Criteria

Text:
Topic:
Content:
Display:

Results

Viewing 1 to 30 of 9395
2015-07-30
Standard
AIR1273B
This SAE Aerospace Information Report (AIR) establishes a positive identification of the functions and, if applicable, the hazards and direction of flow of pipe, hose, tube, or electrical conduit lines.
2015-07-28
Standard
AMS5656F
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, extrusions, flash welded rings, and stock for forging, extruding, or flash welded rings.
2015-07-28
Standard
AMSQQP416D
This specification covers the requirements for electrodeposited cadmium plating.
2015-07-28
Standard
AMS6935B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 32 square inches (204.46 cm2), and stock for forging of any size (See 8.7).
2015-07-17
WIP Standard
AMS2430U
This specification covers the requirements for automatic shot peening of surfaces of parts by impingement of media, including metallic, glass, or ceramic shot.
2015-07-16
Standard
AMS5580L
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
2015-07-16
Standard
AMS6921B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-16
Standard
AMS6925B
This specification covers a titanium alloy in the form of bars up through 7.000 inches (177.80 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 7.000 inches (177.80 mm), inclusive, and stock for forging of any size.
2015-07-16
Standard
AMS6926B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-16
Standard
AMS6920C
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-13
Standard
AMS4333D
This specification covers an aluminum alloy in the form of die forgings 4.000 inches (102 mm) and under in nominal thickness and of forging stock of any size.
2015-07-13
Standard
AMS6947A
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes 4.000 inches (101.60 mm) and under, and stock for forging, heading, or flash welded rings of any size.
2015-07-08
Standard
J2286_201507
This interface document SAE J2286 revises the requirements for file formats as were originally described in SAE J1924. This document describes Interface 1 (I/F 1) in SAE J2461. This document does not imply the use of a specific hardware interface, but may be used with other hardware interfaces such as SAE J1939, ISO 15765 or ISO 14229. The requirements of SAE J2286 supersede the requirements defined by SAE J1924. SAE J2461 establishes the requirements for Interface 1 (I/F 1), as a replacement of the file-based interface described by SAE J1924, as shown by Figure 1. Interface 1 (I/F) is a bi-directional link between the OEM Shop Floor Program (CSCI 1) and the Vendor Component Program (CSCI 2). Using I/F 1, the OEM Shop Floor Program communicates the desired parameters and programming limits for an assembly job to the Vendor Component Program (VCP). In response, the VCP returns programming results to the OEM Shop Floor Program (CSCI 1).
2015-07-07
WIP Standard
D15AB
This specification covers an aluminum alloy in the form of sheet and plate clad on both sides.
2015-07-06
Standard
AMS6425D
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-07-06
Standard
AMS4467A
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.
2015-07-06
Standard
AMS6482A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-07-06
Standard
AMS7909C
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of blocks, blanks or shapes.
2015-07-06
Standard
AMS4510H
This specification covers a copper alloy (phosphor bronze) in the form of sheet, strip, and plate.
2015-07-06
Standard
AMS5701E
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
2015-07-06
Standard
AMS4972H
This specification covers a titanium alloy in the form of bars, wire, flash welded rings up through 4.000 inches (101.60 mm), inclusive in diameter or least distance between parallel sides, and stock for flash welded rings or heading of any size.
2015-07-06
Standard
AMS4984F
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size.
2015-07-06
Standard
AMS5879D
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness. (See 8.4).
2015-07-06
Standard
AMSQQN290C
These products have been used typically for electrodeposited nickel plating on steel, copper and copper alloys, and zinc and zinc alloys, but usage is not limited to such applications.
2015-06-30
Standard
J2467_201506
The SAE Standard covers normalized electric resistance welded, cold-drawn, single-wall, SAE 1021 carbon steel pressure tubing intended for use as pressure lines and in other applications requiring tubing of a quality suitable for bending, flaring, forming, and brazing. The grade of material produced to this specification is higher in carbon content and manganese content than the grade of material specified in SAE J525 and is intended to service higher pressure applications than equivalent sizes of SAE J525. Due to the higher carbon and manganese content the forming characteristics of the finished tube are diminished versus the SAE J525 product. Special attention to the overall forming requirements of the finished assembly shall be taken into consideration when specifying material produced to this specification.
2015-06-30
Standard
J2441_201506
This SAE Standard covers the engineering requirements for peening surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot. To induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking.
2015-06-23
WIP Standard
AMS4598B
This specification covers a copper-nickel-tin alloy in the form of mechanical tube.
2015-06-22
WIP Standard
AS36100B
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of Title 14 CFR Part 25, except for the 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
2015-06-18
Standard
J2175_201506
This SAE Recommended Practice describes chemical analysis, hardness, microstructure, and physical characteristic requirements for low carbon cast steel shot to be used for shot peening or blast cleaning operations.
2015-06-18
Standard
AS6886
Counterfeiting of refrigerants has seen a dramatic rise over the past two decades. This rise can be partially attributed to global restrictions placed on production and use of refrigerants by the 1987 Montreal and the 1997 Kyoto Protocols (1, 2). These Protocols regulate the gradual phase-out and strict regulations on the use of refrigerants with high Ozone Depletion Potential (ODP) and high Global Warming Potential (GWP). These protocols require that older refrigerants shall be replaced with newer, more expensive, and environmentally friendly chemicals (3, 4) and necessitates redesigned or replaced equipment to operate efficiently with these new refrigerants.
Viewing 1 to 30 of 9395