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Viewing 631 to 660 of 35886
2017-09-27
WIP Standard
AMS5702E
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C), oxidation resistance up to 1800 degrees F (982 degrees C), and good machinability, particularly parts which are welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.
2017-09-27
WIP Standard
AMS5700G
This specification covers a corrosion and heat-resistant steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
2017-09-27
WIP Standard
AMS5714E
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
2017-09-27
WIP Standard
AMS5719E
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, extrusions, and stock for forging, flash welded rings, or extruding.
2017-09-27
WIP Standard
AMS5731M
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 flanges, cases, and fasteners, requiring moderate strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1500 degrees F (816 degrees C), particularly those which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.

CURRENT
2017-09-27
Standard
AS5179C
CURRENT
2017-09-27
Standard
AS1339H
This Aerospace Standard (AS) defines the requirements for a lightweight polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000 psi, aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall.
2017-09-27
WIP Standard
AMS4040P
This specification covers an aluminum alloy in the form of sheet and plate, alclad two sides, 0.188 to 1.750 inch (4.775 to 44.450 mm) inclusive, in thickness, supplied in the annealed (O) condition (see 8.5).
2017-09-27
WIP Standard
AMS5399E
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
2017-09-27
WIP Standard
AMS5637J
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides.

These products have been used typically for small parts, such as bolts, screws, and clevis pins, requiring corrosion resistance up to 700 degrees F (371 degrees C) and which may be fabricated by heading or by machining from bars or wire and roll threading, but usage is not limited to such applications.

2017-09-27
WIP Standard
AMS4041S
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the –T3/-T351 temper.
2017-09-27
WIP Standard
AMS5504N
This specification covers a corrosion and moderate heat-resistant steel in the form of sheet, strip, and plate.
2017-09-26
WIP Standard
AMS2634C
This specification covers procedures for ultrasonic inspection of thin wall metal tubing of titanium, titanium alloy, and corrosion and heat resistant steels and alloys having nominal OD over 0.1875 inch (4.762 mm) with OD to wall thickness ratio of 8 or greater and wall thickness variation not exceeding + or - 10% of nominal.

This process has been used typically for locating internal defects, such as cracks, voids, seams, and other discontinuities, which may or may not be exposed to the surface, but usage is not limited to such applications.

2017-09-26
WIP Standard
ARP2654A
To provide general instructions for accomplishing ultrasonic thickness measurements. Measurements can be made from one side of a material when access to the opposite side is restricted.
2017-09-26
WIP Standard
ARP4402A
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
2017-09-26
WIP Standard
AS4792B
This SAE Aerospace Standard (AS) covers water conditioning agents used to facilitate aqueous wet-method magnetic particle inspection. Such conditioning agents, in powder or liquid form, provide suitable corrosion protection, wetting, and particle dispensability properties when mixed in water for application of magnetic particles on the surface of an object for magnetic particle inspection as described in AMS3042, AMS3044, ASTM E1444, and others. Water conditioning agents can consist of varying combinations of such components as dispersants, surfactants, corrosion inhibitors, and anti-foaming agents. Individual components may be added to the bath of a system to develop specific properties. The user is referred to the manufacturer of the conditioning agent to develop the most suitable combination of ingredients for the user’s requirements.
2017-09-26
WIP Standard
AS4787A
This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, aircraft engine hardware with fasteners removed. The inspection is intended to be performed at maintenance and overhaul facilities on engine run hardware. This standard has been typically used to inspect for service-induced surface and near surface cracks, but usage is not limited to such applications.
2017-09-26
WIP Standard
AMS2644G
This specification establishes the classification, technical requirements, tests, and test procedures for the qualification, approval, and quality verification of all materials used in the liquid penetrant methods of inspection with the exception of those excluded in the application section.
2017-09-25
WIP Standard
AMS2427E
This specification covers the engineering requirements for ion vapor deposition (IVD) of aluminum on steel, titanium, and aluminum alloys and the properties of the deposit. This process has been used typically to provide a corrosion-resistant coating to parts operating at service temperatures up to 925 °F (496 °C) and requiring freedom from hydrogen embrittlement and solid metal embrittlement, but usage is not limited to such applications.
2017-09-25
WIP Standard
AMS2479E
This specification establishes the engineering requirements for producing an acid-type, anodic coating on magnesium alloys and the properties of the coating.
2017-09-25
WIP Standard
AMS2478F
This specification establishes the engineering requirements for producing an acid-type, anodic coating on magnesium alloys and the properties of the coating.
2017-09-25
WIP Standard
AMS2506E
This specification covers the requirements for application to fasteners of a corrosion and heat resistant aluminum coating material having a thermosetting inorganic binder and the properties of the finished coating.
2017-09-25
WIP Standard
AMS2807C
This specification covers procedures for identifying carbon and low-alloy steels, corrosion and heat-resistant steels and alloys, maraging and other highly-alloyed steels, and iron alloy sheet, strip, and plate, and aircraft tubing.
2017-09-25
WIP Standard
AMS2437D
This specification covers the engineering requirements for applying coatings to parts by the plasma spray process and the properties of such coatings.
2017-09-25
WIP Standard
AS5969F
SCOPE IS UNAVAILABLE.
2017-09-25
WIP Standard
AS14155
This detail specification defines the dimensional and performance requirements for a three phase aircraft circuit breaker with flat blat style terminals.
2017-09-25
WIP Standard
AS33202
This detail specification defines the dimensional and performance requirements for single phase aircraft circuit breaker with blade terminals.
CURRENT
2017-09-25
Standard
AS100026B
2017-09-24
WIP Standard
ARP5584A
This SAE Aerospace Recommended Practices (ARP) covers the definitions, functions and broad application guidelines of modern aerospace vehicle electric power management systems. As aerospace control systems have become more sophisticated and autonomous, the electric power subsystem no longer is just a generation and distribution bus control system. New electric power systems include integration of individual load logic control, protection, generation, distribution, and load management. This system can report to a higher level control system, typically a vehicle management system, or can be an autonomous system within itself reporting and responding to operator commands.
Viewing 631 to 660 of 35886