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Material Specification

Ti-6Al-6V-2Sn

Ti-6Al-6V-2Sn Fasteners
Highly Beta-Stabilised Alpha-Beta Alloy – Stronger Than Ti-6Al-4V

Titanium 6Al-6V-2Sn Fasteners

Buy Titanium 6Al-6V-2Sn (Ti-662 / UNS R56620) bolts, studs, machined components and forgings from Exotic Alloy. Ti-662 is a highly beta-stabilised two-phase alpha-beta alloy, modified from the Ti-6Al-4V system by raising vanadium to 5–6% and adding tin, copper and iron. The result is appreciably higher strength and better deep hardenability than Ti-6Al-4V, at some cost in ductility and weldability.

Exotic Alloy manufactures Ti-662 components to the governing AMS specifications — including AMS 4971 and AMS 4978 for bar and forgings and AMS 4918 for plate, sheet and strip — and to MIL-T-9046 and MIL-T-9047, in metric M6–M36 and imperial ¼"–1½" sizes, with full EN 10204 3.1 material test certificates for airframe structure and ordnance components.

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Product Range

Ti-6Al-6V-2Sn Fasteners Available

Ti-6Al-6V-2Sn Hex Bolts
Ti-6Al-6V-2Sn
Hex Bolts
Ti-6Al-6V-2Sn Heavy Hex Bolts
Ti-6Al-6V-2Sn
Heavy Hex Bolts
Ti-6Al-6V-2Sn Stud Bolts
Ti-6Al-6V-2Sn
Stud Bolts
Ti-6Al-6V-2Sn Threaded Rods
Ti-6Al-6V-2Sn
Threaded Rods
Ti-6Al-6V-2Sn Anchor Bolts
Ti-6Al-6V-2Sn
Anchor Bolts
Ti-6Al-6V-2Sn Hex Nuts
Ti-6Al-6V-2Sn
Hex Nuts
Ti-6Al-6V-2Sn Washers
Ti-6Al-6V-2Sn
Washers
Ti-6Al-6V-2Sn Cotter Pins
Ti-6Al-6V-2Sn
Cotter Pins
Ti-6Al-6V-2Sn Springs
Ti-6Al-6V-2Sn
Springs
Ti-6Al-6V-2Sn Circlips
Ti-6Al-6V-2Sn
Circlips
Ti-6Al-6V-2Sn Coated Fasteners
Ti-6Al-6V-2Sn
Coated Fasteners
Ti-6Al-6V-2Sn Custom Spacers
Ti-6Al-6V-2Sn
Custom Spacers
Technical Data

Ti-6Al-6V-2Sn Specifications

Chemical Composition — Titanium 6Al-6V-2Sn (wt. %)
ElementTiAlVSnCuFeOC
Min %Balance5.005.001.500.350.35––
Max %Balance6.006.002.501.001.000.200.05
Mechanical Properties — Titanium 6Al-6V-2Sn
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
Annealed (Typical)1035–1105965–103510–14–
Solution Treated & Aged (Typical)1170–12751100–12008–10–
Strength Relative to Ti-6Al-4VApproximately 15% higher–Lower ductility–
Alloy Class–––Alpha-beta, highly beta stabilised
Physical Properties
DensityApproximately 4.54 g/cm³
Modulus of ElasticityApproximately 110 GPa
Melting RangeApproximately 1538–1649°C
Thermal ConductivityApproximately 6.6 W/m·K at 20°C
Maximum Service TemperatureApproximately 315°C
Alloy ClassAlpha-beta — deeply hardenable, limited weldability
Equivalent Grades & Standards
UNSWerkstoff / DINASTM DesignationCommon Name
R56620 – AMS 4918 / 4971 / 4978 / MIL-T-9046 and 9047 Ti-662 / Ti-6-6-2

Key Specifications: AMS 4971 and AMS 4978 (Bar & Forgings) / AMS 4918 (Plate, Sheet & Strip) / MIL-T-9046 and MIL-T-9047. Not covered by ASTM B348. A caution on specification numbers. This alloy is covered by SAE AMS and MIL specifications rather than by ASTM B348, and the AMS numbers quoted for it differ between published sources — partly because several have been revised or superseded over the years. Acceptance values must come from the current SAE revision or the customer drawing that governs your parts, not from a catalogue listing. Our certified test values for your actual product form and heat treatment are supplied with every batch.

