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BSI - BS 2TA 28 - SPECIFICATION FOR FORGING STOCK AND WIRE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 1100-1300 MPA) (LIMITING RULING SECTION 20 MM) (PRIMARILY INTENDED FOR THE MANUFACTURE OF FASTENERS COMPLYING WITH THE REQUIREMENTS OF THE 'A' SERIES OF BRITISH STANDARDS) - AMD 2134: OCTOBER 1976; AMD 3755: APRIL 1984; AMD 6141: NOVEMBER 30, 1990 Organization: BSI
Date: 1974-05-30
MANEY - CAST & WROUGHT ALUMINIUM - CAST AND WROUGHT ALUMINIUM BRONZES - PROPERTIES, PROCESSES, AND STRUCTURE Organization: MANEY
Date: 2000-01-01
Description: FOREWORD This book has been written at the request of the Copper Development Association of Great Britain to bring up to date the information contained in the excellent book by P J Macken and AA Smith, published in 1966, which has hitherto been the standard reference book on aluminium bronze throughout the industrial world.
WRC BUL 152 - INFLUENCE OF WELD DEFECTS ON THE MECHANICAL PROPERTIES OF ALUMINUM ALLOY WELDMENTS - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: WRC
Date: 1970-07-01
Description: Of the hundreds of papers examined, only about 30 contained pertinent and quantitative data, much of which concerned heat-treatable alloys for military or aerospace applications. Except for some British investigations, little study has been reported for the more common structural alloys, such as the 5000 and 6000 series.
MODUK - DEF-166 - ALUMINIUM ALLOY GRAVITY DIE CASTING (CONTROL OF MANUFACTURE AND INSPECTION) (01.69) Organization: MODUK
Date: 1969-01-01
Description: Details of recommended alloys are given in Appendix A. Die castings using materials to British Standard Aircraft or DTD specifications are subject to the inspection requirements of BS L101.
MODUK - DEF-SPEC-30 - ALUMINIUM ALLOY PRESSURE DIE CASTINGS (CONTROL OF MANUFACTURE AND INSPECTION) (01.69) Organization: MODUK
Date: 1969-01-01
Description: Details of recommended alloys are given in Appendix A. Die castings using materials to British Standard Aircraft or DTD specifications are subject to the Inspection requirements of BS L 101.
MODUK - DTD-5363 - CASTINGS OF TITANIUM - ALUMINIUM - VANADIUM ALLOY (ANNEALED) (06.78) Organization: MODUK
Date: 1978-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for Aerospace Material.
MODUK - DTD-5110 - ALUMINIUM-ALLOY-COATED PLATE OF ALUMINIUM-ZINC- MAGNESIUM-COPPER- CHROMIUM ALLOY (SOLUTION TREATED, CONTROLLED STRETCHED AND PRECIPITATION TREATED) (ZN 5.8, MG 2.5, CU 1.6, CR 0.15) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-487 - NICKEL-COPPER-ALUMINIUM ALLOY COLD-HEADED BOLTS (NOT EXCEEDING 5/8 IN DIAMETER) (11.41) - (REPRINTED MARCH 1963) Organization: MODUK
Date: 1941-01-01
Description: This specification is one of a series issued by the Ministry of Aviation, either to meet a limited requirement not covered by any existing British Standard for aircraft material or to serve as a basis for inspection of materials the properties and uses of which are not sufficiently developed to warrant submission to the British Standards Institution for standardisation.
MODUK - DTD-297A - ALUMINIUM - 7 PER CENT MAGNESIUM ALLOY BARS, EXTRUDED SECTIONS AND FORGINGS (06.55) - (REPRINTED MARCH 1966) Organization: MODUK
Date: 1955-01-01
Description: This specification is one of a series issued by the Ministry of Aviation, either to meet a limited requirement not covered by any existing British Standard for aircraft material or to serve as a basis for inspection of materials the properties and uses of which are not sufficiently developed to warrant submission to the British Standards Institution for standardization.
MODUK - DTD 450A - ALUMINIUM - COPPER - MAGNESIUM - SILICON ALLOY TUBES (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) Organization: MODUK
Date: 1955-01-01
Description: This specification is one of a series issued by the Ministry of Supply, either to meet a limited requirement not covered by any existing British Standard Specification or to serve as a basis for inspection of materials the properties and uses of which are not sufficiently developed to warrant submission to the British Standards Institution for standardisation.
MODUK - DTD-450A - ALUMINIUM - COPPER - MAGNESIUM - SILICON ALLOY TUBES (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (01.55) Organization: MODUK
Date: 1955-01-01
Description: This specification is one of a series issued by the Ministry of Supply, either to meet a limited requirement not covered by any existing British Standard Specification or to serve as a basis for inspection of materials the properties and uses of which are not sufficiently developed to warrant submission to the British Standards Institution for standardisation.
MODUK - DTD-5323 - FORGINGS OF TITANIUM - ALUMINIUM - VANADIUM ALLOY (TENSILE STRENGTH 930-1160 MPA) (LIMITING RULING SECTION 150MM) (01.74) Organization: MODUK
Date: 1974-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-722B - INGOTS AND CASTINGS OF ALUMINIUM - SILICON - MAGNESIUM ALLOY (PRECIPITATION TREATED) (SI 5, MG 0.5) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence, to meet a requirement not covered by art existing British Standard for aerospace material.
MODUK - DTD-5018A - INGOTS AND CASTINGS OF ALUMINIUM-MAGNESIUM-ZINC ALLOY (SOLUTION TREATED) (MG 7.7, ZN 1.2) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-716B - INGOTS AND CASTINGS OF ALUMINIUM - SILICON - MAGNESIUM ALLOY (AS CAST) (SI 5, MG 0.5) (01.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Ministry of Defence (Aviation Supply), to meet a requirement not covered by an existing British Standard for aerospace material. Castings of this composition in the solution treated and precipitation treated condition and ├Čngots for their manufacture are covered by specification D.T.D. 735B.
MODUK - DTD-5100A - ALUMINIUM-COATED PLATE OF ALUMINIUM - COPPER - MAGNESIUM - MANGANESE ALLOY (SOLUTION TREATED, CONTROLLED STRETCHED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 1.5, MN 0.6) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Ministry of Defence (Aviation Supply) to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-5040A - ALUMINIUM-COATED PLATE OF ALUMINIUM - COPPER - MAGNESIUM - SILICON - MANGANESE ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED) (CU 4.4, MG 0.5, SI 0.7, MN 0.8) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Ministry of Defence (Aviation Supply) to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-5030A - ALUMINIUM-COATED PLATE OF ALUMINIUM - COPPER - MAGNESIUM - SILICON - MANGANESE ALLOY (SOLUTION TREATED AND AGED AT ROOM TEMPERATURE) (CU 4.4, MG 0.5, SI 0.7, MN 0.8) (06.71) Organization: MODUK
Date: 1971-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-5303 - BAR AND SECTION FOR MACHINING OF TITANIUM - ALUMINIUM - VANADIUM ALLOY (TENSILE STRENGTH 930-1160 MPA) (LIMITING RULING SECTION 150MM) (01.74) Organization: MODUK
Date: 1974-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.
MODUK - DTD-5313 - FORGING STOCK OF TITANIUM - ALUMINIUM - VANADIUM ALLOY (TENSILE STRENGTH 930-1160 MPA) (LIMITING RULING SECTION 150MM) (01.74) Organization: MODUK
Date: 1974-01-01
Description: This specification is one of a series issued by the Procurement Executive, Ministry of Defence to meet a requirement not covered by an existing British Standard for aerospace material.

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