TITAN GRADE 5 Aero can be cold drawn and extruded, although the cold workability is somewhat limited. Cold forming is sometimes used for parts such as brackets and clips. Due to the low modulus of titanium, springback is an issue in roomtemperature forming. Theoretically, it can be compensated for by over-bending; however, in practice hot sizing is often used to correct for the variability that occurs.
Polishing ability:
Magnetism:
Magnetic Attraction: None
Corrosion resistance:
TITAN GRADE 5 Aero immediately and spontaneously forms a stable, continuous, tightly adherent oxide film upon exposure to oxygen in air or water. This accounts for its excellent corrosion resistance in a variety of media. TITAN GRADE 5 Aero is highly resistant to general corrosion in aqueous solutions including seawater, as well as in oxidizing acids, chlorides (in the presence of water), rocket propellants and alkalis. Conditions under which TITAN GRADE 5 Aero is susceptible to general corrosion are in the presence of reducing acids or dry chlorine gas.
Stresscorrosion cracking (SCC) and crevice corrosion have been shown to occur in environments containing chlorides or other halide ions. For this reason, it is general practice to avoid the use of chlorinated solvents, cutting fluids, etc. in processing titanium.
Titanium and its alloys, including TITAN GRADE 5 Aero, are susceptible to hydrogen embrittlement. Gaseous or cathodic hydrogen can diffuse into the metal, forming brittle hydrides. Thus, it is important to minimize hydrogen pickup during processing, particularly heat treating and acid pickling. Specifications for TITAN GRADE 5 Aero mill products typically specify a maximum hydrogen limit of about 150 ppm.
Uses:
TITAN GRADE 5 Aero may be considered in any application where a combination of high strength at low to moderate temperatures, light weight and excellent corrosion resistance are required. Some of the many applications where this alloy has been used include aircraft turbine engine components, aircraft structural components, aerospace fasteners, high-performance automotive parts, marine applications, medical devices, and sports equipment.
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 7.50mm, Toleranz ISO h6
bars 3m
ground
h 6
621 kg
0
141 125 - 621.400
7-500
bars-3m
ground
h-6-en
6.500
70713006500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 6.50mm, Toleranz ISO h6
bars 3m
ground
h 6
924 kg
0
141 125 - 924.000
6-500
bars-3m
ground
h-6-en
7.000
70713007000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 7.00mm, Toleranz ISO h6
bars 3m
ground
h 6
799 kg
0
141 125 - 799.200
7-000
bars-3m
ground
h-6-en
6.000
70713006000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 6.00 mm, tolerance ISO h6
bars 3m
ground
h 6
807 kg
0
141 125 - 806.500
6-000
bars-3m
ground
h-6-en
8.000
70713008000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 8.00mm, Toleranz ISO h6
bars 3m
ground
h 6
681 kg
0
191 225 - 681.300
8-000
bars-3m
ground
h-6-en
8.500
70713008500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 8.50mm, Toleranz ISO h6
bars 3m
ground
h 6
663 kg
0
191 225 - 663.000
8-500
bars-3m
ground
h-6-en
4.000
70713004000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 4.00 mm, tolerance ISO h6
bars 3m
ground
h 6
768 kg
0
190 226 - 768.167
4-000
bars-3m
ground
h-6-en
9.000
70713009000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 9.00mm, Toleranz ISO h6
bars 3m
ground
h 6
596 kg
0
241 125 - 595.500
9-000
bars-3m
ground
h-6-en
4.500
70713004500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 4.50 mm, tolerance ISO h6
bars 3m
ground
h 6
852 kg
0
160 126 - 851.700
4-500
bars-3m
ground
h-6-en
5.000
70713005000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 5.00 mm, tolerance ISO h6
bars 3m
ground
h 6
844 kg
0
260 226 - 844.000
5-000
bars-3m
ground
h-6-en
9.500
70713009500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 9.50mm, Toleranz ISO h6
bars 3m
ground
h 6
0 kg
0
9-500
bars-3m
ground
h-6-en
10.500
70713010500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 10.50mm, Toleranz ISO h6
bars 3m
ground
h 6
635 kg
0
241 125 - 634.500
10-500
bars-3m
ground
h-6-en
11.500
70713011500
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 11.50mm, Toleranz ISO h6
bars 3m
ground
h 6
687 kg
0
141 125 - 550.600|260 126 - 136.000
11-500
bars-3m
ground
h-6-en
12.000
70713012000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 12.00 mm, Toleranz ISO h6
bars 3m
ground
h 6
743 kg
0
141 125 - 497.000|290 126 - 246.000
12-000
bars-3m
ground
h-6-en
11.000
70713011000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 11.00mm, Toleranz ISO h6
bars 3m
ground
h 6
655 kg
0
241 125 - 655.000
11-000
bars-3m
ground
h-6-en
10.000
70713010000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 10.00mm, Toleranz ISO h6
bars 3m
ground
h 6
595 kg
0
141 125 - 595.100
10-000
bars-3m
ground
h-6-en
9.530
70713009530
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as
per AMS 2631 cl. AA and AMS-STD 2154
diam. 9.53 mm (3/8”), Toleranz ISO h6
bars 3m
ground
h 6
712 kg
0
241 125 - 712.100
9-530
bars-3m
ground
h-6-en
26.000
70713226000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl.
