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CURRENT
2017-04-19
Standard
AS20708/66B
CURRENT
2017-04-18
Standard
AS20708/74B
No Scope Available
CURRENT
2017-04-18
Standard
AS20708/67B
No Scope Available
CURRENT
2017-04-18
Standard
AS6416
This SAE Aerospace Standard provides definitions for terms and requirements used in SAE AS procurement specifications for fasteners (bolts, screws, studs, nuts, and other threaded parts).
CURRENT
2017-04-18
Standard
MA620SUP1A
This supplement forms a part of Aerosapce Standard MA620, Hose Assemblies, Convoluted Polytetrafluorethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft, Metric and shall be used to identify hose assembly standards citing this procurement specification.
CURRENT
2017-04-13
Standard
AIR36105B
The present SAE Aerospace Information Report (AIR) provides a list of the main government regulations, SAE and international standards, and standing industry recommendations applying to air cargo unit load devices (pallets, nets, and containers) to be loaded with either baggage or freight on board civil transport aircraft.
CURRENT
2017-04-11
Standard
AS6174/1
The verification matrix (VM) in this slash sheet is intended for use to establish compliance to AS6174A. This slash sheet is applicable to AS6174A. Nothing in this slash sheet, however, supersedes applicable laws and regulations, unless a specific exemption has been obtained through judicial/legal channels.
CURRENT
2017-04-07
Standard
AS4108B
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
HISTORICAL
2017-04-06
Standard
AS1708F
CURRENT
2017-04-05
Standard
ARP6156
The lubricant performance capability for aero propulsion drive systems is derived from the physical properties of the oil and the chemical attributes associated with the oil formulation. All properties, such as viscosity, pressure-viscosity coefficient and full-film traction coefficient are inherent properties of the lubricating fluid. Chemical attributes are critical for the formation of protective boundary lubricating films on the surfaces to prevent wear and scuffing. To assure performance and to provide needed information for engineering design, test methodologies for at least five oil properties or attributes are being addressed: (1) pressure-viscosity coefficient, (2) full-film traction coefficient, (3) scuffing resistance, (4) wear resistance, and (5) micropitting propensity. While viscosity versus temperature data are readily available, the above five properties or attributes must be measured under relevant conditions for aero propulsion hardware systems.
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