Search Results

Standard

Aluminum Alloy, Alclad Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-O) Annealed, Fine Grained

2024-04-25

CURRENT

AMS4278C

This specification covers an aluminum alloy in the form of alclad sheet over 0.039 to 0.126 inches (0.99 to 3.20 mm), inclusive, in nominal thickness with a fine-grain core of ASTM No. 6 or finer (see 8.5).

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).

Standard

Titanium Alloy Welding Wire, 5Al - 2.5Sn

2024-04-25

CURRENT

AMS4953J

This specification covers a titanium alloy in the form of welding wire (see 8.5).

Standard

Clamp - Tube Support, Spring Clips and PTFE Cushion, Procurement Specification for

2024-04-24

CURRENT

MA3399A

This procurement specification covers the requirements for metal tube support clamps comprising of two spring clips made of corrosion and heat resistant steel and the associated PTFE single split cushion that supports the tube. See Figure 1.

Standard

BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTRA LIGHT DUTY, CORROSION RESISTANT NITROGEN STEEL (CREN)

2024-04-23

CURRENT

AS27646/1B

Standard

Rivets, Solid, UNS N04400, Corrosion Resistant 67Ni - 31Cu Procurement Specification for

2024-04-23

CURRENT

AS7233A

This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi minimum shear strength.

Standard

Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement Specification For

2024-04-23

CURRENT

AS7234A

This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.

Standard

Rivets, UNS S66286, Steel, Corrosion and Heat Resistant, 80 ksi Shear Strength, Procurement Specification for

2024-04-23

CURRENT

AS7235A

This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 80 ksi single shear strength at room temperature.

Standard

Vehicle Management Systems - Flight Control Function, Design, Installation and Test of Piloted Military Aircraft, General Specification For

2024-04-16

WIP

AS94900B

This SAE Aerospace Standard (AS) provides the general performance, design, installation, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military piloted aircraft. It also provides specification guidance for the flight control interfaces with other systems and subsystems of the aircraft.

Standard

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 45° SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)

2024-04-10

CURRENT

AS85049/125A

Standard

Aluminum Alloy, Sheet 4.4Cu - 1.5Mg - 0.60Mn (2024-O) Annealed, Fine Grained

2024-04-01

CURRENT

AMS4276C

This specification covers an aluminum alloy in the form of sheet 0.020 to 0.126 inch (0.51 to 3.20 mm), inclusive, in nominal thickness, with fine grain structure (see 8.5).

Standard

Nickel Wire and Ribbon 99Ni

2024-04-01

CURRENT

AMS5555G

This specification covers a nickel in the form of round wire and rectangular ribbon.

Standard

Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20Al) Three-Component Mixture

2024-04-01

CURRENT

AMS5792C

This specification covers a blend of tungsten carbide-cobalt aggregate, a nickel alloy, and a nickel aluminum aggregate in the form of powder.

Standard

Pins, Cotter, Steel, Corrosion Resistant UNS S30200 Procurement Specification for

2024-04-01

CURRENT

AS7210B

This procurement specification covers split cotter pins with optional ends (see Figure 1), made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200.

Standard

Steel Bars, Forgings, and Mechanical Tubing and Forging Stock, Carburizing, Aircraft Quality, 0.50Cr - 1.8Ni - 0.25Mo - (0.17 - 0.23C), (SAE 4320H)

2024-04-01

CURRENT

AMS6299H

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.