Criteria

Text:
Content:
Display:

Results

Viewing 271 to 300 of 38467
2015-07-07
WIP Standard
MA3422A
No scope available.
2015-07-07
WIP Standard
MA3424A
No scope available.
2015-07-07
WIP Standard
MA3426A
No scope available.
2015-07-07
Standard
AMS6419H
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
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
AMS3823E
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs. This specification covers one type of woven glass cloth treated with a chrome-silane finish.
2015-07-06
Standard
AMS3833B
This specification covers a polyester and cotton blended broadcloth, chemically treated with a durable press finish and cured.
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
AMS4926N
This specification covers a titanium alloy in the form of bars, wire, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and 16 square inches (103 cm2) and under in cross-sectional area, and stock of any size for flash welded rings.
2015-07-06
Standard
AMS3821C
This specification covers a style 7781 glass cloth impregnated with a heat-curable epoxy resin system, the resin being processd to a "B" stage condition, and furnished in the form of continous rolls.
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
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
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
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
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.
2015-07-04
Standard
AIR4004A
Recent field experience has indicated significant problems with some types of wire and cables as routed on aircraft landing gear. This SAE Aerospace Information Report (AIR) is intended to identify environmental concerns the designer should consider, materials that appear to be most suitable for use in these areas, routing, clamping, and other protection techniques that are appropriate in these applications. In recent years aircraft certification regulatory agencies introduced new regulations regarding Electrical Wiring Interconnection Systems (EWIS) to further enhance safety of the associated systems and aircraft overall.
2015-07-04
Standard
AS28772B
SCOPE IS UNAVAILABLE.
2015-07-04
Standard
AS6479/2
This detail specification defines fiber optic fusion splicers acceptable for the installation and repair of a wide range of optical fibers and cables with virtually no insertion loss, particularly in aerospace applications, but not in flammable or explosive atmospheres (Type II). The requirements for acquiring the splicer described herein shall consist of this specification and the latest issue of AS6479.
2015-07-04
Standard
AS5861A
This SAE Aerospace Standard (AS) covers solid polytetrafluoroethylene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic system components as anti-extrusion devices in conjunction with O-rings, packings and other elastomeric seals. Because of the construction of groove dimensions, back-ups specific to rod applications are designated “R” - Rod (Female), back-ups specific to piston applications are designated “P” - Piston (Male). Retainers specified herein have been designed for a temperature range of -65 to 275 °F (-54 to 135 °C) and a nominal operating pressure of 3000 psi (20 684 kPa) for code 09 material and 5000 psi (34 474 kPa) for code 10 material. Material codes are based on AMS3678 material types.
2015-07-04
Standard
ARP694C
This ARP is intended to cover all external lights on the tanker and fixed wing receiver airplanes used to accomplish aerial refueling. This ARP describes lights used for two basic types of aerial refueling: The Probe and Drogue, and the Boom/Receptacle method.
2015-07-04
Standard
AS6479/1
This detail specification defines fiber optic fusion splicers acceptable for the installation and repair of a wide range of optical fibers and cables with virtually no insertion loss in hazardous environments (potentially flammable or explosive atmospheres, Type I), particularly aerospace applications. The requirements for acquiring the splicer described herein shall consist of this specification and the latest issue of AS6479.
Viewing 271 to 300 of 38467