DEFSTAN 00-970(PT1)SEC6/13(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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 1: FIXED WING - SECTION 6: EQUIPMENT
Available format(s)
Hardcopy , PDF
Superseded date
30-01-2015
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Preface
SECTION 6 - EQUIPMENT
SUPPLEMENTS
Specifies requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military operation.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC6/12(2014). (10/2014)
|
| DocumentType |
Standard
|
| Pages |
272
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| BS C 18:1976 | Specification for V-flange couplings for aircraft piping and ducting - metric series |
| DEFSTAN 00-35(PT4)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 4: NATURAL ENVIRONMENTS |
| BS G 230:1984 | Specification for general requirements for aircraft electrical cables (second series) |
| BS 2G 143:1965 | Specification for a.c. and d.c. rotary and linear actuators for aircraft |
| BS J12(1966) : LATEST | |
| BS 2G 180:1974 | Specification for permanent splicing of aircraft electrical cables |
| DEFSTAN 61-10(PT1)/1(1995) : 1995 | GENERATOR SETS (GROUND, ENGINE DRIVEN) POWER AND DISTRIBUTION - PART 1: BOX, DISTRIBUTION 13 A 3 WAY, 240 V FOR FIELD ELECTRICAL POWER DISTRIBUTION SYSTEMS INCORPORATING CECC 75201.007 INPUT CONNECTOR |
| BS 2G 134:1970 | Specification for d.c. generators |
| BS 2G 210:1991 | Specification for PTFE insulated equipment wires and cables, single and multi-core, with silver plated copper conductors (190°C) or nickel plated copper conductors (260°C) |
| BS M 43:1973 | Methods of zoning aircraft and referencing access doors and panels |
| 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 00-35(PT5)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS |
| BS 5M 23:1987 | Specification for an identification scheme for pipelines |
| 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 |
| BS G 231:1983 | Specification for conductors for general purpose aircraft electrical cables and aerospace applications |
| BS G 207:1969 | Specification for aircraft electrical circuit diagrams |
| BS 3G 197:1982 | Specification for stud-type terminal blocks for terminations on aircraft electric cables |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| DEFSTAN 00-35(PT1)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 1: CONTROL AND MANAGEMENT |
| DEFSTAN 05-43/1(1977) : 1977 | STANDARD PROCEDURES FOR TAKING SAMPLES OF HYDRAULIC FLUIDS FOR EVALUATION OF PARTICULATE CONTAMINATION |
| DEFSTAN 61-12(PT9)/5(2008) : 2008 | WIRES, CORDS AND CABLES ELECTRICAL - METRIC UNITS - PART 9: CABLES AND WIRES ELECTRICAL FOR CABLES, RADIO FREQUENCY INCLUDING LIMITED FIRE HAZARD (LFH) VARIANTS |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| BS M 52:1983 | Method for impulse testing of hydraulic hose, tubing and fittings assemblies for aerospace fluid systems |
| BS 2G 202:1988 | Specification for design and performance requirements for airframe-fit electrical connectors for d.c. and low frequency a.c. applications |
| DEFSTAN 59-35(PT0)/3(1990) : 1990 | CONNECTORS ELECTRICAL - PART 0: GUIDE TO CONNECTORS ELECTRICAL, DIRECT CURRENT, LOW FREQUENCY AND RADIO FREQUENCY APPLICATIONS |
| BS G 212:1971 | Specification for general requirements for aircraft electrical cables |
| 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 |
| BS 2G 100-2:1962 | Specification for general requirements for electrical equipment and indicating instruments for aircraft Environmental and operating conditions |
| 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 |
| STANAG 3323 : 0 | PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC) |
| BS G 232:1984 | Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation |
| DEFSTAN 00-31/1(1987) : 1987 | THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
| BS M 44:1974 | Specification for identification of aircraft servicing, maintenance, ground handling and safety/hazard points |
| 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 |
| DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
| BS G 209:1970 | Specification for transformer rectifier units |
| DEFSTAN 00-35(PT3)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| BS M 48:1975 | Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
| BS 5G 205-1:1990 | Secondary batteries for aircraft Specification for lead-acid batteries |
| BS M 60:1986 | Specification for separable tube fittings for fluid systems |
| BS 2G 146:1966 | Specification for d.c. motors for aircraft |
| BS G 203:1967 | Specification for Unified screws with captive facing and locking washers |
| BS 2G 223:1989 | Specification for screen terminating devices for aircraft electric cables |
| BS 2G 229:1987 | Schedule for environmental conditions and test procedures for airborne equipment |
| 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) |
| BS C 13:1960 | Sizes of gravity filling orifices on aircraft |
| DEFSTAN 00-42(PT4)/3(2014) : 2014 | RELIABILITY AND MAINTAINABILITY ACTIVITY - PART 4: TESTABILITY |
| MIL-D-81641 Base Document:1972 | Display, Head-up, General Specification for |
| 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 |
| BS G 233:1984 | Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation |
| BS 2G 196:1971 | Specification for static invertors |
| MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| BS 2G 219:1983 | Specification for general requirements for ground support electrical supplies for aircraft |
| BS C 9:1970 | Specification for coupling dimensions for high pressure air charging valves for aircraft |
| 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 |
| BS 2G 100-3:1968 | General requirements for aircraft electrical equipment and indicating in struments Characteristics of aircraft electrical systems |
| BS G 217:1975 | Specification for general requirements for cockpit lighting controllers |
| ARINC 404A : 1974 | AIR TRANSPORT EQUIPMENT CASES AND RACKING |
| BS G 194:1965 | Specification for lever-operated manual switches for aircraft |
| BS G 102:1971 | Specification for general requirements for rotating electrical machinery |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| BS 4G 229:1996 | Schedule for environmental conditions and test procedures for airborne equipment |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| BS G 222:1976 | Specification for Efglas type electric cables (metric units) |
| DEFSTAN 00-970/VOL1/1(1983) : AMD 14 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES |
| DEFSTAN 00-970/VOL2/1(1984) : 1984 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
| DEFSTAN 00-52/4(2014) : 2014 | THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |
| ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
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