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CURRENT
2017-09-14
Standard
AMS5337E
This specification covers an alloy steel in the form of investment castings.
2017-09-14
WIP Standard
J356
The SAE Standard covers normalized electric-resistance welded flash-controlled single-wall, low-carbon steel pressure tubing intended for use as pressure lines and in other applications requiring tubing of a quality suitable for bending, double flaring, beading, forming, and brazing. Material produced to this specification is not intended to be used for single flare applications due to the potential leak path that would be caused by the ID weld bead or scarfed region. Assumption of risks when using this material for single flare applications to be defined by agreement between the producer and tube purchaser. This specification also covers SAE J356 Type-A tubing. The mechanical properties and performance requirements of standard SAE J356 and SAE J356 Type-A are the same. Therefore, the designated differences of Type-A tubing are not meant to imply that Type-A tubing is in anyway inferior to standard SAE J356.
2017-09-14
WIP Standard
J527
This SAE Standard covers brazed double wall low-carbon steel tubing intended for general automotive, refrigeration, hydraulic, and other similar applications requiring tubing of a suitable quality for bending, flaring, beading, forming, and brazing.
CURRENT
2017-09-14
Standard
AMS5338H
This specification covers a low-alloy steel in the form of investment castings.
CURRENT
2017-09-13
Standard
AMS4466A
This specification covers an aluminum alloy in the form of alclad sheet and plate 0.020 to 0.500 inch (0.508 to 12.70 mm) inclusive, in thickness, supplied in the -T361 temper (see 8.5).
CURRENT
2017-09-13
Standard
ARP5637A
The information in this document is intended to apply to commercial jet transport category airplanes that incorporate plastic (polycarbonate or acrylic) lenses on exterior light assemblies, or are being considered for such an application as opposed to glass lens designs. Exterior lighting applications include position light assemblies, anticollision light asemblies, and landing light assemblies. However, much of the material provided herein is general in nature and is directly applicable to many aircraft categories including, but not limited to, helicopters, general aviation aircraft, and military aircraft.
2017-09-13
WIP Standard
AMS3721
The scope of the project is to write a specification for the measuring of adhesion of coatings.
CURRENT
2017-09-13
Standard
AMS4163F
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 2.999 inches, incl (76.17 mm, incl) in thickness, nominal diameter or wall thickness with cross-sectional area 25 in2 (161 cm2) and under (see 8.5).
CURRENT
2017-09-13
Standard
AMS5336J
This specification covers a low-alloy steel in the form of investment castings.
CURRENT
2017-09-13
Standard
J2597_201709
This SAE Recommended Practice defines a procedure for the use of computer generated saturation curves to determine peening intensity. Calculation of intensity within a tolerance band for each data set in Table 1 one is required for compliance with this practice.
2017-09-12
WIP Standard
J174
This test procedure is intended to provide a quality control method for checking torque-tension characteristics of non-prevailing torque type threaded steel fasteners 1/4 through 1 in nominal diameters. Realistically, torque-tension relationships for specific individual fastener assembly joints will vary due to the different joint parameters. Tests using actual joint components will be required to determine accurate torque-tension values for those conditions. For the metric version, see SAE J174M.
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.
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
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
2017-09-11
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.
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
J1237_201709
This SAE Standard covers material, dimensional, performance and test requirements for metric thread rolling screws suitable for use in general engineering applications.
CURRENT
2017-09-05
Standard
AMS4892D
This specification covers a nickel-copper alloy in the form of castings.
Viewing 211 to 240 of 20547