AA and AMS-STD 2154
diam. 26.00 mm, Toleranz ISO h8
bars 3m
ground
h 8
440 kg
0
180 326 - 440.000
26-000
bars-3m
ground
h-8-en
20.000
70713220000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl. AA and AMS-STD 2154
diam. 20.00 mm, Toleranz ISO h8
bars 3m
ground
h 8
473 kg
0
150 626 - 473.000
20-000
bars-3m
ground
h-8-en
25.400
70713225400
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl.
AA and AMS-STD 2154
diam. 25.40 mm (1”), Toleranz ISO h8
bars 3m
ground
h 8
372 kg
0
090 626 - 372.000
25-400
bars-3m
ground
h-8-en
30.000
70713230000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl. AA and AMS-STD 2154
diam. 30.00 mm, Toleranz ISO h9
bars 3m
ground
h 8
474 kg
0
270 526 - 474.000
30-000
bars-3m
ground
h-8-en
30.000
70713235000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl. AA and AMS-STD 2154
diam. 35.00 mm, Toleranz ISO h9
bars 3m
ground
h 8
0 kg
0
30-000
bars-3m
ground
h-8-en
5.500
70713005500
Brief description
Klein designation:
TITAN GRADE 5 Aero
Class of steels:
Material number:
Standard UNS:
RoHS 2 – 2011/65/EU:
Machinability:
Hardening capability:
Forming:
Cold working hardening:
TITAN GRADE 5 Aero can be cold drawn and extruded, although the cold workability is somewhat limited. Cold forming is sometimes used for parts such as brackets and clips. Due to the low modulus of titanium, springback is an issue in roomtemperature forming. Theoretically, it can be compensated for by over-bending; however, in practice hot sizing is often used to correct for the variability that occurs.
Polishing ability:
Magnetism:
Magnetic Attraction: None
Corrosion resistance:
TITAN GRADE 5 Aero immediately and spontaneously forms a stable, continuous, tightly adherent oxide film upon exposure to oxygen in air or water. This accounts for its excellent corrosion resistance in a variety of media. TITAN GRADE 5 Aero is highly resistant to general corrosion in aqueous solutions including seawater, as well as in oxidizing acids, chlorides (in the presence of water), rocket propellants and alkalis. Conditions under which TITAN GRADE 5 Aero is susceptible to general corrosion are in the presence of reducing acids or dry chlorine gas.
Stresscorrosion cracking (SCC) and crevice corrosion have been shown to occur in environments containing chlorides or other halide ions. For this reason, it is general practice to avoid the use of chlorinated solvents, cutting fluids, etc. in processing titanium.
Titanium and its alloys, including TITAN GRADE 5 Aero, are susceptible to hydrogen embrittlement. Gaseous or cathodic hydrogen can diffuse into the metal, forming brittle hydrides. Thus, it is important to minimize hydrogen pickup during processing, particularly heat treating and acid pickling. Specifications for TITAN GRADE 5 Aero mill products typically specify a maximum hydrogen limit of about 150 ppm.
Uses:
TITAN GRADE 5 Aero may be considered in any application where a combination of high strength at low to moderate temperatures, light weight and excellent corrosion resistance are required. Some of the many applications where this alloy has been used include aircraft turbine engine components, aircraft structural components, aerospace fasteners, high-performance automotive parts, marine applications, medical devices, and sports equipment.
bars 3m
ground
h 6
769 kg
0
241 125 - 769.000
5-500
bars-3m
ground
h-6-en
35.000
70713335000
Titan Grade 5 Aero
Ti 6Al 4V as per AMS 4928 and AMS 4967
ASTM B-348 Gr.5, EN2002-1, EN4267
titanium alloy for aeronautical application
annealed ground, stress relieved,
in bars of 3m (+100/0mm)
end of bars: chamfered
100% eddy current crack tested as per AMS 2631 cl. AA and AMS-STD 2154
diam. 35.00 mm, Toleranz ISO h9
Pure titanium undergoes an allotropic transformation from the hexagonal close-packed alpha phase to the body-centered cubic beta phase at a temperature of 882.5°C (1’620.5°F). Alloying elements can act to stabilize either the alpha or beta phase. Through the use of alloying additions, the beta phase can be sufficiently stabilized to coexist with alpha at room temperature. This fact forms the basis for creation of titanium alloys that can be strengthened by heat treating. Titanium alloys are generally classified into three main categories. Alpha alloys, which contain neutral alloying elements (such as Sn) and/or alpha stabilizers (such as Al, O) only and are not heat treatable; Alpha + beta alloys, which generally contain a combination of alpha and beta stabilizers and are heat treatable to various degrees; and Beta alloys, which are metastable
and contain sufficient beta stabilizers (such as Mo, V) to completely retain the beta phase upon quenching, and can be solution treated and aged to achieve significant increases in strength. TITAN GRADE 5 Aero, as an α+β titanium alloy, is among the most widely used titanium materials and accounts for more than 50% of total titanium consumption. The alloy is heat treatable and allows moderate increases in strength.
TITAN GRADE 5 Aero is recommended for use at service temperatures up to approximately 350°C (660°F). TITAN GRADE 5 Aero offers a combination of high strength, light weight, formability and corrosion
resistance which have made it a world standard in aerospace applications.
