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DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)

Superseded date

13-07-2015

Published date

14-04-2015

DevelopmentNote
Supersedes DEFSTAN 00-970(PT7)SEC2/SUPPD/4(2014). (04/2015)
DocumentType
Miscellaneous Product
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Superseded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
DEFSTAN 17-3/1(1972) : 1972 ADAPTORS, AIRCRAFT JACKING POINTS (DETACHABLE JACKING PADS)
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
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
MIL B 83054 : B BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
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-A-83377 Revision B:1978 ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR
DEFSTAN 05-18/5(2007) : 2007 SYMBOL MARKINGS OF SERVICING AND SAFETY/HAZARD POINTS ON AIRCRAFT, GROUND SUPPORT EQUIPMENT AND GUIDED WEAPONS SYSTEMS
MIL-C-7762 Revision A:1967 COMPASS, INSTALLATION OF
SAE J 1013 : 1992 MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES
MIL O 27210 : F 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 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 00-29/1(1982) : 1982 FUNGAL CONTAMINATION AFFECTING THE DESIGN OF MILITARY MATERIAL
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
MIL-A-9067 Revision C:1961 ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR
DEFSTAN 61-15/3(1990) : 1990 AMD 1 1991 PRECAUTIONS AGAINST ELECTRICAL SHOCK IN MAINTENANCE AREAS
DEFSTAN 05-61(PT12)/1(1987) : 1987 QUALITY ASSURANCE PROCEDURAL REQUIREMENTS - PART 12: CONTROL OF WALL THICKNESS IN DESIGN AND MANUFACTURE OF FLYING CONTROL SYSTEMS
MIL-S-58095 Revision A:1986 SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
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
MIL-W-81752 Revision A:1987 WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR
ASTM D 1781 : 1998 Standard Test Method for Climbing Drum Peel for Adhesives
MIL-A-25463 Revision B:1982 ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION
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
EN 2243-1 : 2005 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 1: SINGLE LAP SHEAR
MIL P 8184 : E PLASTIC SHEET, ACRYLIC, MODIFIED
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
DEFSTAN 07-55(PT2)SEC4/1(1975) : 1975 AMD 3 1983 ENVIRONMENTAL TESTING OF SERVICE MATERIAL - PART 2: TESTS - SECTION 4: PENETRATION AND IMMERSION
MIL-STD-1290 Revision A:1988 LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE
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
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
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 6F 100:1998 Procedure for inspection and testing of textiles for aerospace purposes
MIL-I-8673 Base Document:1955 INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
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
MIL-P-83310 Base Document:1971 PLASTIC SHEET, POLYCARBONATE, TRANSPARENT
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
DEFSTAN 00-50/1(1982) : 1982 GUIDE TO CHEMICAL ENVIRONMENTAL CONTAMINANTS AND CORROSION AFFECTING THE DESIGN OF MILITARY MATERIAL
BS 2C 12:1980 Specification for jacking pads for aircraft
MIL-STD-1294 Revision A:1985 ACOUSTICAL NOISE LIMITS IN HELICOPTERS
MIL-T-23103 Revision A:1971 THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR
MIL-E-7080 Revision B:1962 ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
MIL-S-85510 Base Document:1981
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
STANAG 3950 : 0 HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION
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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