Refine Your Search

Topic

Search Results

Standard

Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip and Plate

1981-10-01
HISTORICAL
AMS2262D
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of nickel, nickel alloys, and cobalt alloys ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range.
Standard

Tolerances, Metric, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate

1981-10-01
HISTORICAL
MAM2262
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of nickel, nickel alloys, and cobalt alloys ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term 'excl' is used to apply only to the higher figure of a specified range.
Standard

Bearings - Copper Lead Tin Castings

1981-07-01
AMS4840A
1. ACKNOWLEDGMENT: A vendor must mention this specification number and its last revision in all quotations and when acknowledging purchase orders.
Standard

Steel, Low Carbon, Bars, Forgings, Tubing, Sheet, Strip, and Plate, 0.25 Carbon, Maximum

1981-07-01
HISTORICAL
AMS5062D
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
Standard

Aluminum Alloy Forgings and Rolled Rings, 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6), Solution and Precipitation Heat Treated

1981-07-01
HISTORICAL
AMS4133A
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and forging stock. These products have been used typically for aircraft structural members requiring moderately high strength. Certain design and processing procedures may cause these forgings and rolled rings to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.
Standard

Aluminum Alloy, Extrusions and Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr - (6061-T6) Solution and Precipitation Heat Treated

1981-07-01
HISTORICAL
AMS4150G
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing, flash welded rings fabricated from extruded stock, and stock for flash welded rings. These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications.
X