DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
Hardcopy , PDF
31-10-2011
English
01-01-2011
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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
Leaflets
Describes the requirements covering the design and construction of the aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC4/6(2010). (05/2011)
|
| DocumentType |
Standard
|
| Pages |
1041
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| ISO 2631:1978 | Guide for the evaluation of human exposure to whole-body vibration |
| STANAG 3370 : 2004 | AIRCREW STATION ALERTING SYSTEMS |
| BS 2SP90(2008) : 2008 | SPECIFICATION FOR CORROSION-RESISTING STEEL SPLIT COTTER PINS FOR AIRCRAFT - INCH SERIES |
| DEFSTAN 17-1/2(1984) : 1984 | AIRCRAFT LIFTING SLINGS, APERTURE OF TERMINAL RING OR LINK |
| DTD 5577 : NOV 65 | HEAT STABLE STRUCTURAL ADHESIVES |
| DTD 775 : A | ADHESIVE SUITABLE FOR JOINING METALS |
| DEFSTAN 05-18/5(2007) : 2007 | SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS |
| 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 |
| 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 |
| 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 |
| ASTM D 1781 : 1998 | Standard Test Method for Climbing Drum Peel for Adhesives |
| STANAG 3647 : 0 | NOMENCLATURE IN AIRCREW STATIONS |
| 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 |
| 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 |
| DEFSTAN 95-7/1(1976) : AMD 2 | WIRE FOR LOCKING PURPOSES AND WIRE LOCKING PRACTICE FOR AEROSPACE USES |
| STANAG 3224 : 2005 | AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
| BS 3A125 TO 3A[...](1981) : 1981 | AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT |
| 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 |
| BS 6F 100:1998 | Procedure for inspection and testing of textiles for aerospace purposes |
| MMM-A-132 Revision B:1994 | ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL |
| PD 6484:1979 | Commentary on corrosion at bimetallic contacts and its alleviation |
| DEFSTAN 03-2/5(2009) : 2009 | CLEANING AND PREPARATION OF METAL SURFACES |
| DEFSTAN 16-17/2(1983) : 1983 | AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
| MIL-HDBK-691 Revision B:1987 | Adhesive Bonding |
| 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 |
| SAEITC TS120-6 | TS120 AGS2000 Series Stiffnuts (including Clinch Nuts) BA and BSF Threads for Aircraft |
| SAE ARP 1524 : 2013 | SURFACE PREPARATION AND PRIMING OF ALUMINUM ALLOY PARTS FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
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