Machinability: titanium’s low thermal conductivity is the governing problem — the heat generated at the cut stays at the cutting edge instead of being carried away. Use rigid setups, sharp tooling, low surface speeds, heavy positive feeds and high-volume flood coolant directed into the cutting zone, and never let the tool dwell. Fine chips and grinding dust are a fire hazard and are handled wet. Threads are rolled rather than cut wherever the section permits, both for fatigue life and because cutting titanium threads invites the same galling that affects them in service. Ti-662 is harder to machine than Ti-6Al-4V in proportion to its higher strength, and the copper and iron additions make it slightly more abrasive.

Welding: weldability is poorer than Ti-6Al-4V and is the main penalty for the extra strength. The heavy beta stabilisation means weld and heat-affected zone ductility falls off significantly, and fusion welding of load-bearing joints is generally avoided. Welding requires full inert gas shielding of the weld, the heat-affected zone and the root — trailing shields and backing gas are standard practice. Weld colour is the first-pass check: bright silver is acceptable, straw and blue indicate increasing contamination, and grey or white powder means the weld must be cut out. Where joints are needed, mechanical fastening is the preferred route.

Forming: hot work in the 870–955°C range. Cold formability is poor. Thread rolling is practicable and strongly preferred to cutting.

Heat Treatment: Ti-662 is more deeply hardenable than Ti-6Al-4V, which is the practical consequence of its higher beta stabiliser content — solution treatment and ageing develops full properties through thicker sections than Grade 5 can manage. Fasteners are supplied annealed or solution treated and aged to the condition stated on the order. All heat treatment above roughly 500°C must be carried out in vacuum or inert gas, or the oxygen-enriched alpha case removed afterwards, because titanium absorbs oxygen, nitrogen and hydrogen rapidly at temperature and a contaminated surface layer is brittle.

Ti-662 is a strength alloy and its corrosion behaviour follows Ti-6Al-4V rather than the commercially pure grades — good in marine and oxidising environments, limited in reducing acids, and not a substitute for the CP or lean corrosion grades on corrosion duty. The copper and iron additions, which are deliberate here rather than residual, slightly reduce corrosion performance relative to Grade 5.

The reason to choose it is roughly 15% more strength than Ti-6Al-4V with deeper hardenability, which matters for thick-section forgings and for highly loaded fasteners where Grade 5 is marginal. The trade-offs are real and should be weighed: lower ductility, poorer weldability, and a lower useful service temperature than the near-alpha alloys.

Titanium alloys divide into four classes, and the class tells you more than the grade number does. Alpha and near-alpha alloys are weldable and creep resistant and run hottest, but are not heat treatable to high strength. Alpha-beta alloys — of which Ti-6Al-4V is the archetype — are heat treatable, strong and the general structural choice. Near-beta and metastable beta alloys are deeply hardenable, can be cold formed in the solution-treated condition and then aged to very high strength, which makes them the natural choice for fasteners and springs. Commercially pure and lean corrosion grades trade all strength away for corrosion performance.

Three absolute exclusions apply to every titanium grade: it must not be used in dry chlorine, with which it reacts violently; not with red fuming nitric acid; and it is rapidly attacked by hydrofluoric acid at any concentration. Fine titanium swarf and grinding dust are a fire hazard and are handled wet.

Titanium galls, and for a threaded fastener this is the dominant practical issue. A titanium thread run against another titanium thread will cold-weld and seize, often badly enough that the fastener has to be cut off. Every titanium bolted joint needs one of three mitigations: an anti-seize compound or dry-film lubricant such as molybdenum disulphide; a plated or coated thread, commonly silver or solid-film lubricant; or a nut in a dissimilar material. Specify which at order stage.

Titanium is galvanically noble. It will not corrode itself, but a titanium fastener in an aluminium, carbon steel, zinc or magnesium assembly drives accelerated corrosion of the structure around it, and a bolted joint’s small-anode, large-cathode geometry is the worst case. Insulating washers and sleeves or a barrier coating should be specified in those assemblies.

Key Characteristics

  • Approximately 15% stronger than Ti-6Al-4V in the same condition.
  • Deeper hardenability than Grade 5 for thick-section forgings.
  • Highly beta-stabilised alpha-beta structure.
  • Deliberate copper and iron additions, not residuals.
  • Solution treated and aged to 1170–1275 MPa typical.

Typical Applications

  • Aerospace: highly loaded airframe fastener assemblies.
  • Thick-section structural forgings requiring through hardening.
  • Ordnance and defence hardware.
  • High-strength rotating and structural components.
  • Applications where Ti-6Al-4V is marginal on strength.