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2014-12-23
Standard
AMS5010L
This specification covers a free-machining carbon steel in the form of bars.
2014-12-23
Standard
AMS4347D
This specification covers an aluminum alloy in the form of sheet from 0.020 to 0.249 inch (0.51 to 6.32 mm), inclusive, in thickness (See 8.5).
2014-12-22
Article
New adjustable angle heads from BENZ help manufacturers improve their machining and milling operations by enhancing productivity and efficiency.
2014-12-22
Standard
AMS4366
This specification covers an aluminum-lithium alloy in the form of extruded profiles with a maximum cross-sectional area of 19 square inches (123 cm 2 ) and a maximum circle size of 11 inches (279mm) from 0.040 to 0.499 inches (1.00 to 12.50 mm) in thickness.
2014-12-22
Standard
AMS4353
This specification covers an aluminum alloy in the form of extruded round rods. This specification covers products from 1.750 to 5.900 inches (44.45 to 150.00 mm) in diameter.
2014-12-22
Standard
AMS4141G
This specification covers an aluminum alloy in the form of die forgings and forging stock ordered to inch/pound units. These forgings have been used typically for parts requiring good resistance to stress-corrosion cracking but with lower strength than AMS4126, but usage is not limited to such applications.
2014-12-22
Standard
AMS4050J
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for parts requiring a high level of mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.
2014-12-22
Standard
AMS4113F
This specification covers an aluminum alloy in the form of extruded profiles such as angles, channels, tees, zees, I-beams, and H-beams. These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications.
2014-12-21
WIP Standard
AMS4371B
This specification covers a magnesium alloy in the form of rolled plate. This product has been used typically for parts requiring a combination of light weight, high yield strength up to 480 °F (250 °C), relatively high corrosion resistance, and good flammability resistance for magnesium alloys,but usage is not limited to such applications.
2014-12-17
Article
At any one time, up to 80 new steel grades are under development at ArcelorMittal. The person responsible for these advanced-development activities is Greg Ludkovsky, Vice President of Global R&D. Ludkovsky spoke with Automotive Engineering this fall at the AM/NS Calvert plant in Alabama, which the company touts as “the world’s most advanced steel finishing facility.”
2014-12-16
Article
Interest in automated guided vehicles to convey product from one station to another on the plant floor assembly line continues to grow as manufacturers look for greater flexibility, scalability, and sustainability in their operations, says RedViking.
2014-12-12
Article
Al-Fe Heat Treating adds glycol quenching to its aluminum heat treat services.
2014-12-12
Standard
AS755F
This SAE Aerospace Standard (AS) provides a performance station designation system for aircraft propulsion systems and their derivatives. The station numbering conventions presented herein are for use in all communications concerning propulsion system performance such as computer programs, data reduction, design activities, and published documents. They are intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. The contents of this document were previously a subset of AS755E. Due to the growing complexity of station numbering schemes and an industry desire to expand nomenclature descriptions, a decision was made to separate the “station numbering” and “nomenclature” contents of AS755 into two separate documents. AS755 will continue to maintain standards for station numbering. SAE Aerospace Standard AS6502 will maintain standards for classical nomenclature moving forward.
2014-12-11
Standard
AMS4140K
This specification covers an aluminum alloy in the form of die forgings and forging stock.
2014-12-11
Standard
AMS5675H
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
2014-12-11
Standard
AMS4111E
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
2014-12-11
Standard
AMS5629/H1000
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, and extrusions in the solution and precipitation heat treated (H1000) condition. These products have been used typically for parts requiring corrosion resistance, stress-corrosion resistance, high strength up to 600 °F (316 °C), and good ductility and strength in the transverse direction in large section sizes, but usage is not limited to such applications.
2014-12-11
Standard
AMS4783G
This specification covers a cobalt alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of powder in a suitable binder. This filler metal has been used typically for joining cobalt alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications.
2014-12-11
Standard
AMS5544K
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
2014-12-08
Standard
MA3433A
SCOPE IS UNAVAILABLE.
2014-12-05
WIP Standard
AIR1869D
This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft. This document brings together data concerning the lower deck capacity of wide-body and standard- body airplanes. The information includes airplanes manufactured by Airbus, Boeing, British Aerospace, British Aircraft, Fokker-VFW, Hawker Siddeley, Ilyushin, Lockheed and McDonnell- Douglas.
2014-12-05
Standard
AIR5444A
This SAE Aerospace Information Report (AIR) shall be limited to general information about tin whisker formation on tin plated conductors. It summarizes the mechanisms of metal whisker formation and describes possible conclusions as related to tin plated conductors. It also provides a number of reference documents that describes research and observations of the whisker phenomena, recommendations to prevent its formation and conclusions. The investigation by this task group of AE-8D was initiated by a request of the Naval Air Warfare Center, Indianapolis, Indiana, to determine if the phenomenon of tine whiskers is a problem in aerospace wire and cable.
2014-12-03
Article
SAE International’s new book, Counterfeit Electronic Parts and Their Impact on Supply Chains, examines how counterfeit parts are negatively affecting the aviation, spacecraft, and defense sectors and what can be done about it.
2014-12-01
Article
Dry drilling of composite-Ti stack-ups via CO2 avoids the problems associated with liquid coolants used in fuselage hole drilling, while delivering benefits in productivity, tool life, and hole quality.
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