DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date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
Superseded by
Language(s)
English
Published date
01-01-2006
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
Specifies the requirements covering the design and construction of the aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC4/3(2003) (04/2006)
|
| DocumentType |
Standard
|
| Pages |
1032
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 ARP1524A | 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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