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15/30329889 DC : 0

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

BS A 266 TO 271 - BOLT, 100 DEGREES COUNTERSUNK HEAD, HI-TORQUE SPEED DRIVE RECESS, UNJF THREAD, SPLIT PIN HOLE OPTION, TITANIUM ALLOY, VARIOUS FINISHES, CLASSIFICATION: 80 TF/IN[2] (1100 MPA) AT TA/+315 DEGREES C

Available format(s)

Hardcopy , PDF

Language(s)

English

Superseded date

29-02-2016

£20.00
Excluding VAT

Foreword
1 Scope
2 Normative referenced
3 General requirements
4 BS part number
5 Identification and marking
Bibliography

BS A 266 to 271.

Committee
ACE/12
DocumentType
Draft
Pages
19
PublisherName
British Standards Institution
Status
Superseded
SupersededBy

BS A 346:2000 UNJ threads. General requirements and limit dimensions
BS A242,A243,A244,A245(1974) : 1974 SPECIFICATION FOR HEXAGONAL CASTLE NUTS (OF CLASS 3B UNJ THREAD)
BS EN 3813:2013 Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. D<sub>e</sub> ≤ 50 mm
BS A 273:1978 Specification for gauging practice for 100° countersunk head fasteners for flushness control
DEFSTAN 01-5/17(2011) : 2011 FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS
BS EN 2808:1997 Anodizing of titanium and titanium alloys
ISO 8080:1985 Aerospace — Anodic treatment of titanium and titanium alloys — Sulfuric acid process
SAE AS5272E Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification
BS A 272:1977 Specification for Hi-torque speed drive recess: dimensions and gauging for countersunk head fasteners
DTD 942 : AUG 73 ANODIZING OF TITANIUM AND TITANIUM ALLOYS
BS EN 2133:2010 Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
SAE AMS03_19 Electro-Deposition of Cadmium
BS A101(1969) : 1969 GENERAL REQUIREMENTS FOR TITANIUM BOLTS
BS 3TA28(2009) : 2009 AEROSPACE SERIES - SPECIFICATION FOR FORGING STOCK AND WIRE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 1100-1300 MPA) (LIMITING RULING SECTION 20 MM)
BS M 58:1986 Specification for anodic coating of titanium and titanium alloys by the sulphuric acid process
SAE AMS4967L Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable
ISO 3161:1999 Aerospace — UNJ threads — General requirements and limit dimensions

£20.00
Excluding VAT