Search
Advanced Search
of the following are true

Results

Items (207,314)
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990
AMS P17 Polymer Matrix Composites Committee
Alloy: L-605 UNS Number: R30605
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 10/17/90. Use AMS 7276 or 7280
AMS CE Elastomers Committee
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of Januray 1990
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system
AMS G9 Aerospace Sealing Committee
This specification covers a fuel and low-temperature resistant butadiene-acrylonitrile (NBR) rubber in the form of molded rings
AMS CE Elastomers Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.1874 inch (4.76 mm) and under in nominal thickness
AMS F Corrosion and Heat Resistant Alloys Committee
AMS3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 120 °C (250 °F) vacuum curing. The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests
AMS CACRC Commercial Aircraft Composite Repair Committee
The PS, AMS3970/3, specifies the batch release and delivery requirements for carbon fiber fabric epoxy prepreg used for repair
AMS CACRC Commercial Aircraft Composite Repair Committee
AMS F Corrosion and Heat Resistant Alloys Committee
AMS F Corrosion and Heat Resistant Alloys Committee
AMS F Corrosion and Heat Resistant Alloys Committee
No scope available
AMS E Carbon and Low Alloy Steels Committee
Parts, such as bolts, turbine wheels, discs, buckets, and blades, for high strength and oxidation resistance up to 1500 F when suitably heat treated
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers chrome-molybdenum alloy 4130, steel sheet, strip, and plate of thickness to and including 1.50 inches
AMS E Carbon and Low Alloy Steels Committee
This specification covers corrosion-resistant, heat treatable steel in sheet and strip form (see 6.3), of the compositions and conditions indicated
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers low-carbon steel, sheet or strip, of aircraft quality
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft quality, chrome-vanadium (6150) steel bars and forging stock
AMS E Carbon and Low Alloy Steels Committee
Items per page:
1 – 50 of 207314