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Standard

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate, 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti, Consumable Electrode or Vacuum Induction Melted, 1800 °F (982 °C) Solution Heat Treated

2018-09-25
WIP
AMS5605G
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate 1.00 inch (25.4 mm) and under in nominal thickness. These products have been used typically for parts requiring good machinability and high strength at room and cryogenic temperatures and for short-time use up to 1000 degrees F (538 degrees C), particularly for those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.
Standard

Nickel Alloy, Corrosion and Heat Resistant, Sheet and Strip 73Ni - 15.5Cr - 2.4Ti - 0.7Al - 7.0Fe Annealed

2018-09-25
WIP
AMS5541H
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet and strip.

These products have been used typically for parts requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Standard

Nickel Alloy, Corrosion and Heat-Resistant Sheet, Strip, and Foil, Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W, Vacuum Induction Melted and Consumable Electrode Remelted, Solution Heat Treated

2018-09-25
WIP
AMS5960A
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil. These products have been used typically for parts requiring resistance to creep and stress-rupture up to 1400 °F (760 °C) and oxidation resistance up to 1800 °F (982 °C), particularly those parts which are formed or welded and then precipitation heat treated to develop desired properties, but usage is not limited to such applications.
Standard

Aircraft Compartment Automatic Temperature Control Systems

2018-09-24
WIP
ARP89E
The recommendations of this SAE Aerospace Recommended Practice (ARP) for aircraft compartment automatic temperature control systems are primarily intended to be applicable to occupied or unoccupied compartments of civil and military aircraft.
Standard

Aircraft Tire Selection and Qualification

2018-09-21
WIP
ARP6822
This document is to provide a general understanding of aircraft tire constructions and characteristics and how they relate to the decision-making process in selecting a tire. In addition, guidance on qualification requirements is addressed.
Standard

Generic Open Architecture (GOA) Framework

2018-09-21
CURRENT
AS4893A
This SAE Aerospace Standard (AS) establishes a Generic Open Architecture (GOA) Framework for application independent hardware/software systems. This document defines the interface classes for the GOA Framework. Supplemental documents define the guidelines for applying the GOA Framework to specific applications.
Standard

Phosphate Treatment, Paint Base

2018-09-20
WIP
AMS2480J
This specification covers the requirements for producing a zinc phosphate coating on ferrous alloys and the properties of the coating. This process has been used typically to produce a coating that will ensure satisfactory paint adherence, but usage is not limited to such applications.
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