DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
Available format(s)
Hardcopy , PDF
Superseded date
07-26-2022
Superseded by
Language(s)
English
Published date
01-01-2015
Publisher
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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
Describes the requirements covering the design and construction of the aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC4/13(2015). Reproducible but contains Colour Pages, Advise dispatch. (10/2015)
|
| DocumentType |
Standard
|
| Pages |
951
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| DEFSTAN 00-003/5(2016) : 2016 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| DEFSTAN 00-003/6(2017) : 2017 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| ISO 2631:1978 | Guide for the evaluation of human exposure to whole-body vibration |
| STANAG 3370 : 2004 | AIRCREW STATION ALERTING SYSTEMS |
| DTD 925 D : JUL 69 | THE FABRICATION OF ACRYLIC PANELS AND SHAPINGS |
| DEFSTAN 66-26(PT1)/1(1977) : 1977 | GENERAL REQUIREMENTS FOR AIRCRAFT INSTRUMENTS AND DISPLAY - PART 1: AIRCRAFT INSTRUMENT CASES |
| DEFSTAN 17-1/2(1984) : 1984 | AIRCRAFT LIFTING SLINGS, APERTURE OF TERMINAL RING OR LINK |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| BS G 175:1959 | Aircraft fuel nozzle grounding plugs and sockets |
| DTD 5577 : NOV 65 | HEAT STABLE STRUCTURAL ADHESIVES |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| 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 |
| 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 |
| DEFSTAN 05-18/5(2007) : 2007 | SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS |
| MIL-PRF-27210 Revision J:2013 | OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS |
| SAE J 1013 : 1992 | MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES |
| 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) |
| MIL-DTL-83054 Revision C:2003 | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| DEFSTAN 49-2/2(1975) : 1975 AMD 3 | LUBRICATING GUNS, HAND AND GUNS, FLUID, DIRECT DELIVERY |
| DEFSTAN 05-34/2(1984) : 1984 | MARKING OF SERVICE MATERIAL |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| DEFSTAN 05-21/1(1973) : 1973 | QUALITY CONTROL SYSTEM REQUIREMENTS FOR INDUSTRY |
| DEFSTAN 03-24/5(2008) : 2008 | CHROMIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
| 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 |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| 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 |
| DTD 761C : DEC 65 | SAFETY GLASS WINDSCREEN, WEAPON SIGHTING QUALITY |
| FAA AC 20-100 : 1977 | GENERAL GUIDELINES FOR MEASURING FIRE-EXTINGUISHING AGENT CONCENTRATIONS IN POWERPLANT COMPARTMENTS |
| DTD 5548 : AMD 1 | GLAZING COMPOUNDS |
| DTD 5627 : APR 82 | FIBROUS POLYAMIDE MATERIAL FOR USE AS AN EXPLOSION SUPPRESSANT AND AS A BAFFLE MATERIAL IN AIRCRAFT FUEL TANKS |
| ASTM D 1781 : 1998 | Standard Test Method for Climbing Drum Peel for Adhesives |
| DTD 5624 : MAR 81 | FIBROUS POLYESTER MATERIAL FOR USE AS A FLAME AND FIRE SUPPRESSANT IN AIRCRAFT DRY BAYS |
| DEFSTAN 15-3 : LATEST | TRANSPARENT GLAZING MATERIALS AND ACCESSORIES FOR AEROSPACE APPLICATIONS |
| STANAG 3647 : 0 | NOMENCLATURE IN AIRCREW STATIONS |
| DTD 861A : DEC 59 | ADHESIVE FOR METAL (LOW PRESSURE TYPE) |
| 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-DTL-23659 Revision F:2010 | Initiators, Electric, General Design Specification for |
| DTD 218D : SEP 66 | LAMINATED SAFETY GLASS |
| 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 |
| 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 |
| STANAG 3224 : 2005 | AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL-H-5484 Revision C:1964 | Heater, Aircraft, Combustion Type |
| BS 3G 230:2000 | Specification for general requirements for aircraft electrical cables (second series) |
| 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 |
| DEFSTAN 03-2/6(2011) : 2011 | CLEANING AND PREPARATION OF METAL SURFACES |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| STANAG 3208 : 2009 | AIR CONDITIONING CONNECTIONS |
| DEFSTAN 16-24/1(1983) : 1983 | SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
| DTD 870A : NOV 57 | BULLET RESISTANT SAFETY GLASS, HIGH LIGHT TRANSMISSION |
| DEFSTAN 66-26(PT3)/1(1979) : 1979 | GENERAL REQUIREMENTS FOR AIRCRAFT INSTRUMENTS AND DISPLAYS - PART 3: REFLECTION-REDUCING COATINGS USED ON GLASS ELEMENTS IN AIRCREW STATION DISPLAYS (SPECIFICATION) |
| DEFSTAN 66-26(PT7)/1(1986) : 1986 | GENERAL REQUIREMENTS FOR AIRCRAFT INSTRUMENTS AND DISPLAYS - PART 7: COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF INSTRUMENTS |
| 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) |
| PREN 2101 : 1987 | CHROMIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS |
| 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 6F 100:1998 | Procedure for inspection and testing of textiles for aerospace purposes |
| DTD 5576A : JAN 66 | LAMINATED SAFETY GLASS HEATED BY ELECTRICALLY CONDUCTING FILM(S) |
| MIL-T-18606 Base Document:1955 | TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
| PD 6484:1979 | Commentary on corrosion at bimetallic contacts and its alleviation |
| DTD 5592 : LATEST | ACRYLIC SHEETS FOR AIRCRAFT GLAZING |
| 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 |
| DTD 869A : NOV 57 | LAMINATED SAFETY GLASS, HIGH LIGHT TRANSMISSION |
| SAEITC TS120-6 | TS120 AGS2000 Series Stiffnuts (including Clinch Nuts) BA and BSF Threads for Aircraft |
| 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 25-7/1(1968) : 1968 AMD 1 | HORNS, ELECTRICAL |
| BS C 10:1958 | Coupling dimensions for aircraft ground air-conditioning connections |
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