SAE AMS 4912 : NONCURRENT
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SHEET AND STRIP, 4A1 3MO 1V, SOLUTION HEAT TREATED
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SAE AMS 5525 : 2012
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STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED
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SAE AMS 4911 : 2014
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TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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SAE AMS 5599 : 2016
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NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED
|
SAE AMS 5512 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 10.5NI - 0.80CB (SAE 30347), SOLUTION HEAT TREATED
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SAE AMS 5542 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED
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SAE AMS 5595 : 2014
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STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 9.0MN - 20CR - 6.5NI - 0.28N, SOLUTION HEAT TREATED
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SAE AMS 5526 : 1989
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STEEL SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT, 19.5CR - 9.5NI - 1.4MO - 1.4W - 0.42(CB+TA) - 0.22TI, SOLUTION HEAT TREATED
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SAE AMS 5510S : 2014
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STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 18CR - 10.5NI - 0.40TI (SAE 30321) SOLUTION HEAT TREATED
|
SAE AMS 5603 : 2001
|
SHEET AND STRIP-15CR 8.4NI 2.2MO 1.1AL, VAC. INDUCT. MELTED, SOLUTION HEAT TREATED
|
MIL W 27664 : NOTICE 1
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WELDING, SPOT, INERT-GAS SHIELDED ARC
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SAE AMS 4910 : 2017
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED
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SAE AMS 5545 : 2010
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NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 54NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.5AL - 0.006B, VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATABLE, PRECIPITATION HEAT TREATED
|
SAE AMS 5548 : 2012
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STEEL, CORROSION AND HEAT-RESISTANT, SHEET AND STRIP, 16.5CR - 4.5NI - 2.9MO - 0.10N, 1850 TO 1975 DEGREES F (1010 TO 1079 DEGREES C) ANNEALED
|
MIL-W-8611 Revision A:1957
|
WELDING, METAL ARC AND GAS STEELS AND CORROSION AND HEAT RESISTANT ALLOYS PROCESS FOR
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SAE AMS 5528 : 2012
|
STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 17CR - 7.1NI - 1.1AL, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE
|
MIL-W-6858 Revision D:1978
|
WELDING RESISTANCE, SPOT AND SEAM
|
SAE AMS 4916 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED
|
SAE AMS 5596 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED
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SAE AMS 4901 : 2015
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA)
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SAE AMS 4900 : 2014
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH
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