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Standard

Core, Flexible Honeycomb, Aluminum Alloy, Treated for Sandwich Construction, 5052, 350 (177)

1990-01-01
HISTORICAL
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.
Standard

Castings Lead Alloy, 6.5sb 0.5sn

1990-01-01
CURRENT
AMS7720A
This specification has been CANCELLED by the Aerospace Materials Division, SAE, as of January, 1990. By this action, the subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications.
Standard

Polyimide Printed Circuit Boards Fabrication of

1990-01-01
CURRENT
ARP1612A
This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multilayer boards.
Standard

Tolerances, Metric, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire

1990-01-01
HISTORICAL
MAM2261A
This specification covers established metric manufacturing tolerances applicable to bars, rods, and wire of nickel, nickel alloys, and cobalt alloys ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range.
Standard

Tolerances, Corrosion and Heat Resistant Steel, Tubing

1990-01-01
HISTORICAL
AMS2243G
This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat resistant steel ordered to inch dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID).
Standard

Compound, Solid Runway and Taxiway Deicing/Anti-Icing

1990-01-01
HISTORICAL
AMS1431
This specification covers a deicing and anti-icing compound in the form of a solid. This compound are intended for use at airports on aircraft maneuvering areas, such as aprons, runways, and taxiways, for the prevention and removal of frozen deposits of snow, frost, and ice..
Standard

Adhesive, Urethane Two-Part

1990-01-01
HISTORICAL
AMS3139A
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
Standard

Aluminum Alloy Tempers

1990-01-01
HISTORICAL
AS1990
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

Steel, Corrosion Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu, Consumable Remelted, Precipitation Hardenable

1990-01-01
HISTORICAL
AMS5659G
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, extrusions, and stock for forging, flash welded rings, or extruding. These products have been used typically for parts requiring corrosion resistance and high strength up to 600 °F (316 °C) with good ductility and strength in the transverse direction in large section sizes, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions.
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