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Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate

1980-07-01
HISTORICAL
MAM2242
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion and heat resistant steels, iron alloys, titanium, and titanium alloys 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, Corrosion and Heat Resistant Steel Tubing

1980-07-01
HISTORICAL
MAM2243
This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat resistant steel ordered to metric dimension. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID).
Standard

Steel, Corrosion and Heat Resistant, Seamless Tubing, 9.0Mn - 20Cr - 6.5Ni - 0.28N, Solution Heat Treated

1980-07-01
HISTORICAL
AMS5562A
This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts, such as fluid-conducting lines, requiring both corrosion and heat resistance, especially when such parts are welded or brazed during fabrication, and which require strength higher than that of the 18-8 type steels or require oxidation resistance up to 1100 degrees F (593 degrees C), but usage is not limited to such applications.
Standard

Steel, Corrosion Resistant, Sheet and Strip, 17Cr - 7.1Ni - 1.1Al, Solution Heat Treated and Cold Rolled, Precipitation Hardenable, 0.0015 to 0.050 Inch (0.038 to 1.27 mm) Nominal Thickness

1980-07-01
HISTORICAL
AMS5529C
This specification covers a corrosion-resistant steel in the form of sheet and strip 0.0015 to 0.050 inch (0.038 to 1.27 mm) in nominal thickness. These products have been used typically for parts such as springs requiring corrosion resistance and high strength up to 600 °F (316 °C), but usage is not limited to such applications. Strength of these cold-worked products will be impaired if parts are welded during fabrication. ertain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions.
Standard

Cobalt Alloy, Corrosion and Heat-Resistant, Bars, Forgings and Rings, 40Co - 22Cr - 22Ni - 14.5W - 0.07La, Solution Heat Treated

1980-07-01
HISTORICAL
AMS5772A
This specification covers a corrosion and heat resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring high strength up to 1800 degrees F (982 degrees C) and oxidation resistance up to 2000 degrees F (1093 degrees C), but usage is not limited to such applications.
Standard

ENGINE GRAY FINISHING Low Baking

1980-04-15
HISTORICAL
AMS2510D
This specification covers the engineering requirements for finishing aircraft parts and assemblies with an engine gray enamel.
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