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Viewing 121 to 150 of 10049
CURRENT
2017-06-08
Standard
AS7109/6B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/6. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/6. Cancelled specifications are available from SAE.
CURRENT
2017-06-07
Standard
J811_201706
This SAE Information Report covers applications of mechanical prestressing, improving fatigue resistance, theory of surface rolling for fatigue improvement, calculations for the surface rolling process, tooling for surface rolling, control and inspection, effect of surface rolling on properties other than fatigue, and other methods for mechanical prestressing.
2017-06-06
WIP Standard
GA-E17AB
General Agreement to give guidance on utility of previous revision material in stock.
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
2017-06-01
Standard
AMS7510/2C
This specification covers one type of samarium-cobalt permanent magnets.
CURRENT
2017-06-01
Standard
AMS5357D
This specification covers a corrosion-resistant steel in the form of investment castings.
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
AMS4021H
This specification covers an alclad aluminum alloy in the form of sheet and plate.
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.

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.
CURRENT
2017-05-30
Standard
AMS4009C
This specification covers an aluminum alloy in the form of foil.
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
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
AMS4425D
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-05-25
Standard
AMS6529D
This specification covers a special aircraft-quality, low-alloy steel in the form of bars.
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
AMS4420P
This specification covers a magnesium alloy in the form of sand castings.
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
AMS4631F
This specification covers one type of aluminum bronze in the form of rods, bars, forgings, and forging stock.
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.
CURRENT
2017-05-24
Standard
AIR5742A
The scope of this document is related to the particular needs of oxygen equipment with regards to packaging and transportation. The document provides guidance for handling chemical, gaseous and liquid oxygen equipment. It summarizes national and international regulations to be taken into account for transportation on land, sea and air and provides information on classification of hazardous material. The aim of this document is to summarize information on packaging and transportation of oxygen equipment. Statements and references to regulations cited herein are for information only and should not be considered as interpretation of a law. Processes to maintain cleanliness of components and subassemblies during processing and assembly or storage of work-in-progress are outside the scope of this document. Guidance on this can be obtained from ARP1176.
CURRENT
2017-05-22
Standard
AMS4302C
This specification covers an aluminum alloy in the form of sheet laminated with one or more layers of unidirectional aramid fiber/epoxy prepreg.
CURRENT
2017-05-19
Standard
AMS4444E
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-05-18
Standard
AIR6130A
14-day material test to determine the cyclic effects of runway deicing compounds on cadmium plated parts.
Viewing 121 to 150 of 10049