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Viewing 61 to 90 of 20308
CURRENT
2017-06-05
Standard
AMS4966R
This specification covers a titanium alloy in the form of forgings and forging stock. These forgings have been used typically for parts requiring strength up to 800 °F (427 °C) and that may be welded during fabrication, but usage is not limited to such applications.
CURRENT
2017-06-05
Standard
AMS5802E
This specification covers a corrosion and heat-resistant iron-nickel alloy in the form of welding wire.
CURRENT
2017-06-05
Standard
AMS7445E
This specification covers balls made of high-carbon corrosion-resistant steel of three carbon ranges.

These products have been used typically for bearing balls, but usage is not limited to such applications.

CURRENT
2017-06-05
Standard
AS14227D
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-05
Standard
AS5620B
This SAE Aerospace Standard (AS) shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for Ti-3Al-2.5V cold worked and stress relieved hydraulic system tubing. The basic tubing shall comply with the requirements of AMS 4946.
2017-06-01
WIP Standard
AMS4368
This new draft specification is for an aluminum material hot isostatically pressed from 6061B aluminum powder, each powder particle discontinuously reinforced with silicon carbide particulate.
CURRENT
2017-06-01
Standard
AMS5357D
This specification covers a corrosion-resistant steel in the form of investment castings.
CURRENT
2017-06-01
Standard
AMS1548B
This specification covers a solvent-emulsion cleaner in the form of a solvent-base liquid concentrate.
CURRENT
2017-06-01
Standard
AMS7510/2C
This specification covers one type of samarium-cobalt permanent magnets.
CURRENT
2017-06-01
Standard
AS1005H
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-01
Standard
AS20218B
SCOPE IS UNAVAILABLE.
CURRENT
2017-05-31
Standard
AMS7510C
This specification and its supplementary detail specifications cover commonly-available rare-earth/cobalt permanent magnets produced by powder metallurgy.
CURRENT
2017-05-30
Standard
AMS4009C
This specification covers an aluminum alloy in the form of foil.
CURRENT
2017-05-30
Standard
AMS4021H
This specification covers an alclad aluminum alloy in the form of sheet and plate.
CURRENT
2017-05-30
Standard
AMS4416B
This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness (see 8.5).
CURRENT
2017-05-30
Standard
AMS4490K
This specification covers a magnesium alloy in the form of die castings.
2017-05-30
WIP Standard
AMS4478A
This specification covers an aluminum alloy in the form of Alclad sheet and plate supplied in the –T81/-T851 temper. These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum corrosion resistance and whose fabrication does not involve welding, but usage is not limited to such applications.
2017-05-30
WIP Standard
AMS4467B

This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.

2017-05-26
WIP Standard
ARP4977A
This SAE Aerospace Recommended Practice (ARP) describes standard methods for drying commercial aircraft composite structures prior to repair and gives general guidelines on use and applicability. It addresses the removal of liquids that have collected inside the structures through open damage, microcracks, or porosity and the removal of absorbed moisture from the composite material. The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the original equipment manufacturer (OEM) or regulatory authority. If this document is used for the drying of materials other than thermosetting composite materials, the fitness for this purpose must be determined by the user. The purpose of this document is to provide a set of standard drying methods that may be referenced in repair documents produced by airlines or airframe and engine manufacturers.
CURRENT
2017-05-25
Standard
AMS4148F
This specification covers an aluminum alloy in the form of die forgings and forging stock.
CURRENT
2017-05-25
Standard
AMS4266B
This specification covers an aluminum alloy powder metallurgy product in the form of sheet 0.010 to 0.250 inch (0.25 to 6.35 mm) in nominal thickness.

This sheet has been used typically for parts requiring a combination of intermediate strength, high modulus, and thermal stability up to 750 degrees F (399 degrees C), but usage is not limited to such applications.

CURRENT
2017-05-25
Standard
AMS4254C
This specification covers aluminum alloy sheet laminated with one or more layers of unidirectional aramid fiber/epoxy prepreg. The outer layers are always aluminum alloy.
CURRENT
2017-05-25
Standard
AMS4258B
This specification covers an aluminum alloy in the form of sheet laminated with two or more layers of unidirectional aramid fiber/epoxy prepreg.
CURRENT
2017-05-25
Standard
AMS4036L
This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.
CURRENT
2017-05-25
Standard
AMS4420P
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-05-25
Standard
AMS4425D
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-05-25
Standard
AMS4631F
This specification covers one type of aluminum bronze in the form of rods, bars, forgings, and forging stock.
CURRENT
2017-05-25
Standard
AMS3213M
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for parts, such as gaskets, diaphragms, bushings, grommets, and sleeves, requiring resistance to aromatic and aliphatic fuels when continuously or alternately exposed to both.
CURRENT
2017-05-25
Standard
AMS6529D
This specification covers a special aircraft-quality, low-alloy steel in the form of bars.
CURRENT
2017-05-24
Standard
AMS6950
This specification covers a titanium alloy in the form of bars and forgings 14.000 inches (355.60 mm) and under in nominal diameter or least distance between parallel sides and stock for forging.
Viewing 61 to 90 of 20308