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Tolerances, Metric, Titanium and Titanium Alloy Tubing

2003-03-12
HISTORICAL
MAM2244B
This specification covers established metric manufacturing tolerances applicable to titanium and titanium alloy tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Tubing

1994-04-01
HISTORICAL
MAM2244A
This specification covers established metric manufacturing tolerances applicable to titanium and titanium alloy tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Tubing

1983-01-01
HISTORICAL
MAM2245
This specification covers established manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Extruded Bars, Rods, and Shapes

2003-03-12
HISTORICAL
MAM2245B
This specification covers established metric manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Tubing

2007-08-24
CURRENT
MAM2245C
This specification covers established manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Tubing

2007-07-19
CURRENT
MAM2244C
This specification covers established metric manufacturing tolerances applicable to titanium and titanium alloy tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of the specified range.
Standard

Tolerances, Metric, Titanium and Titanium Alloy Extruded Bars, Rods, and Shapes

1994-04-01
HISTORICAL
MAM2245A
This specification covers established metric manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed

1994-06-01
HISTORICAL
MAM4911A
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP 982 recommends practices to minimize such conditions.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed

2003-03-12
CURRENT
MAM4911B
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP 982 recommends practices to minimize such conditions.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed

1988-04-01
HISTORICAL
MAM4911
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP 982 recommends practices to minimize such conditions.
Standard

Tolerances Titanium and Titanium Alloy Extruded Bars, Rods, and Shapes

1983-01-01
HISTORICAL
AMS2245A
This specification covers established inch/pound manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term “excl” applies only to the higher figure of the specified range.
Standard

TOLERANCES Titanium and Titanium-Base Alloy Extruded Bars, Rods, and Shapes

1973-12-01
HISTORICAL
AMS2245
This specification covers established manufacturing tolerances applicable to titanium and titanium-base alloy extruded bars, rods, and shapes. These tolerances apply to all conditions, unless otherwise noted. The term “excl” applies only to the higher figure of the specified range.
Standard

Tolerances Titanium and Titanium Alloy Extruded Bars, Rods, and Shapes

2003-06-16
CURRENT
AMS2245B
This specification covers established manufacturing tolerances applicable to titanium and titanium alloy extruded bars, rods, and shapes. These tolerances apply to all conditions, unless otherwise noted. The term “excl” applies only to the higher figure of the specified range.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 13.5v 11cr 3.0al, Solution Heat Treated

1994-04-01
HISTORICAL
AMS4917E
This specification covers a titanium alloy in the form of sheet, strip, and plate. Primarily for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated. Suitable for parts, such as pressure vessels and aircraft structures, requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C). This alloy may have poor crack propagation resistance in the precipitation heat treated condition. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.
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