Browse Topic: Corrosion

Items (1,468)
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion and heat-resistant steel in the form of bars, forgings, and forging stock. These products have been used typically for parts requiring oxidation resistance and high strength up to 800 °F (427 °C) and where such parts may require welding during fabrication, but usage is not limited to such applications.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness (see 8.7).
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a carbon steel in the form of bars up through 3.000 inches (76.2 mm), forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers bonded honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered.
AMS D Nonferrous Alloys Committee
This specification establishes the requirements for brush plating of cadmium by electrodeposition.
AMS B Finishes Processes and Fluids Committee
Test Publishing Document6667
A-6 Aerospace Actuation, Control and Fluid Power Systems
Corrosion occurs in diverse environments mainly on metallic parts. Helicopters are made of a huge percentage of metallic parts and need to have several maintenance steps to guarantee its functioning and its durability. The military helicopters are flying in different kinds of environment, which cover large spectrum of severity of the atmospheric corrosion [1]. In maritime conditions, the most influencing factor is the Time of Wetness, which is a direct result Relative Humidity and Salt loading. The main material used for aircraft and that is suffering from corrosion is aluminium. There are plenty of data to follow the corrosion as a function of the environmental conditions, mainly on the sensitivity with sodium chloride, Relative Humidity, film thickness, etc... [2][3]. The maintenance efficiency on helicopters is dependent on the environmental severity. The U.S. armed forces estimate $10.2 billion in corrosion costs for their aviation and missile fleets during 2016 [4] [5] [6]. The aim of the present analysis consists of defining the Condition Based Maintenance related to corrosion risk to better apply a maintenance program when it is really needed.
Sinopoli, Davidmiranda dias, PATRICIADEVILLIERS, GEORGES
ABSTRACT
Restis, JudeKokaly, MatthewDubberly,  MichaelManning, Dale
ABSTRACT
Sugiura, MasahikoKimura, KeitaOyama, AkiraSugawara, HideakiTanabe, YasutadaMinajima, TakumaMinajima, TakumaKanazaki, MasahiroKishi, YukiKikuchi, DaisukeSato, MakotoYoshikawa, KotaButo, Yuta
This specification covers adhesion promoters in liquid form for use with aerospace sealing compounds.
AMS G9 Aerospace Sealing Committee
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate 0.0010 inch (0.025 mm) and above in nominal thickness (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to components made of ferrous and non-ferrous alloys. The recommendations in this document do not apply to components made of non metallic composite materials.
A-5B Gears, Struts and Couplings Committee NEW Name Goes Her
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, foil, and plate 0.0015 inch (0.038 mm) and greater in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an iron-nickel alloy in the form of strip.
AMS F Corrosion Heat Resistant Alloys Committee
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs.
AMS G8 Aerospace Organic Coatings Committee
ABSTRACT
Otto, MassimilianoTaylor, MaxEhlinger,  JoshImig,  Jeff
This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1).
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) in nominal thickness (see 8.7).
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes.
AMS G Titanium and Refractory Metals Committee
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.
AMS G Titanium and Refractory Metals Committee
This specification covers an aluminum alloy in the form of hand forgings up to 6 inches (152 mm) inclusive, in nominal as-forged thickness and having a cross-sectional area of not more than 156 square inches (1006 cm2) (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.015 to 1.5 inches (0.38 to 38 mm) in nominal thickness (see 8.5).
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers an aluminum bronze alloy in the form of bars, rods, forgings, and forging stock.
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers a premium aircraft-quality maraging steel in the form of bars 0.50 inch (12.7 mm) and over in nominal diameter or least distance between parallel sides, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with nominal thickness up to 3.000 inch (76.20 mm), inclusive, and having a cross sectional area of 42 square inches (271 square centimeters) maximum and a circumscribing circle diameter (circle size) of 15 inches (38 cm) maximum (see 8.9). See 8.3 for definition of circumscribing circle size.
AMS D Nonferrous Alloys Committee
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