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Standard

Decarburization in Hardened and Tempered Unified Threaded Fasteners

1996-05-01
HISTORICAL
J121_199605
This SAE Recommended Practice covers methods for measuring, classifying, and specifying decarburization in the threaded section of hardened and tempered steel bolts, screws, studs, and similar parts. It is not intended to cover products which are specifically carburized to achieve special properties.
Standard

School Bus Stop Arm

1996-05-01
HISTORICAL
J1133_199605
This document provides test procedures, requirements, and guidelines for school bus stop arms.
Standard

Aluminum Alloy, Welding Wire, 6.3Cu - 0.30Mn - 0.18Zr - 0.15Ti - 0.10V (2319)

1996-05-01
HISTORICAL
AMS4191E
This specification covers an aluminum alloy in the form of welding wire. This wire has been used typically as filler metal for gas-metal-arc or gas-tungsten-arc welding of aluminum alloys of similar composition where the joint is capable of being heat treated to a strength level comparable to that of the parent metal, but usage is not limited to such applications.
Standard

Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 17Cr 12Ni 2.5Mo, Solution Heat Treated

1996-05-01
HISTORICAL
AMS5648
This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring corrosion and heat resistance up to 1600 degrees F (871 degrees C), but usage is not limited to such applications. At comparable elevated temperatures, strength of this steel is slightly higher than, and oxidation resistance is similar to, the 18-8 type steels. Alloy: 30316 UNS Number: S31600
Standard

Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0al 4.0v Solution Heat Treated and Aged

1996-05-01
HISTORICAL
AMS4965G
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging and flash welded rings. These products have been used typically for parts which are machined after solution and precipitation heat treatment and aging and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, but usage is not limited to such applications.
Standard

Horsepower Correction Formulae

1996-05-01
HISTORICAL
ARP2B
This document discusses formulae considered applicable to aircraft engines having integral supercharging without aftercooling, and using gasoline introduced at the entrance to the supercharger or directly into the cylinders. Such engines are normally designated as single and two speed engines. Correction formulae for engines having two stage or exhaust turbo supercharging will not be discussed. Corrections for engines having a high degree of integral supercharging will be discussed in general terms only and no specific formulae will be presented. The correction formulae and methods listed are empirical and subject to error due to conditions beyond the scope of known corrections. Usage has indicated, however, that the correction formulae listed will provide a satisfactory approximation of power output under standard conditions.
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