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Viewing 1 to 30 of 2915
2011-07-27
Magazine
Material matters While new airplane designs now entering service will use more carbon-fiber composites than ever, it is no time to count out aluminum, as promising new versions of alloys such as aluminum-lithium gain ground.
HISTORICAL
1942-03-01
Standard
AMS5025
2017-05-02
WIP Standard
AMS4134G
This specification covers an aluminum alloy in the form of die forgings and forging stock.
CURRENT
2012-01-06
Standard
AMS4134F
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
1997-01-01
Standard
AMS4134D
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
2006-05-17
Standard
AMS4134E
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
1976-07-01
Standard
AMS4134B
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
1945-10-01
Standard
AMS4134
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
1984-01-01
Standard
AMS4134C
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
1952-02-01
Standard
AMS4134A
This specification covers an aluminum alloy in the form of die forgings and forging stock.
HISTORICAL
2002-01-16
Standard
AMS4195C
This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 inch (12.70 mm) and under in nominal thickness.
HISTORICAL
1989-01-01
Standard
AMS4195B
This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 inch (12.70 mm) and under in nominal thickness.
HISTORICAL
1983-01-01
Standard
AMS4195A
This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 in. (12.50 mm) and under in nominal thickness.
HISTORICAL
1970-11-01
Standard
AMS4195
This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 inch (12.70 mm) and under in nominal thickness.
2017-05-05
WIP Standard
AMS4178F
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.
CURRENT
2008-10-21
Standard
AMS4178E
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form.
HISTORICAL
2006-09-14
Standard
AMS4178D
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form.
HISTORICAL
1995-11-01
Standard
AMS4178C
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form.
HISTORICAL
1990-01-01
Standard
AMS4178B
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.
HISTORICAL
1976-01-01
Standard
AMS4178
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.
HISTORICAL
1983-01-01
Standard
AMS4178A
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.
HISTORICAL
1970-11-01
Standard
AMS4176
This specification covers one type of honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered.
CURRENT
2001-11-28
Standard
AMS4175C
This specification covers one type of honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered.
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