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  • DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

    Available format(s):  Hardcopy, PDF

    Superseded date:  07-01-2013

    Language(s):  English

    Published date:  01-01-2012

    Publisher:  UK Ministry of Defence Standards

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

    Preface
    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 Processes 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
    SUPPLEMENTS
    Leaflets 0 to 97

    Abstract - (Show below) - (Hide below)

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

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    Development Note Supersedes DEFSTAN 00-970(PT1)SEC4/8(2011). (08/2012)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Superseded

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

    MIL F 8785 : C FLYING QUALITIES OF PILOTED AIRPLANES
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL E 22285 : 0 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
    MIL B 83054 : B BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
    MIL P 46111 : C PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT)
    MIL PRF 27210 : J OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS
    MIL B 81365 : 0 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
    MIL I 8672 : B INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG]
    MIL D 21625 : G DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES
    MIL DTL 23659 : F INITIATORS, ELECTRIC, GENERAL DESIGN SPECIFICATION FOR
    MIL E 18927 : E ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL P 6992 : 0 PUMP ASSEMBLY, FUEL, ELECTRICALLY DRIVEN, AIRCRAFT HEATER
    MIL H 5484 : C HEATER, AIRCRAFT, COMBUSTION TYPE
    MIL M 8609 : B MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL F 23447 : 0 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    MIL STD 1472 : G HUMAN ENGINEERING
    MMM A 132 : B ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL
    MIL T 18606 : 0 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
    MIL I 8670 : B INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
    MIL T 23103 : A THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR
    MIL HDBK 221 : 0 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
    BS C10(1958) : 1958 COUPLING DIMENSIONS FOR AIRCRAFT GROUND AIR-CONDITIONING CONNECTIONS
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