Refine Your Search

Search Results

Standard

Nickel Alloy, Corrosion and Heat Resistant, Bars and Wire 52.5Ni 19Cr 3.0Mo 5.1Cb 0.90Ti 0.50Al 19Fe Consumable Electrode or Vacuum Induction Melted 1775°F (968°FC) Solution Treated and Cold Worked Precipitation Hardenable

2018-04-12
WIP
AMS5962B
This specification covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire, 1 1/2 inches (38 mm) and under in nomial diameter.

These products have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 220 ksi (1517 MPa) after precipitation heat treatement for use up to 900 °F (482 °C) and having oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications.

Standard

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 72Ni 15.5Cr 7.0Fe 2.5Ti 1.0(Cb + Ta) 0.70Al, 2100°F (1149°C) Solution and Precipitation Heat Treated

2018-04-12
WIP
AMS5668K
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as bolts, turbine blades, and turbine seals, requiring oxidation resistance and high strength at 1250 to 1500 degrees F (675 to 816 degrees C), but usage is not limited to such applications.
Standard

Age Control of Age Sensitive Elastomeric Materials

2018-04-11
CURRENT
AIR1364B
This SAE Aerospace Information Report (AIR) summarizes data and background relative to age control of specific classes of those nitrile type synthetic elastomers used in sealing devices which are resistant to petroleum base hydraulic fluids, lubricating oils, and aircraft fuels. This includes, but is not limited to, those nitrile (NBR or BUNA-N) elastomers previously covered by Section I of MIL-STD-1523.
Standard

Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged (Composition similar to UNS AA6156)

2018-04-10
CURRENT
AMS4405C
1.1 Form This specification covers an aluminum alloy procured in the form of sheet 0.078 to 0.197 inch (2.00 to 5.00 mm), inclusive, in nominal thickness, Alclad on both sides (see 8.5). 1.2 Application These products have been used typically for formed structural parts requiring good formability in T4 temper and ability to develop improved resistance to fatigue crack growth and high toughness with moderate strength when aged to T62 temper, but usage is not limited to such applications.
X