Kochlin SPECIAL ALLOYS · SINCE 2009

UNS R56620Ti-6Al-6V-2Sn

High-strength structural forgings — wing joints and fittings

Titanium
Units
Tensile Rm
1207
MPa · ≥ std. min
Yield Rp0.2
1103
MPa · ≥ std. min
Elongation A
8
% · ≥ std. min
Service limit
315
°C · indicative max
Density
4.54
g/cm³

Chemical composition

Ti 85%Al 5.5%V 5.5%Sn 2%Fe 0.68%Cu 0.68%Minor & residual 0.30%

Nominal: mid-range where both limits are given, the cap where only a maximum is, balance takes the remainder. Exact specified ranges below.

ElementName Content %
Main elements6 elements
Ti TitaniumBal.
Al Aluminium5 – 6%
V Vanadium5 – 6%
Sn Tin1.5 – 2.5%
Fe Iron0.35 – 1%
Cu Copper0.35 – 1%
ElementName Content %
Minor & residual4 elements
O Oxygen≤ 0.2%
C Carbon≤ 0.05%
N Nitrogen≤ 0.04%
H Hydrogen≤ 0.015%

Mechanical minima by form

Guaranteed values differ by form, size and delivery condition; quotations confirm the specification, form, size and condition.

FormCondition Rm MPaRp0.2 MPaA ≥ %
Bar, wire, forgings and flash-welded rings (section ≤25.40 mm)Supplied annealed; capability values on specimens solution treated at 899 ± 14 °C for 60 min, water quenched, then aged at 538 ± 8 °C for 4 h, air cooled ≥ 1207 (175 ksi) ≥ 1103 (160 ksi) ≥ 8
Bar, wire, forgings and flash-welded rings (>25.40–50.80 mm)Values to be met after solution treatment and ageing ≥ 1172 (170 ksi) ≥ 1069 (155 ksi) ≥ 8
Bar, wire, forgings and flash-welded rings (>50.80–76.20 mm)Values to be met after solution treatment and ageing ≥ 1069 (155 ksi) ≥ 1000 (145 ksi) ≥ 8
Bar, wire, forgings and flash-welded rings (>76.20–101.60 mm)Values to be met after solution treatment and ageing ≥ 1034 (150 ksi) ≥ 965 (140 ksi) ≥ 8
Annealed bar, wire, forgings and flash-welded rings (section ≤50.80 mm)Annealed at 704-788 °C × 1-2 h, accepted in the as-delivered condition ≥ 1034 (150 ksi) ≥ 965 (140 ksi) ≥ 10
Annealed bar, wire, forgings and flash-welded rings (>50.80–101.60 mm)Annealed at 704-788 °C × 1-2 h, accepted in the as-delivered condition ≥ 1000 (145 ksi) ≥ 931 (135 ksi) ≥ 10

Where this grade is recommended

Matched in 1 service conditions; ranks and scores computed from the condition-scoring matrix.

Service conditionIndustry TemperatureRankScore
Airframe & lightweight Aerospace 200 – 400 °C 1 / 10 87

Designations & equivalents

UNSR56620
Trade name(s)Ti-6Al-6V-2Sn
AMS (SAE aerospace)4971 / 4978

Cross-references are common near-equivalents for search and shortlisting; substitution across standards requires clause-by-clause verification. All grades in one cross-reference table →

Applicable standards

2 specifications. Name the standard and its edition on the order.

Guaranteed values and required tests differ between specifications — see Mechanical minima by form for the figures per form.

Frequently asked questions

What is TC10 (Ti-6Al-6V-2Sn)?

TC10 (Ti-6Al-6V-2Sn) — Titanium. High-strength structural forgings — wing joints and fittings

What is the maximum service temperature of TC10?

Typically about 315 °C; the practical limit depends on media, stress and design life — acceptance per the governing standard.

What is the tensile strength of TC10?

The specified minimum tensile strength is 1207 MPa for the main product form. Minima for other forms and sizes are listed under "Mechanical minima by form" on this page.

Which standards cover TC10?

SAE AMS4971 Ti-6Al-6V-2Sn, SAE AMS4978 Ti-6Al-6V-2Sn

Where is TC10 typically used?

Airframe & lightweight (Aerospace)

In which forms is TC10 available?

Tube, plate, strip, bar, forgings, wire and other forms — sizes and delivery condition confirmed per order, with EN 10204 3.1 / 3.2 certification.

Same series

Download PDF datasheet

This grade’s datasheet as an A4 PDF — for filing, printing or forwarding to colleagues.

Download PDF datasheet

Supply & enquiry

Tube & pipeφ1 – 219 × 0.25 – 25 mmPlate4.76 – 80 mmBarφ8 – 300 mmWire & filler metalsφ0.01 – 8 mm

For this grade we can supply, against your service conditions:

Or email us: info@kochlin.com