN 59-113/2(2012) : 2012 | LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT |
| DTD 775 : A | ADHESIVE SUITABLE FOR JOINING METALS |
| MIL-P-46111 Revision C:1978 | PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
| BS C 6:1966 | Specification for aircraft engine nacelle fire extinguisher doors |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| DEFSTAN 05-18/5(2007) : 2007 | SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS |
| MIL-C-7762 Revision A:1967 | COMPASS, INSTALLATION OF |
| STANAG 3294 : 0 | AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
| SAE J 1013 : 1992 | MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES |
| MIL O 27210 : F | OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
| DEFSTAN 05-19/1(1972) : 1972 | LIMITS AND FITS FOR ENGINEERING |
| DEFSTAN 53-9/1 : LATEST | BOLTS, MACHINE SCREWS, AND NUTS FOR AEROSPACE VEHICLES |
| MIL-HDBK-725 Base Document:1972 | ADHESIVES - A GUIDE TO THEIR PROPERTIES AND USES AS DESCRIBED BY FEDERAL AND MILITARY SPECIFICATIONS |
| DEFSTAN 17-10/2(1984) : 1984 | TOWING ATTACHMENTS AND TOWING/STEERING EQUIPMENT FOR AIRCRAFT |
| SAE AS 401 : 1993 | POWERPLANT FIRE DETECTION INSTRUMENTS - THERMAL AND FLAME CONTACT TYPES (RECIPROCATING ENGINE POWERED AIRCRAFT) |
| STANAG 3278 : 2014 | AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| DEFSTAN 49-2/2(1975) : 1975 AMD 3 | LUBRICATING GUNS, HAND AND GUNS, FLUID, DIRECT DELIVERY |
| DEFSTAN 00-29/1(1982) : 1982 | FUNGAL CONTAMINATION AFFECTING THE DESIGN OF MILITARY MATERIAL |
| DEFSTAN 05-34/2(1984) : 1984 | MARKING OF SERVICE MATERIAL |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| DEFSTAN 05-21/1(1973) : 1973 | QUALITY CONTROL SYSTEM REQUIREMENTS FOR INDUSTRY |
| DEFSTAN 03-24/5(2008) : 2008 | CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
| DEFSTAN 53-88/1(1979) : 1979 | WASHERS, LOCK, KEY (TAB) AND SPRING TENSION (CRINKLE), INCH SERIES, FOR AEROSPACE APPLICATIONS |
| STANAG 3218 : 86 AMD 2 | LOCATION, ACTUATION AND SHAPE OF ENGINE CONTROLS AND SWITCHES |
| MIL-A-9067 Revision C:1961 | ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR |
| STANAG 3639 : 2004 | AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
| DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991 | PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS |
| DEFSTAN 05-61(PT12)/1(1987) : 1987 | QUALITY ASSURANCE PROCEDURAL REQUIREMENTS - PART 12: CONTROL OF WALL THICKNESS IN DESIGN AND MANUFACTURE OF FLYING CONTROL SYSTEMS |
| MIL-S-58095 Revision A:1986 | SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
| BS SP 90:1961 | Specification for corrosion-resisting steel split cotter pins for aircraft |
| BS G 212:1971 | Specification for general requirements for aircraft electrical cables |
| MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
| DTD 761C : DEC 65 | SAFETY GLASS WINDSCREEN, WEAPON SIGHTING QUALITY |
| STANAG 3216 : 84 AMD 4 | LAYOUT OF FLIGHT DATA IN PILOTS DISPLAYS |
| FAA AC 20-100 : 1977 | GENERAL GUIDELINES FOR MEASURING FIRE-EXTINGUISHING AGENT CONCENTRATIONS IN POWERPLANT COMPARTMENTS |
| DTD 5548 : AMD 1 | GLAZING COMPOUNDS |
| DTD 5627 : APR 82 | FIBROUS POLYAMIDE MATERIAL FOR USE AS AN EXPLOSION SUPPRESSANT AND AS A BAFFLE MATERIAL IN AIRCRAFT FUEL TANKS |
| MIL-W-81752 Revision A:1987 | WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
| ASTM D 1781 : 1998 | Standard Test Method for Climbing Drum Peel for Adhesives |
| DTD 5624 : MAR 81 | FIBROUS POLYESTER MATERIAL FOR USE AS A FLAME AND FIRE SUPPRESSANT IN AIRCRAFT DRY BAYS |
| MIL-A-25463 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 |
| DTD 861A : DEC 59 | ADHESIVE FOR METAL (LOW PRESSURE TYPE) |
| ASTM D 3983 : 1998 | Standard Test Method for Measuring Strength and Shear Modulus of Nonrigid Adhesives by the Thick-Adherend Tensile-Lap Specimen |
| DEFSTAN 53-1/3(1981) : 1981 AMD 1 1984 | USE OF UNIFIED SCREW THREADS |
| DTD 218D : SEP 66 | LAMINATED SAFETY GLASS |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| EN 2243-2:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 2: Peel metal-metal |
| EN 2243-1:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 1: Single lap shear |
| STANAG 3611 : 73 AMD 4 | CHARACTERISTICS OF COMPRESSED BREATHING AIR FOR AIRCRAFT USE |
| STANAG 3593 : 1997 | NUMBERING OF ENGINES AND THEIR ASSOCIATED CONTROLS AND DISPLAYS IN AIRCRAFT |
| MIL P 8184 : E | PLASTIC SHEET, ACRYLIC, MODIFIED |
