15/30329889 DC : 0

Superseded

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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

Superseded date

02-29-2016

Language(s)

English

Publisher

British Standards Institution

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Status	Superseded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 2A 266 to 2A 271:2016+A1:2019

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 AS 5272 : 2016	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 AMS 03-19 : 2015	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 AMS 4967 : 2014	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