Standard
GAF24AF (GAE24AF) Tensile Test Strain Rate Implementation
2024-05-09
WIP
GAF24AF
Update of when to implement a specific strain rate into tensile testing.
Search Results
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
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
Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, 125 ksi (862 MPa) Tensile Strength
2024-05-09
CURRENT
AMS6361H
This specification covers aircraft-quality, low-alloy steel in the form of round, seamless tubing.
Standard
Machine Requalification Considerations for Fusion-Based Metal Additive Manufacturing
2024-05-09
CURRENT
ARP7064
This document defines a recommended practice for addressing metal additive manufacturing (AM) machine requalification for all fusion-based metal AM machines. In general, this applies to powder bed fusion (PBF) and wire- or powder-fed directed energy deposition (DED) technologies. Plasma, electron beam, or lasers are applicable energy source(s).
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
Polytetrafluoroethylene (PTFE) Sheet, Molded, Premium Grade, As Sintered
2024-05-08
WIP
AMS3669H
This specification covers virgin, unfilled polytetrafluoroethylene (PTFE) in the form of sheet, manufactured by compression molding and sintering.
Standard
Polytetrafluoroethylene (PTFE) Moldings, Premium Grade, As Sintered
2024-05-08
WIP
AMS3668F
This specification covers two types of virgin, unfilled polytetrafluoroethylene (PTFE) in the form of molded rods, tubes, and shapes. This specification does not apply to product over 12 inches (305 mm) in length, rods under 0.750 inch (19.05 mm) in diameter, and tubes having wall thickness under 0.500 inch (12.70 mm).
Standard
Polytetrafluoroethylene (PTFE) Moldings, General Purpose Grade, As Sintered
2024-05-06
WIP
AMS3660F
This specification covers virgin, unfilled, polytetrafluoroethylene (PTFE) in the form of molded rods, tubes, and shapes. This specification does not apply to product over 12 inches (305 mm) in dimension parallel to the direction of applied molding pressure, rods under 0.750 inch (19.05 mm) in diameter, and tubes having wall thickness under 0.500 inch (12.70 mm).
Standard
Aircraft Sealant Removal Techniques
2024-05-03
WIP
AIR3270B
This SAE Aerospace Information Report (AIR) provides information on the possible methods of sealant removal. The discussion will focus on the methods of sealant removal and give the strengths and weaknesses of each method.
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
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
Application of AMS3144 Anodic Electrodeposition Primer
2024-05-01
WIP
G824AB
This standard establishes the recommended requirements for application of AMS3144 anodic electrodeposition primer to aerospace components. Adherence to these requirements will help facilitate satisfactory performance of the applied primer.
Standard
Primer, Anodic Electrodeposition for Aircraft Applications
2024-05-01
WIP
AMS3144B
This specification establishes the requirements for a waterborne, corrosion inhibiting, chemical and solvent resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C).
Standard
Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 17Cr - 0.52Mo (0.95 - 1.20C) (SAE 51440C) for Bearing Applications
2024-05-01
CURRENT
AMS5880F
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
Standard
Coating System, Advanced Performance, for Exterior Aerospace Applications
2024-04-30
WIP
G824AA
This specification establishes the requirements for coating systems having high durability for use as aircraft exterior surface finishes. These coating systems normally are comprised of a surface treatment, a primer, and a topcoat and include a chemical stripper and a cleaning compound for topcoat washing.
Standard
Laser Powder Bed Fusion Produced Parts, Aluminum Alloy 7A50.60L (A7050-RAM2, composition similar to UNS A97050), Hot Isostatic Pressed and T74 Aged
2024-04-26
WIP
AMS7071
Material specification for parts produced using 7A50.60L (A7050-RAM2) using the laser powder bed fusion process
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.
