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Viewing 721 to 750 of 35602
CURRENT
2017-08-02
Standard
AS5756/7A
CURRENT
2017-08-02
Standard
ARP4737J
This document establishes the minimum requirements for ground based aircraft deicing/anti-icing Methods and procedures to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models. NOTE: Particular airline or aircraft manufacturers' published manuals, procedures, or methods supplement the information contained in this document.
CURRENT
2017-08-02
Standard
AS3209A
2017-08-02
WIP Standard
AS1895/1E
No scope available.
2017-08-01
WIP Standard
ARP7208
This ARP establishes guidelines for the use of IEEE-802.3 as a data bus network in military and aerospace vehicles. It encompasses the data cable and its connections for a system utilizing 10Base-T, 100Base-T, 1000BASE-T and 10GBASE-T over copper medium dependent interfaces (MDI). This document contains extensions/restrictions to “off-the-shelf” IEEE-802.3 standards, and assumes that the reader already has a working knowledge of IEEE-802.3.
CURRENT
2017-08-01
Standard
AMSQQW428/2B
2017-07-31
WIP Standard
AMS7005
This specification establishes process controls for the repeatable production of aerospace parts by High Deposition Rate (HDR). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
2017-07-31
WIP Standard
AS4370F
SCOPE IS UNAVAILABLE.
2017-07-28
WIP Standard
ARP8000
This SAE Aerospace Recommended Practice (ARP) document covers the requirements for a Snowcompressor with carrier vehicle used to clear snow from airport operational areas by compressing the volume of collected snow into smaller volumes for loading into a hauling/dump truck or for depositing reduced-volume windrows for snow banking. The term carrier vehicle represents the various self-propelled prime movers that provide the power necessary to move snow and ice control equipment during winter operations. For two-stage rotary plows that primarily are used to cast heavy concentrations of snow away from airport operational areas such as runways and taxiways, see ARP5539.
CURRENT
2017-07-26
Standard
AMS2428
This specification covers the requirements for electrodeposited nanocrystalline cobalt-phosphorus plating.
CURRENT
2017-07-26
Standard
AS123301D
2017-07-24
WIP Standard
AMSQQA200/6C
This specification covers the specific requirements for aluminum alloy 5454 bar, rod, shapes, tube, and wire produced by extrusion.
2017-07-24
WIP Standard
AMSQQA200/4C
This specification covers the specific requirements for aluminum alloy 5083 bar, rod, shapes, tube, and wire produced by extrusion.
2017-07-24
WIP Standard
AMSQQA200/7C
This specification covers the specific requirements for aluminum alloy 5456 bar, rod, shapes, tube, and wire produced by extrusion.
2017-07-24
WIP Standard
AMSWWT700/5B
This specification covers the specific requirements for seamless tube drawn from aluminum alloy 5086.
2017-07-24
WIP Standard
AMSWWT700B
This specification covers the general requirements for aluminum and aluminum alloy tube; drawn, seamless (see 6.1.1). Specific requirements for these products in a particular alloy are covered by the applicable detail specification (see 6.3).
CURRENT
2017-07-24
Standard
ARP5483/2A
This method outlines the standard procedure for testing the hardness of bearing components. Bearings covered by this test method shall be any rolling element bearing used in airframe control.
CURRENT
2017-07-24
Standard
ARP6216
This SAE Aerospace Recommended Practice (ARP) identifies the minimum requirements for the testing of insulated electrical wiring for on-aircraft, aeronautical and aerospace applications. The testing requirements defined herein, ensure that a wire fault can be found safely when using a high potential voltage tester (hipot). This test is intended to aid in finding a breach in the wire insulation, and not for the identification of the resistance of the insulation. The test method defined herein is limited to equipment which ia able to control and limit the DC output to 1500 VDC maximum. This type of wire dielectric tester is typically designed to trip on current leakage and not necessarily on arc detection. This test method is solely designed to identify gross/large wire insulation damage or degradation. For additional related information on this topic and related test methods, refer to the documents cited in Section 2.
CURRENT
2017-07-20
Standard
AMS5930B
This specification covers a premium aircraft-quality, alloy steel in the form of bars, forgings, and forging stock.
CURRENT
2017-07-20
Standard
AMS5951A
This specification covers a corrosion and heat-resistant nickel based alloy in the form of sheet, strip, and plate 0.020 to 1.0 inch (0.508 to 25.4 mm) in thickness (see 8.5).
2017-07-20
WIP Standard
ARP5873B
This document presents minimum criteria for the design and installation of LED passenger reading light assemblies in commercial aircraft. The use of “shall” in this specification expresses provisions that are binding. Non-mandatory provisions use the term “should.”
CURRENT
2017-07-20
Standard
AMS4975N
This specification covers a titanium alloy in the form of bars, wire, flash welded rings 3.00 inches (76.2 mm) and under in nominal diameter or least distance between parallel sides and 16 in2(103 cm2) and under in cross-sectional area and stock of any size for flash welded rings (see 8.4).
CURRENT
2017-07-20
Standard
AMS5862M
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 4.0 inches (102 mm) and under in nominal thickness (see 8.5).
Viewing 721 to 750 of 35602