DEFSTAN 00-970(PT7)SEC2/SUPP6/6(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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
Superseded date
26-07-2022
Superseded by
Published date
26-02-2016
Publisher
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| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015). (02/2016)
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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Superseded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 |
| DEFSTAN 47-25/1(1982) : 1982 | PIPELINES AND PIPE COUPLINGS FOR AIRCRAFT FLUID SYSTEMS (METRIC) |
| SAE AIR 4015 : 2013 | ICING TECHNOLOGY BIBLIOGRAPHY |
| BS C 18:1976 | Specification for V-flange couplings for aircraft piping and ducting - metric series |
| DEFSTAN 59-100(PT2)/1(1981) : 1981 | FUSEHOLDERS; CARRIERS, CARTRIDGE FUSE LINK AND WIRE FUSE ELEMENT; AND BASES ELECTRICAL FUSE - PART 2: LISTS |
| STANAG 3456 : 0 | AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
| DEFSTAN 59-100(PT1)/3(1995) : 1995 | FUSE-HOLDERS, CARRIERS AND BASES ELECTRICAL FUSE (BLOCK AND EXTRACTOR POST TYPES) - PART 1: SPECIFICATIONS |
| BS 2G 143:1965 | Specification for a.c. and d.c. rotary and linear actuators for aircraft |
| DEFSTAN 62-10(PT2)/1(1974) : 1974 | MARKINGS OF LAMPS, ELECTRIC AND THEIR PACKAGES |
| BS 2G 134:1970 | Specification for d.c. generators |
| DEFSTAN 16-26/1(1983) : 1983 | CHARGING VALVES FOR AIRCRAFT HIGH PRESSURE NITROGEN AND HYDRAULIC FLUID SYSTEMS |
| STANAG 3153 : 0 | AIRCRAFT NAVIGATION AND ANTI-COLLISION LIGHTS |
| DEFSTAN 81-24/5(2004) : 2004 | IDENTIFICATION MARKING OF TRANSPORTABLE CONTAINERS, COMPRESSED GAS |
| BS M 55:1984 | Method for rotary flexure testing of hydraulic tubing joints and fittings for aerospace use |
| DEFSTAN 00-10/3(1986) : 1986 AMD 2 1993 | GENERAL DESIGN AND MANUFACTURING REQUIREMENTS FOR SERVICE ELECTRONIC EQUIPMENT |
| BS 5M 23:1987 | Specification for an identification scheme for pipelines |
| 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 |
| BS M 51:1982 | Classification for pressure and temperature for fluid systems and components |
| DEFSTAN 59-97/3(1990) : AMD 1 | HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL |
| 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 59-76/1(1981) : 1981 | TRANSFORMERS AND INDUCTORS - GENERAL REQUIREMENTS FOR THE PROCUREMENT OF TRANSFORMERS AND INDUCTORS - CAPABILITY APPROVAL |
| DTD 933A : FEB 64 | GLASS FABRIC REINFORCED POLYESTER LAMINATES FOR AIRCRAFT STRUCTURES AND AIRBORNE RADOMES |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| DTD 856A : LATEST | EXTERNAL FINISHES FOR RADOMES |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| DEFSTAN 05-123/1(1983) : 1983 | TECHNICAL PROCEDURES FOR THE PROCUREMENT OF AIRCRAFT, WEAPON AND ELECTRONIC SYSTEMS |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| 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 |
| BS 5G 178-1:1993 | Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools |
| DEFSTAN 59-71/1(1988) : 1988 AMD 1 1990 | CRIMPED ELECTRICAL CONNECTIONS FOR COPPER CONDUCTORS - GENERIC SPECIFICATION |
| DEFSTAN 05-56/1(1980) : 1980 | GRAPHICAL SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC 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 |
| BS M 24:1955 | Graphical symbols for aircraft hydraulic and pneumatic systems |
| BS G 229:1982 | Schedule for environmental conditions and test procedures for airborne equipment |
| BS M 52:1983 | Method for impulse testing of hydraulic hose, tubing and fittings assemblies for aerospace fluid systems |
| DEFSTAN 59-35(PT0)/3(1990) : 1990 | CONNECTORS ELECTRICAL - PART 0: GUIDE TO CONNECTORS ELECTRICAL, DIRECT CURRENT, LOW FREQUENCY AND RADIO FREQUENCY APPLICATIONS |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| BS 2G 127:1967 | Specification for power and current transformers for use in aircraft electrical power supply systems |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| BS M 53:1983 | Method for thermal shock testing of pipes and fittings for aerospace fluid systems |
| DEFSTAN 47-12/4(1987) : 1987 | POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES (WIRE REINFORCED) FOR MEDIUM AND HIGH PRESSURE FLUID SYSTEMS IN AIRCRAFT |
