Refine Your Search

Search Results

Viewing 1 to 16 of 16
Standard

Aluminum Alloy Plate, Alclad - 5.6zn - 2.5mg - 1.6cu - 0.26cr (Alclad 7075-T651)

1968-01-01
CURRENT
AMS4039C
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4049, ALUMINUM ALLOY SHEET AND PLATE (Alclad 7075; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4049 shall be fulfilled whenever reference is made to this specification.
Standard

Aluminum Alloy Plate, Alclad - 5.6zn - 2.5mg - 1.6cu - 0.26cr (Alclad 7075-T651)

1960-06-01
HISTORICAL
AMS4039
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4049, ALUMINUM ALLOY SHEET AND PLATE (Alclad 7075; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4049 shall be fulfilled whenever reference is made to this specification.
Standard

Aluminum Alloy, Plate, Alclad 4.4cu 1.5mg 0.60m

1960-06-01
HISTORICAL
AMS4034
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4041, ALUMINUM ALLOY SHEET AND PLATE, ALCLAD (Alclad 2024 and 1-1/2% Alclad 2024-T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate). The requirements of the latest issue of AMS 4041 shall be fulfilled whenever reference is made to this specification.
Standard

Aluminum Alloy, Plate, Alclad 4.4cu 1.5mg 0.60m

1964-01-01
HISTORICAL
AMS4034A
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4041, ALUMINUM ALLOY SHEET AND PLATE, ALCLAD (Alclad 2024 and 1-1/2% Alclad 2024-T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate). The requirements of the latest issue of AMS 4041 shall be fulfilled whenever reference is made to this specification.
Standard

Aluminum Alloy, Plate, Alclad 4.4cu 1.5mg 0.60m

1967-11-01
HISTORICAL
AMS4034B
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4041, ALUMINUM ALLOY SHEET AND PLATE, ALCLAD (Alclad 2024 and 1-1/2% Alclad 2024-T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate). The requirements of the latest issue of AMS 4041 shall be fulfilled whenever reference is made to this specification.
Standard

Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products

1964-01-01
HISTORICAL
ARP823
The purpose of this recommended practice is to provide the aerospace industry with recommendations concerning minimizing of stress-corrosion cracking (SCC) in wrought high-strength aluminum alloy products. The detailed recommendations are based on practical engineering experience and reflect those design practices and fabricating procedures which have been found to be most effective in minimizing stress-corrosion cracking in wrought high-strength aluminum alloy products. This ARP provides general guidelines. For further information see references in 4.3.
X