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DEF STAN 05-69 - Standard Colour Scheme of Metallic Materiels for Aerospace Applications
November 10, 2000 - MODUK

This standard sets out a standard scheme for the colour code identification of metallic materials intended for aerospace applications. The colour codes listed in Annexes A and B are appropriate to the contents of the RAF stores vocabulary sections 30A to 30E inclusive. Codes for similar standards...

Cast and Wrought Aluminium Bronzes
January 1, 2000 - MANEY

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...

DEF-SPEC-30 - Aluminium Alloy Pressure Die Castings (Control of Manufacture and Inspection) (01.69)
January 1, 1969 - MODUK

This specification deíìnes the requirements for the manufacture and inspection of aluminium pressure die castings for Service use. Castings made by low pressure methods (e.g, of the order of 5-10 lbf/in2} are not appropriate to this specification. It includes a castings classification scheme...

Crack resistance curves.
November 1, 1995 - ESDU

ESDU 85031 provides R-curves for several aluminium, steel and titanium aerospace sheet materials in SI and British (lbf, in) units on transparencies for overlaying on plots of stress intensity factor against crack length appropriate to the user's structure (matching blank grids are...

DTD-722B - Ingots and Castings of Aluminium - Silicon - Magnesium Alloy (Precipitation Treated) (Si 5, Mg 0.5) (06.71)
January 1, 1971 - MODUK

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.

DTD-716B - Ingots and Castings of Aluminium - Silicon - Magnesium Alloy (as Cast) (Si 5, Mg 0.5) (01.71)
January 1, 1971 - MODUK

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 ìngots for their...

DTD-5343 - Forging Stock of Titanium - Aluminium - Molybdenum - Tin - Silicon Alloy (Tensile Strength 1080-1260 MPa) (Limiting Ruling Section 100mm) (06.74)
January 1, 1974 - MODUK

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.

DTD-5313 - Forging Stock of Titanium - Aluminium - Vanadium Alloy (Tensile Strength 930-1160 MPa) (Limiting Ruling Section 150mm) (01.74)
January 1, 1974 - MODUK

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.

DTD-5024 - Aluminium - Zinc - Magnesium - Copper - Manganese Alloy Forgings (Not Exceeding 10 Inches Diameter or Minor Sectional Dimension) (Solution Treated and Precipitation Treated) (03.58)
January 1, 1958 - MODUK

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...

DTD-5044 - Aluminium - Zinc - Magnesium - Copper - Manganese Alloy Bars and Extruded Sections (Not Exceeding 10 Inches or Minor Sectional Dimension) (Solution Treated and Precipitation Treated) (03.58)
January 1, 1958 - MODUK

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 for aircraft material or to serve as a basis for inspection of materials the properties and uses of which are not sufficiently developed...

DTD-5104 - Forging Stock and Forgings of Aluminium- Zinc-Magnesium-Copper- Manganese Alloy (Solution Treated, Boiling Water Quenched and Duplex Precipitation Treated to Improve Stress Corrosion Resistance) (Zn 5.7, Mg 2.5, Cu 0.5, Mn 0.5) (06.71)
January 1, 1971 - MODUK

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.

SAE ITC TS39 - Manufacturing and Inspection Requirements for Rivet, Blind, Self-Plugging, Flush Break, Mechanically Locked Stem, Aluminium Alloys AS46784 to AS46787
May 1, 1992 - SAE-ITC

FOREWORD On the 1st January 2015 the SAE Industry Technologies Consortia (SAE ITC) acquired the ADS Aerospace Standards, previously known as the Society of British Aerospace Companies (SBAC) Aerospace Standards. The SAE ITC established in 2003 operates as a trade association as part of the...

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