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Viewing 271 to 300 of 35602
CURRENT
2017-10-13
Standard
AMS4463A
This specification covers an aluminum alloy in the form of plate 0.750 to 1.500 inch, incl ( 19.05 to 38.10 mm, incl) in thickness (see 8.5).
CURRENT
2017-10-13
Standard
AMS4296C
This specification covers an aluminum alloy in the form of sheet and plate 0.032 to 0.310 inch, incl (0.81 to 7.87 mm, incl) in thickness, clad on both sides (see 8.4).
CURRENT
2017-10-12
Standard
AMS6328N
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2017-10-12
Standard
AS102C
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
2017-10-12
Standard
AMS2804D
This specification covers the requirements for identification of castings.
CURRENT
2017-10-11
Standard
AS6089
This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that this verification document only verifies the specific requirements from AS5653 and does not verify all of the requirements invoked by documents that are referenced by AS5653. The procuring authority may require further testing to verify the requirements not explicitly defined in AS5653 and in this verification document.
CURRENT
2017-10-10
Standard
AMS4206C
This specification covers an aluminum alloy in the form of plate 0.500 to 1.500 inches (12.70 to 38.10 mm) inclusive, in thickness (see 8.4).
CURRENT
2017-10-10
Standard
AMS4464A
This specification covers an aluminum alloy in the form of plate 0.500 to 1.500 inch, incl (12.70 to 38.10 mm, incl) in thickness (see 8.4).
CURRENT
2017-10-10
Standard
AMS4467B
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.
CURRENT
2017-10-10
Standard
AS85049/153
This AS85049 product will accommodate the user demand for a metal version of the AS85049/105 style accessory.
CURRENT
2017-10-10
Standard
ARP5945A
The purpose of this ARP is to provide the sample selection criteria and test procedures for SAE Type I aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G 12 Holdover Time Subcommittee. A significant body of previous research and testing has indicated that all Type I fluids formulated with glycol perform in a similar manner from an endurance time perspective. This applies to Type I deicing/anti-icing fluids formulated with propylene glycol, ethylene glycol, and diethylene glycol only. Type I deicing/anti-icing fluids containing these glycol bases no longer require testing for endurance times. The methods described in this ARP shall be employed, however, if endurance time testing of a glycol-based Type I deicing/anti-icing fluid is desired or requested by a fluid manufacturer, operator or other organization.
CURRENT
2017-10-10
Standard
AIR6504
This SAE Aerospace Information Report (AIR) provides a method for assessing particle losses that occur in a sampling system of specified geometry based on the nvPM mass and number measured at the end of the sampling system. Both size dependent diffusion loss and size independent thermophoretic loss mechanisms are included in the method. The penetration function of that system must be determined by measurement and/or by computation using an analytical method as described within this report. The outcome of this line loss assessment provides estimated correction factors for nvPM mass and number concentration with associated uncertainties based upon nvPM measurement uncertainties and method assumptions. These correction factors give an estimation of nvPM mass and number values at the inlet to the sampling system.
CURRENT
2017-10-10
Standard
ARP6385
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
CURRENT
2017-10-10
Standard
AMS4329B
This specification covers an aluminum alloy in the form of plate 4.001 to 7.000 inch, incl. (101.62 to 177.80 mm, incl.) in thickness (see 8.4).
CURRENT
2017-10-10
Standard
ARP5485B
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures, for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G 12 Holdover Time Subcommittee.
CURRENT
2017-10-10
Standard
ARP6207
This document describes: 1) the preparatory steps to test experimental Type I fluids according to AMS1424; 2) the recommendations for the preparation of samples for endurance time testing according to ARP5945; 3) a short description of recommended field spray test; 4) the protocol to generate draft holdover time guidelines from endurance time data as obtained from ARP5945; 5) the role of the SAE G-12 Fluids Subcommittee; 6) the role of the SAE G-12 Holdover Time Subcommittee; 7) the process for the publication of holdover time guidelines and FAA/Transport Canada list of fluids.
CURRENT
2017-10-10
Standard
AS18280/1C
This SAE Aerospace Standard (AS) establishes the requirements for bite type sleeves for use with 24° cone flareless fluid connection fittings per AS18280.
2017-10-09
WIP Standard
TEMPBALAMS2801
Ballot of AMS2801 to AMEC members only.
2017-10-06
WIP Standard
AMS5395D
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of January 1995. It is recommended, therefore, that this specification not be specified for new designs.
2017-10-05
WIP Standard
ARP5483/7B
This test method outlines the recommended machine function, fixtures and procedures for performing dynamic radial load tests on track roller bearings for airframe applications. Bearings covered by this test method shall be yoke and stud type track roller, needle bearings.
2017-10-05
WIP Standard
ARP5483/8B
This test method outlines the recommended machine function, fixtures and procedures used to test airframe rolling element bearings for dynamic performance under steady unidirectional radial load and oscillatory motion. Bearings covered by this test method shall be ball, roller and needle type in either annular or rod end configuration, used in airframe control applications.
2017-10-05
WIP Standard
AIR6811
Provide guidance for applying aircraft equipment electromagnetic, electrical, and mechanical qualification standards, including RTCA/DO-160, MIL-STD-461, MIL-STD-810, and MIL-STD-704, to civil aircraft certification intended for military use and for military aircraft equipment installed on civil aircraft. The guidance will identify where the equipment environmental qualification standards meet the intent of the civil or military aircraft certification requirements. Conversely, the guidance will identify where the equipment environmental qualification standards have differences that do not meet the intent of the civil or military aircraft certification requirements and when these differences matter based on equipment criticality.
CURRENT
2017-10-04
Standard
AMS03_28PT1A
This SAE Standard covers the requirements for coatings of high purity aluminum on low alloy steels, high strength steels, corrosion-resisting steels, aluminum alloys and titanium alloys and other materials where appropriate.
CURRENT
2017-10-04
Standard
AMS03_28PT3A
This SAE Standard specifies the requirements for coatings of titanium nitride on non-corrosion resisting and corrosion resisting steels, cast irons and other suitable materials. Standard engineering items such as coated tools, drills and dies would not normally be included.
CURRENT
2017-10-04
Standard
AMS03_28PT2A
This SAE Standard covers the requirements for the deposition of cadmium coatings on carbon steel, low alloy steels, high strength steels, corrosion resisting steels and other materials where appropriate.
CURRENT
2017-10-04
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.
CURRENT
2017-10-04
Standard
AMS03_11A
This SAE Standard specifies requirements for the processing of iron and steel (excluding corrosion resisting steels) to produce coatings consisting essentially of inorganic phosphates, which are intended to be used in conjunction with supplementary finishes for the protection of the basis metal against corrosion (and in certain cases to give, additionally, anti-wear properties to sliding surfaces).
Viewing 271 to 300 of 35602