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Viewing 1 to 30 of 18868
2017-12-11
WIP Standard
AMS2819C
This specification covers the procedures for identification and marking of bare welding wire by a color code system and marking of spools.
CURRENT
2017-12-11
Standard
AMS2451/4D
This specification establishes the requirements for brush plating of cadmium by electrodeposition.
2017-12-08
WIP Standard
AMS4330C
This specification covers an aluminum alloy in the form of plate.
2017-12-08
WIP Standard
AMS4306C
This specification covers an aluminum alloy in the form of plate.
2017-12-07
WIP Standard
ARP7488
This Aerospace Recommended Practice (ARP) describes design and processing considerations for the shot peening process when AMS2430 or AMS2432 are specified.
CURRENT
2017-12-07
Standard
AMS4434N
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-12-07
Standard
AMS4958E
This specification covers a titanium alloy in the form of bars and rods 1.00 inch (25.4 mm) and under in nominal diameter.
CURRENT
2017-12-07
Standard
AMS5532H
This specification covers a corrosion and heat-resistant iron alloy in the form of sheet, strip, and plate.
CURRENT
2017-12-07
Standard
AMS6349E
This specification covers an aircraft quality, low alloy steel in the form of bars.
CURRENT
2017-12-07
Standard
AMS6452E
This specification covers a low-alloy steel in the form of welding wire.
CURRENT
2017-12-07
Standard
AMSQQA200/6C
This specification covers the specific requirements for aluminum alloy 5454 bar, rod, shapes, tube, and wire produced by extrusion.
CURRENT
2017-12-07
Standard
AMSQQA200/7C
This specification covers the specific requirements for aluminum alloy 5456 bar, rod, shapes, tube, and wire produced by extrusion.
CURRENT
2017-12-07
Standard
AS1650E
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
2017-12-07
WIP Standard
AS7232A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made form a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600. Primarily for fastener applications requiring corrosion resistance and heat and oxidation resistance up to 2000 degrees F, but with reduced strength at the elevated temperatures. Rivets shall not be hand peened during driving.
CURRENT
2017-12-07
Standard
AMS4035M
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.750 inch (0.25 to 44.45 mm) in thickness, supplied in the annealed (O temper) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper.
CURRENT
2017-12-07
Standard
AMS5350K
This specification covers a corrosion and moderate heat-resistant steel in the form of investment castings.
CURRENT
2017-12-07
Standard
AMS4928W
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings.
CURRENT
2017-12-07
Standard
AMS5537J
This specification covers a corrosion and heat-resistant cobalt alloy in the form of sheet, strip, foil, and plate up to 2.250 inches (57.15 mm) inclusive, in nominal thickness (see 8.4).
CURRENT
2017-12-07
Standard
AMS6931D
This specification covers a titanium alloy in the form of bars and forgings up through 10.000 inches (254.00. mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 79.0 in2 (506.45 cm2) and forging stock of any size (see 8.7).
CURRENT
2017-12-05
Standard
AMS6466G

This specification covers a corrosion-resistant steel in the form of welding wire.

2017-12-03
WIP Standard
AMSQQA200/5B
This specification covers the specific requirements for aluminum alloy 5086 bar, rod, shapes, tube, and wire produced by extrusion.
2017-12-03
WIP Standard
AMSQQA225C
This specification covers the general requirements for aluminum and aluminum alloy bar, rod, wire, or special shapes; rolled, drawn, or cold finished. Specific requirements for these products are covered by the applicable detail specification (See 6.3).
2017-12-03
WIP Standard
AMSQQA200/13C
This specification covers the specific requirements for aluminum alloy 7178 bar, rod, shapes, tube, and wire produced by extrusion.
2017-12-03
WIP Standard
AMSQQA200/14B
This specification covers the specific requirements for aluminum alloy 7178-T76 bar, rod, shapes, and wire produced by extrusion.
2017-12-01
WIP Standard
AMS3021F
This specification covers a neopentyl polyol ester fluid.
2017-12-01
WIP Standard
ARP1176B
This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces, parts (including regulator and valve parts), cylinders and ground-based equipment that may be used to support aircraft oxygen systems. This revision introduces a cleanliness coding scheme that can be referenced as a requirement, and/or referenced to identify compliance to meeting such a requirement. These methods may apply to gaseous and liquid oxygen equipment. This document specifies work area details, methods to select suitable cleaning agents, cleaning methods, test methods to verify cleanliness level, and methods of packaging the components and parts after cleaning. Technicians designated to clean oxygen equipment must be qualified and trained to clean oxygen equipment. This ARP is applicable to metallic and non-metallic parts.
Viewing 1 to 30 of 18868