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  • DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 1: FIXED WING - SECTION 6 - EQUIPMENT

    Available format(s):  Hardcopy, PDF

    Superseded date:  20-07-2012

    Language(s):  English

    Published date:  01-01-2011

    Publisher:  UK Ministry of Defence Standards

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    Table of Contents - (Show below) - (Hide below)

    Preface
    SECTION 6 - EQUIPMENT
    6.0 Introduction
    6.1 General
    6.2 Avionic Equipment Installations
    6.3 Static Pressure Systems
    6.4 Magnetic Compass Installations
    6.5 Automatic Pilot Systems
    6.6 Electrical Systems
    6.7 Lights
    6.8 Safety Equipment
    6.9 Ice Protection
    6.10 EMC of Safety Critical Systems
    6.11 Hydraulic Systems
    6.12 Pneumatic Systems
    6.13 Oxygen Systems
    6.14 Pressurised Gas Storage Vessels
    6.15 Data Recording Systems
    SUPPLEMENTS
    Section 6 - Leaflets 0 to 34

    Abstract - (Show below) - (Hide below)

    Describes the requirements relating to equipment and systems embodied on any aircraft.

    General Product Information - (Show below) - (Hide below)

    Development Note Supersedes DEFSTAN 00-970(PT1)SEC6/7(2011). (11/2011)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    BS 3J 12:1991 Specification for pressure-sensitive adhesive identification tape
    BS C 18:1976 Specification for V-flange couplings for aircraft piping and ducting - metric series
    BS 2M 51:1989 Classification for pressure and temperature for fluid systems and components
    DEFSTAN 00-35(PT4)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 4: NATURAL ENVIRONMENTS
    BS 2G 143:1965 Specification for a.c. and d.c. rotary and linear actuators for aircraft
    DEFSTAN 00-13/3(1994) : 1994 REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT
    BS 2G 134:1970 Specification for d.c. generators
    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
    BS 2C 13:1988 Specification for sizes of aircraft gravity filling orifices and associated replenishment nozzles (metric series)
    BS 3M 60:1998 Separable tube fittings for fluid systems, 24° cone. General specification
    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
    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 207:1969 Specification for aircraft electrical circuit diagrams
    DTD 933A : FEB 64 GLASS FABRIC REINFORCED POLYESTER LAMINATES FOR AIRCRAFT STRUCTURES AND AIRBORNE RADOMES
    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
    DTD 856A : LATEST EXTERNAL FINISHES FOR RADOMES
    DEFSTAN 01-5/17(2011) : 2011 FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS
    ISO 6771:2007 Aerospace Fluid systems and components Pressure and temperature classifications
    BS 2M 53:1997 Aircraft. Fluid systems. Thermal shock testing of piping and fittings
    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
    BS 3G 231:1997 Specification for conductors for general-purpose aircraft electrical cables and aerospace applications
    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
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    BS 2M 52:1989 Method for impulse testing of hydraulic hose, tubing and fitting 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
    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
    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
    BS 2G 232:1987 Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation
    DEFSTAN 00-35(PT3)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS
    BS M 48:1975 Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series
    DTD 926B : SEP 63 PROCESS FOR THE EXTERNAL FINISHING OF RADOMES
    BS 3G 230:2000 Specification for general requirements for aircraft electrical cables (second series)
    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
    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)
    DEFSTAN 59-36/5(1995) : 1995 SELECTION OF ELECTRONIC AND ELECTRICAL COMPONENTS FOR USE IN DEFENCE EQUIPMENT
    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 3G 210:1996 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 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
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    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
    DEFSTAN 61-3/5(1992) : INTERIM GENERIC SPECIFICATION FOR BATTERIES, NON RECHARGEABLE, PRIMARY
    BS 6G 205-1:1995 Secondary batteries for aircraft Specification for lead-acid batteries
    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 G 217:1975 Specification for general requirements for cockpit lighting controllers
    BS 2917-1:1993 Graphic symbols and circuit diagrams for fluid power systems and components. Specification for graphic symbols
    ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING
    BS G 194:1965 Specification for lever-operated manual switches for aircraft
    BS 3G 233:1990 Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation
    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)
    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
    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
    DEFSTAN 00-52/3(1991) : 1991 THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES
    STANAG 3212 : 2017 DIAMETERS FOR GRAVITY FILLING ORIFICES
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