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Viewing 451 to 480 of 35876
2017-10-25
WIP Standard
AMS5788G
This specification covers a corrosion and heat-resistant cobalt alloy in the form of welding rods, coating rods, or wrought wire.
2017-10-25
WIP Standard
AMS5792C
This specification covers a blend of tungsten carbide-cobalt aggregate, a nickel alloy, and a nickel aluminum aggregate in the form of powder.
2017-10-25
WIP Standard
AMS5805J
This specification covers a corrosion and heat resistant steel in the form of welding wire.
2017-10-25
WIP Standard
AMS5808D
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
2017-10-25
WIP Standard
AS5017A
This SAE Aerospace Standard (AS) describes the characteristics of an air filling valve used in reusable shipping and storage containers.
2017-10-25
WIP Standard
AS5135A
This SAE Aerospace Standard (AS) describes the characteristics of a desiccant port installed through the flat wall of a shipping and storage container. With the cover removed, the desiccant port shall provide access to the interior of the container for installation and removal of desiccant.
2017-10-25
WIP Standard
AS18013A
No scope available.
2017-10-25
WIP Standard
ARP726B
This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen. An external tracer gas supply may be used to increase the capacity of the system. The detector shall be capable of detecting leaks as small as .05 ounce of tracer gas per year, with a system pressure of 70 psig or less. The purpose of this document is to provide a recommended practice for the design of a universal leak detector which will pressurize a closed system with a mixture of inert and tracer gas and provide a probe and detector to indicate location and rate of system leakage with a high degree of accuracy.
CURRENT
2017-10-25
Standard
ARP60493
This guide provides detailed information, guidance, and methods for demonstrating electromagnetic compatibility (EMC) on civil aircraft. This guide addresses aircraft EMC compliance for safety and functional performance of installed electrical and electronic systems. The EMC guidance considers conducted and radiated electromagnetic emissions and transients generated by the installed electrical and electronic systems which may affect other installed electrical and electronic systems on the aircraft. Application of appropriate electrical and electronic equipment EMC requirements are discussed. Methods for aircraft EMC tests and analysis are described. This guide does not address aircraft compatibility with the internal electromagnetic environments of portable electronic devices (PED) or with the external electromagnetic environments, such as high-intensity radiated fields (HIRF), lightning, and precipitation static.
2017-10-25
WIP Standard
AMS5737Q
This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, and stock for forging or heading.

These products have been used typically for parts, such as turbine rotors, shafts, blades, vanes, dowels, flanges, and fittings, requiring moderate strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1500 degrees F (816 degrees C), but usage is not limited to such applications.

2017-10-25
WIP Standard
AMS5732K
This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings, or heading.

These products have been used typically for parts, such as turbine discs, shafts, spacers, dowels, and fittings, requiring moderate strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1500 degrees F (816 degrees C), but usage is not limited to such applications.

CURRENT
2017-10-25
Standard
AMS6372N
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
CURRENT
2017-10-25
Standard
AMS6381J
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
2017-10-25
WIP Standard
AMS5853D
This specification covers a corrosion and heat resistant steel in the form of work-strengthened bars and wire 1-1/4 inches (31.8 mm) and under in nominal diameter or least distance between parallel sides.

These bars and wire have been used typically for parts, such as fasteners, requiring room- temperature minimum tensile strength of 160 ksi (1103 MPa) after precipitation heat treatment for use up to 1000 °F (538 °C) and having oxidation resistance up to 1200 °F (649 °C), but usage is not limited to such applications.

CURRENT
2017-10-25
Standard
AMS2259F
This specification defines limits of variation for determining acceptability of the composition of wrought low-alloy and carbon steel parts and material acquired from a producer.
2017-10-25
WIP Standard
ARP4898A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.
2017-10-24
WIP Standard
B17AE
This specification covers requirements for processes and equipment used in the fabrication of forged products that are considered by the supplier and customer to be aerospace grade, have customer part number(s), and are made by any of the following forging processes and equipment.
2017-10-24
WIP Standard
AS25027B
Scope is unavailable.
2017-10-23
WIP Standard
AMS1435D
This specification covers deicing and anti-icing materials in the form of a fluid. This deicing/anti-icing fluid has been used typically on runways, taxiways, and other aircraft maneuvering areas for the prevention and removal of frozen deposits of frost and ice. Fluids must not be used to deice/anti-ice aircraft.
CURRENT
2017-10-23
Standard
AMS3218D
This specification covers a fluorocarbon (FKM) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7259 specification.
2017-10-22
WIP Standard
ARP6001A
This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic “passive” side stick that could be used for fly by wire transport and business aircraft. It addresses the following: - The functions to be implemented - The geometric and mechanical characteristics - The mechanical and electrical interfaces - The safety and certification requirements
2017-10-20
WIP Standard
AIR5128B
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnetic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). This AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds.
CURRENT
2017-10-20
Standard
AMS5031G
This specification covers a low-carbon steel in the form of covered welding electrodes.
CURRENT
2017-10-20
Standard
AMS5122K
This specification covers a carbon steel in the form of strip.
2017-10-20
WIP Standard
AS1895E
This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as “the joint”, shall operate within the temperature range of -65 to +1200 °F.
2017-10-19
WIP Standard
AMS3741
This specification covers an 80 durometer fluorosilicone (FVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
2017-10-19
WIP Standard
AMS3303L
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
2017-10-19
WIP Standard
AMS3305K
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for parts required to operate or seal from -65 to +205 degrees C (-85 to +401 degrees F). Silicone elastomer is resistant to deterioration by weathering and petroleum-base lubricating oil and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with gasoline or aromtic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
Viewing 451 to 480 of 35876