| ISO 7169:2014 | Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric |
| DEFSTAN 00-971/1(1987) : 1987 | GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
| DEFSTAN 59-71(PT2)/1(1993) : 1993 | CRIMPED ELECTRICAL CONNECTORS FOR COPPER CONDUCTORS - PART 2: SPECIALISED CRIMPING PROCESSES |
| DEFSTAN 59-4(PT7)/1(1969) : 1969 | PLUGS AND SOCKETS, ELECTRICAL - PART 7: ORIENTATION AND CONTACT ALLOCATIONS RESERVED FOR POWER SUPPLIES |
| BS M 48:1975 | Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
| DEFSTAN 16-21/2(1986) : 1986 AMD 1 1986 | MARKING OF AIRCRAFT HYDRAULIC COMPONENTS |
| 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 |
| DEFSTAN 66-7(PT1)/3(1983) : 1983 AMD 1 1985 | INSTRUMENTS, ELECTRICAL INDICATING (SEALED) 50 MM TO 100 MM - PART 1: SPECIFICATION |
| BS M 60:1986 | Specification for separable tube fittings for fluid systems |
| DTD 926B : SEP 63 | PROCESS FOR THE EXTERNAL FINISHING OF RADOMES |
| BS 2G 146:1966 | Specification for d.c. motors for aircraft |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| BS 2G 199:1984 | Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration |
| BS 6275-1:1982 | Hydraulic fluid power filter elements Method of evaluating filtration performance (multi-pass method) |
| MIL-STD-12 Revision D:1981 | ABBREVIATIONS FOR USE ON DRAWINGS, SPECIFICATIONS FOR STANDARDS AND IN TECHNICAL DOCUMENTS |
| DEFSTAN 59-36/5(1995) : 1995 | SELECTION OF ELECTRONIC AND ELECTRICAL COMPONENTS FOR USE IN DEFENCE EQUIPMENT |
| BS C 13:1960 | Sizes of gravity filling orifices on aircraft |
| DEFSTAN 61-10/4(1984) : 1984 | GENERATOR SETS (GROUND, ENGINE DRIVEN) |
| DEFSTAN 00-41(PT1)/2(1989) : 1989 | MOD PRACTICES AND PROCEDURES FOR RELIABILITY AND MAINTAINABILITY - PART 1: RELIABILITY DESIGN PHILOSOPHY |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| DEFSTAN 59-96(PT2)/1(1980) : 1980 | FUSES, ELECTRICAL - PART 2: FUSE LINKS, ELECTRICAL LISTS |
| STANAG 3632 : 0 | AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| DEFSTAN 16-6/2(1991) : 1991 | CHARGING VALVE FOR AIRCRAFT LIQUID SPRING UNDERCARRIAGE UNITS |
| DEFSTAN 59-42/2(1987) : LATEST | HEAT SHRINK SOLDER SHEATHS, GENERAL REQUIREMENTS AND TEST METHODS FOR CAPABILITY APPROVAL |
| BS C 9:1970 | Specification for coupling dimensions for high pressure air charging valves for aircraft |
| DEFSTAN 61-3/5(1992) : INTERIM | GENERIC SPECIFICATION FOR BATTERIES, NON RECHARGEABLE, PRIMARY |
| 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-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| DEFSTAN 47-22/1(1979) : 1979 | END FITTINGS FOR FLEXIBLE HOSE ASSEMBLIES FOR AIRCRAFT - METRIC |
| BS G 174:1959 | Invertors for secondary electrical supplies for aircraft |
| DEFSTAN 61-6/3(1989) : 1989 | AIRCRAFT ELECTRICAL CIRCUIT IDENTIFICATION |
| STANAG 3329 : 0 | NUMERALS AND LETTERS IN AIRCREW STATIONS |
| BS G 102:1971 | Specification for general requirements for rotating electrical machinery |
| 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-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 62-10(PT1)/1(1974) : 1974 | LAMPS, FILAMENT |
| DEFSTAN 59-96(PT1)/2(1995) : 1995 | FUSE-LINKS ELECTRICAL - PART 1: SPECIFICATIONS |
| BS G 142:1953 | Specification for heavy duty, electro-magnetically operated, single-pole circuit-breakers for extra-low voltage d.c. systems in aircraft |
| DEFSTAN 00-35/2(1996) : 1996 AMD 1 1997 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL |
| DEFSTAN 16-7/3(1990) : 1990 | COMPRESSED AIR, CHARACTERISTICS, SUPPLY, PRESSURE AND HOSES FOR TECHNICAL PURPOSES |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
| DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984 | V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC) |
| DEFSTAN 59-56(PT2)/1(1976) : 1976 AMD 1 | PLUGS AND SOCKETS, ELECTRICAL - PATTERN 602 ITEMS NO LONGER TO BE PROVISIONED |
| DEFSTAN 17-5/2(1986) : 1986 | POWER DRIVEN HYDRAULIC GROUND SERVICING EQUIPMENT FOR AIRCRAFT |
| ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
| DEFSTAN 66-7(PT2)/1(1971) : AMD 6 | INSTRUMENTS, ELECTRICAL INDICATING (SEALED) - PART 2: LIST OF INSTRUMENTS |
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