Event
AMS Metals Group Committee Meetings
2025-03-17
Search Results
Event
AMS Metals Group Committee Meetings
2024-09-16
Event
Aerospace Metals and Engineering Committee
2024-07-09
Technical Paper
Elastomeric Swaging Finite Element Analysis Methodology to Evaluate Structural Integrity of Internal Swaged Joints
2024-06-01
2024-26-0428
In applications demanding high performance under extreme conditions of pressure and temperature, a range of Mechanically Attached Fittings (MAFs) is offered by various Multinational Corporations (MNCs). These engineered fittings have been innovatively designed to meet the rigorous requirements of the aerospace industry, offering a cost-effective and lightweight alternative to traditional methods such as brazing, welding, or other mechanically attached tube joints. One prominent method employed for attaching these fittings to tubing is through Internal Swaging, a mechanical technique. This process involves the outward formation of rigid tubing into grooves within the fitting. One of the methods with which this intricate operation is achieved is by using a drawbolt - expander assembly within an elastomeric swaging machine.
Standard
Nickel Alloy, Corrosion- and Heat-Resistant Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Solution Heat Treated, Precipitation Hardenable
2024-05-09
CURRENT
AMS5582H
This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness.
Standard
Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of
2024-05-09
CURRENT
ARP1947D
This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa).
Standard
Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form
2024-05-09
CURRENT
AS7250E
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
Standard
Nuts, Self-Locking, UNS N07001 730 °C, 1100 MPa, and 1210 MPa Procurement Specification for, Metric
2024-05-09
CURRENT
MA1943C
This procurement specification covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) types of nuts made from a corrosion and heat-resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Tension height nuts having overall length of threaded portion not less than 1.2 times the nominal thread diameter have 1210 MPa minimum tensile strength at room temperature. Shear height nuts having shorter threaded portion have 1100 MPa minimum tensile strength at room temperature. Maximum test temperature of parts is 730 °C.
Standard
Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized
2024-05-01
CURRENT
AMS4375N
This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.5).
Standard
Magnesium Alloy, Extrusions, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated
2024-05-01
CURRENT
AMS4352K
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 square inches (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.5).
Standard
Copper, Sheet, Strip, and Plate Soft Annealed
2024-05-01
CURRENT
AMS4500L
This specification covers unalloyed copper in the form of sheet, strip, and plate at least 0.015 inch (0.38 mm) in nominal thickness.
Standard
Steel, Corrosion Resistant Bars and Forgings, 12.5Cr - 1.0Ni - 15.5Co - 2.0Mo, Vacuum Induction Plus, Vacuum Consumable Electrode Remelted
2024-04-26
WIP
AMS5933B
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, forgings, and forging stock.
Standard
F23AB/AMS5971 Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 12.25Cr– 2.5Ni – 0.6Mo -- 0.45Ti (<0.13C), Carburizing Aircraft Premium Quality, VIM-VAR or VAR, 190ksi (Composition similar to UNS S41429)
2024-04-26
WIP
F23AB/AMS5971
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
Standard
F23AA/AMS5970 Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 12.25Cr– 2.5Ni – 0.6Mo -- 0.45Ti (<0.13C), Carburizing Aircraft Premium Quality, VIM-VAR or VAR, 170ksi (Composition similar to UNS S41429)
2024-04-26
WIP
F23AA/AMS5970
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock
Standard
Aluminum Alloy, Extruded Profiles (2395-T84), 3.95Cu - 1.15Li - 0.3Ag - 0.5Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and Aged
2024-04-25
CURRENT
AMS4359A
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 1.500 inches (1.02 to 38.10 mm), inclusive, in thickness, and produced with maximum cross-sectional area of 23.25 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 15.5 inches (394 mm) (see 2.4.1 and 8.6).
Standard
Aluminum Alloy, Sheet and Plate, 2.5Mg - 0.25Cr (5052-H32), Strain Hardened, Quarter-Hard, and Stabilized
2024-04-25
CURRENT
AMS4016N
This specification covers an aluminum alloy in the form of sheet and plate 0.017 to 2.000 inches (0.43 to 50.80 mm), inclusive, in nominal thickness (see 8.6).
Standard
Aluminum Alloy Sheet, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T4 Flat Sheet), Solution Heat Treated, High Formability
2024-04-25
CURRENT
AMS4297C
This specification covers an aluminum alloy in the form of sheet 0.020 to 0.128 inch (0.51 to 3.25 mm), inclusive, in nominal thickness (see 8.5).
Standard
Aluminum Alloy, Plate (7160-T7651), 7.0Zn - 2.2Cu - 1.5Mg - 0.10Zr, Solution Heat Treated, Stress Relieved, and Overaged
2024-04-25
CURRENT
AMS4378A
This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inches (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.5).
Standard
Aluminum Alloy, Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T861 Sheet and Plate), Solution Heat Treated, 6% Cold Worked and Artificially Aged
2024-04-25
CURRENT
AMS4467C
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.
Standard
Aluminum Alloy, Coiled Sheet, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024; -T4 Coiled Sheet), Solution Heat Treated
2024-04-25
CURRENT
AMS4475C
This specification covers an aluminum alloy in the form of alclad coiled sheet from 0.010 to 0.128 inch (0.25 to 3.25 mm), inclusive, in thickness supplied in the -T4 temper (see 8.5).
