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Viewing 91 to 120 of 35188
CURRENT
2017-09-12
Standard
AS7513
Male ferrule, swaged, for procurement specification AS6335 and will supersede AS5833.
CURRENT
2017-09-12
Standard
AS7516
SCOPE IS UNAVAILABLE.
2017-09-12
WIP Standard
SAE9991
This information report provides an overview of the eLoran PNT system.
2017-09-11
WIP Standard
AS6171/6A
Through the use of ultra-high frequency ultrasound, typically above 10 MHz, Acoustic Microscopy (AM) non-destructively finds and characterizes physical features and latent defects (visualization of interior features in a layer by layer process) - such as material continuity and discontinuities, sub-surface flaws, cracks, voids, delaminations and porosity. AM observed features and defects can be indicators that the components were improperly handled, stored, altered or previously used. If AS6171/6 is invoked in the contract, the base document, AS6171 General Requirements shall also apply.
CURRENT
2017-09-11
Standard
AMS4251B
This specification covers an aluminum alloy in the form of sheet 0.040 to 0.249 inch (1.02 to 6.32 mm) in thickness (see 8.6).
CURRENT
2017-09-11
Standard
ARP1621C
This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several.
CURRENT
2017-09-11
Standard
AS4682C
Propose revision to add conductive high purity aluminum coating per MIL-DTL-83488 for aluminum alloy fittings. The W code aluminum parts with new finish will be distinguished by new finish code V at the end of part number.
CURRENT
2017-09-11
Standard
AS5958F
This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium and CRES tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35 000 kPa) maximum and an operating temperature range of -65 to +275 °F (-54 to +135 °C). This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The fitting operating pressure is based on the fitting thread pitch. Extra fine pitch for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures.
CURRENT
2017-09-11
Standard
AS7510
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system.
2017-09-11
WIP Standard
AS7454C

This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675.

AS7454 - 135,000 psi ultimate tensile strength at room temperature.

AS7454-1 - 135,000 psi ultimate tensile strength at room temperature, nickel-cadmium plated.

CURRENT
2017-09-11
Standard
AMS4971L
This specification covers a titanium alloy in the form of bars, wire, forgings and flash welded rings 4.000 inches (101.60 mm) and under in diameter or least distance between parallel sides and stock for forging or flash welded rings of any size (see 8.6).
CURRENT
2017-09-08
Standard
AS4675B
SCOPE IS UNAVAILABLE.
CURRENT
2017-09-08
Standard
AS4677C
SCOPE IS UNAVAILABLE.
CURRENT
2017-09-08
Standard
ARP6253A
This document presents minimum criteria for the design and installation of LED assemblies in aircraft. The use of "shall" in this specification expresses provisions that are binding. Nonmandatory provisions use the term "should."
CURRENT
2017-09-07
Standard
AS4157B
This specification covers the requirements for aircraft hydraulic, self-sealing, quick disconnect couplings for use in 8000 lbf/in2 (gage) lightweight hydraulic systems.
CURRENT
2017-09-07
Standard
AS3326B
SCOPE IS UNAVAILABLE.
CURRENT
2017-09-07
Standard
AS7512
Coupling body for procurement specification AS6335.
CURRENT
2017-09-07
Standard
AS7514
SCOPE IS UNAVAILABLE.
2017-09-06
WIP Standard
AMS03_9A
This SAE Standard specifies the requirements for the electro-deposition of silver on ferrous-base, copper-base, aluminum-base, zinc-base and nickel base materials. It is primarily intended for use on electrical and electronic items which are to be plated with silver to increase the electrical conductivity of the surface. This Standard does not cover the silver plating of threaded items.
CURRENT
2017-09-05
Standard
AMS6407K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Viewing 91 to 120 of 35188