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  • DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION

    Available format(s):  Hardcopy, PDF

    Superseded date:  31-01-2007

    Language(s):  English

    Published date:  01-01-2006

    Publisher:  UK Ministry of Defence Standards

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

    Preface
    Main Text
    SECTION 4 - DESIGN AND CONSTRUCTION
      4.0 Introduction
      4.1 General Detail Design
      4.2 Marking of Aeroplane Parts
      4.3 Protection of Structure
      4.4 Accessibility, Maintenance and Servicing
      4.5 Material Strength Properties and Values
      4.6 Process and Working of Materials
      4.7 Castings
      4.8 Aero-Elasticity, Flutter and Vibration
      4.9 Birdstrike Damage
      4.10 Control Systems
      4.11 Design of Undercarriages
      4.12 Wheels, Tyres and Brakes
      4.13 Operation from Rough Ground/Ground Clearance
      4.14 Nose Wheel Steering
      4.15 Crew Stations - General Requirements
      4.16 Pilot's Station - Layout
      4.17 View and Clear Vision
      4.18 Optically Transparent Components
      4.19 Cockpit Controls
      4.20 Doors
      4.21 Seats, berths, safety belts and harnesses
      4.22 Crash Landing & Ditching
      4.23 Emergency Provisions
      4.24 Ventilation & Heating
      4.25 Pressurised Air Ducts
      4.26 Fire Precautions
      4.27 Electrical Bonding
    Tables
    Diagrams
    Leaflets 0-95

    Abstract - (Show below) - (Hide below)

    Specifies the requirements covering the design and construction of the aircraft.

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    Development Note Supersedes DEFSTAN 00-970(PT1)SEC4/3(2003) (04/2006)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Superseded
    Superseded By
    Supersedes

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

    DEFSTAN 66-26(PT1)/1(1977) : 1977 GENERAL REQUIREMENTS FOR AIRCRAFT INSTRUMENTS AND DISPLAY - PART 1: AIRCRAFT INSTRUMENT CASES
    BS G 230:1984 Specification for general requirements for aircraft electrical cables (second series)
    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
    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
    DEFSTAN 05-18/4(1985) : 1985 AMD 2 1987 SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS
    MIL B 83054 : B BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
    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-PRF-27210 Revision J:2013 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)
    DEFSTAN 49-2/2(1975) : 1975 AMD 3 LUBRICATING GUNS, HAND AND GUNS, FLUID, DIRECT DELIVERY
    MIL-B-81365 Base Document:1966 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
    DEFSTAN 05-34/1(1973) : 1973 MARKING OF SERVICE MATERIAL
    DEFSTAN 05-21/1(1973) : 1973 QUALITY CONTROL SYSTEM REQUIREMENTS FOR INDUSTRY
    DEFSTAN 53-88/1(1979) : 1979 WASHERS, LOCK, KEY (TAB) AND SPRING TENSION (CRINKLE), INCH SERIES, FOR AEROSPACE APPLICATIONS
    DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991 PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS
    BS 1580-3:1965 Specification for Unified screw threads Diameters below ¼ in
    BS 5350-E1:1976 Methods of test for adhesives. Sampling and analysis of test data Guide to statistical analysis
    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
    FAA AC 20-100 : 1977 GENERAL GUIDELINES FOR MEASURING FIRE-EXTINGUISHING AGENT CONCENTRATIONS IN POWERPLANT COMPARTMENTS
    NFPA 326 : 2015 SAFEGUARDING OF TANKS AND CONTAINERS FOR ENTRY, CLEANING, OR REPAIR
    ASTM D 1781 : 1998 Standard Test Method for Climbing Drum Peel for Adhesives
    DEFSTAN 15-3 : LATEST TRANSPARENT GLAZING MATERIALS AND ACCESSORIES FOR AEROSPACE APPLICATIONS
    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
    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
    BS 5350-E2:1979 Methods of test for adhesives. Sampling and analysis of test data Guide to sampling
    EN 2243-1 : 2005 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 1: SINGLE LAP SHEAR
    MIL-P-6992 Base Document:1950 PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER
    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
    BS 3A125 TO 3A[...](1981) : 1981 AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT
    STANAG 3208 : 2009 AIR CONDITIONING CONNECTIONS
    DEFSTAN 03-2/4(2005) : 2005 CLEANING AND PREPARATION OF METAL SURFACES
    DEFSTAN 16-24/1(1983) : 1983 SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT
    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)
    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
    BS 5350-A1:1976 Methods of test for adhesives. Adherends Adherend preparation
    BS 5350-D4:1976 Methods of test for adhesives. Adhesively bonded joints: environmental tests Determination of staining potential
    BS 1580-1&2(1962) : 1962 SPECIFICATION FOR UNIFIED SCREW THREADS - DIAMETERS 1/4 INCH AND LARGER
    DEFSTAN 01-5/14(2005) : 2005 FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS
    MIL-T-18606 Base Document:1955 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
    PD 6484:1979 Commentary on corrosion at bimetallic contacts and its alleviation
    DEFSTAN 16-17/2(1983) : 1983 AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT
    MIL-HDBK-691 Revision B:1987 Adhesive Bonding
    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
    EN 2243-3:2005 Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb core
    BS 2C 12:1980 Specification for jacking pads for aircraft
    MIL-T-23103 Revision A:1971 THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR
    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
    DEFSTAN 03-24/4(2003) : 2003 CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS
    DEFSTAN 25-7/1(1968) : 1968 AMD 1 HORNS, ELECTRICAL
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