| MIL-P-6992 Base Document:1950 | PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER |
| STANAG 3224 : 2005 | AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
| DEFSTAN 07-55(PT2)SEC4/1(1975) : 1975 AMD 3 1983 | ENVIRONMENTAL TESTING OF SERVICE MATERIAL - PART 2: TESTS - SECTION 4: PENETRATION AND IMMERSION |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| STANAG 3221 : 77 AMD 7 | AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) IN AIRCRAFT DESIGN STANDARDS AND LOCATION OF CONTROLS |
| MIL-H-5484 Revision C:1964 | Heater, Aircraft, Combustion Type |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| BS 5423:1987 | Specification for portable fire extinguishers |
| DEFSTAN 95-7/2(2004) : 2004 | WIRE FOR LOCKING PURPOSES AND WIRE LOCKING PRACTICE FOR AEROSPACE USE |
| DEFSTAN 03-2/6(2011) : 2011 | CLEANING AND PREPARATION OF METAL SURFACES |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| STANAG 3208 : 2009 | AIR CONDITIONING CONNECTIONS |
| DEFSTAN 16-24/1(1983) : 1983 | SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
| STANAG 3766 : 2017 | GREASE NIPPLES |
| MIL-F-23447 Base Document:1962 | FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
| BS C 15:1960 | Specification for coupling dimensions for aircraft-to-tractor tow bar connections |
| ASTM E 229 : 1997 | Standard Test Method for Shear Strength and Shear Modulus of Structural Adhesives (Withdrawn 2003) |
| PREN 2101 : 1987 | CHROMIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS |
| EN 2243-4:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| DTD 5625 : JUN 80 | STANDARD ANNEALED FLOAT GLASS FOR AIRCRAFT GLAZING |
| STANAG 3359 : 85 AMD 4 | LOCATION AND ARRANGEMENT OF ENGINE DISPLAYS IN AIRCRAFT |
| BS 6F 100:1998 | Procedure for inspection and testing of textiles for aerospace purposes |
| DTD 5576A : JAN 66 | LAMINATED SAFETY GLASS HEATED BY ELECTRICALLY CONDUCTING FILM(S) |
| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| MIL-T-18606 Base Document:1955 | TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
| STANAG 3258 : 0 | POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
| PD 6484:1979 | Commentary on corrosion at bimetallic contacts and its alleviation |
| STANAG 3219 : 0 | LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
| DTD 5592 : LATEST | ACRYLIC SHEETS FOR AIRCRAFT GLAZING |
| DEFSTAN 16-17/2(1983) : 1983 | AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
| MIL-HDBK-691 Revision B:1987 | Adhesive Bonding |
| MIL-P-83310 Base Document:1971 | PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
| STANAG 3436 : 0 | COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
| DEFSTAN 91-48/2(1997) : 1997 | HYDRAULIC FLUID, PETROLEUM: SUPERCLEAN NATO CODE: H-515 JOINT SERVICE DESIGNATION: OM-15 HYDRAULIC FLUID, PETROLEUM: NORMAL NATO CODE: H-520 JOINT SERVICE DESIGNATION: OM-18 |
| MIL-I-8670 Revision B:1993 | INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
| STANAG 3225 : 75 AMD 7 | LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS FOR ROTARY WING AIRCRAFT |
| EN 2243-3:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb core |
| DEFSTAN 00-50/1(1982) : 1982 | GUIDE TO CHEMICAL ENVIRONMENTAL CONTAMINANTS AND CORROSION AFFECTING THE DESIGN OF MILITARY MATERIAL |
| BS 2C 12:1980 | Specification for jacking pads for aircraft |
| MIL-STD-1294 Revision A:1985 | ACOUSTICAL NOISE LIMITS IN HELICOPTERS |
| MIL-T-23103 Revision A:1971 | THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| DTD 869A : NOV 57 | LAMINATED SAFETY GLASS, HIGH LIGHT TRANSMISSION |
| SAEITC TS120-6 | TS120 AGS2000 Series Stiffnuts (including Clinch Nuts) BA and BSF Threads for Aircraft |
| SAE ARP 1524 : 2013 | SURFACE PREPARATION AND PRIMING OF ALUMINUM ALLOY PARTS FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
| MIL-HDBK-221 Base Document:1965 | FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
| DEFSTAN 61-12(PT20)/1(1980) : 1980 | WIRES, CORDS, AND CABLES, ELECTRICAL - METRIC UNITS - PART 20: BRAIDS, WIRE |
| STANAG 3950 : 0 | HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
| STANAG 3209 : 2014 | TYRE VALVE COUPLINGS |
| DTD 5626 : JUN 80 | HIGH LIGHT TRANSMISSION ANNEALED PLATE GLASS FOR AIRCRAFT GLAZING |
| STANAG 3622 : 73 AMD 7 | EXTERNAL VISION FROM AIRCREW STATIONS |
| DEFSTAN 25-7/1(1968) : 1968 AMD 1 | HORNS, ELECTRICAL |
| BS C 10:1958 | Coupling dimensions for aircraft ground air-conditioning connections |
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