Criteria

Text:
Content:
Display:

Results

Viewing 1 to 30 of 439
CURRENT
2017-03-21
Standard
AS20708/50B
Scope is unavailable.
CURRENT
2017-03-21
Standard
AS20708/46B
No Scope Available
CURRENT
2017-03-21
Standard
AS20708/52B
No Scope Available
CURRENT
2017-03-21
Standard
AS20708/53B
No Scope Available
CURRENT
2017-03-21
Standard
AS20708/55B
No Scope Available
CURRENT
2017-03-21
Standard
AS20708/56B
Scope is unavailable.
CURRENT
2017-03-20
Standard
AS20708/47B
No Scope Available
CURRENT
2017-03-20
Standard
AS20708/49B
No Scope Available
CURRENT
2017-03-20
Standard
AS20708/48B
No Scope Available
CURRENT
2017-03-20
Standard
AS20708/54B
No Scope Available
2017-03-17
WIP Standard
AS20708/62B
No Scope Available
2017-03-17
WIP Standard
AS20708/66B
No Scope Available
2017-03-17
WIP Standard
AS20708/67B
No Scope Available
2017-03-17
WIP Standard
AS20708/74B
No Scope Available
2017-03-17
WIP Standard
AS20708/78B
No Scope Available
2017-03-17
WIP Standard
AS20708/79B
No Scope Available
2017-03-17
WIP Standard
AS20708/80B
No Scope Available
2017-03-17
WIP Standard
AS20708/68B
No scope available.
2017-03-17
WIP Standard
AS20708/76B
No Scope Available
2017-03-17
WIP Standard
AS20708/70B
No Scope Available
2017-03-09
WIP Standard
ARP6950
This SAE Aerospace Recommended Practice (ARP) provides guidance and interpretation on how to apply the objectives and activities in ARP4754A, “Guidelines for Development of Civil Aircraft and Systems”, to propulsion systems with electronic engine control. As the ARP4754A was developed and written more generally at the aircraft level, guidance will be provided to allocate ARP4754A objectives and activities to each side of the aircraft/engine interface. Using this guidance, certification applicants (aircraft and engine manufacturers) will be able to make proposals to coordinate their activities with their respective authority based on this allocation with the objective of distributing efficiently the compliance demonstration efforts between engine and aircraft certification and of avoiding unnecessary duplication of work.
2017-03-02
WIP Standard
J1113/11
This SAE Standard defines methods and apparatus to evaluate electronic devices for immunity to potential interference from conducted transients along battery feed or switched ignition inputs. Test apparatus specifications outlined in this procedure were developed for components installed in vehicles with 12-V systems (passenger cars and light trucks, 12-V heavy-duty trucks, and vehicles with 24-V systems). Presently, it is not intended for use on other input/output (I/O) lines of the device under test (DUT).
CURRENT
2017-02-09
Standard
ARP1705C
The purpose of this procedure is to establish a technique for reliably and repeatedly measuring the RF shielding characteristics of EMI gasket materials and EMI gaskets against various joint surfaces. The procedure is also used to test the reliability of the gasketed joint combinations after being subjected to hostile environments.
CURRENT
2016-12-06
Standard
J1939/11_201612
This document defines a physical layer having a robust immunity to EMI and physical properties suitable for harsh environments. CAN controllers are available which support the CAN Flexible Data Rate Frame Format. These controllers, when used on SAE J1939-11 networks, must be restricted to use only the Classical Frame Format compliant to ISO 11898-1:2015. These SAE Recommended Practices are intended for light- and heavy-duty vehicles on- or off-road as well as appropriate stationary applications which use vehicle derived components (e.g., generator sets). Vehicles of interest include but are not limited to: on- and off-highway trucks and their trailers; construction equipment; and agricultural equipment and implements.
CURRENT
2016-09-16
Standard
J1752/2_201609
This SAE Recommended Practice defines a method for evaluating the near field electric or magnetic component of the electromagnetic field at the surface of an integrated circuit (IC). This technique is capable of providing a detailed pattern of the RF sources internal to the IC. The resolution of the pattern is determined by the characteristics of the probes used and the precision of the mechanical probe positioner. The method is usable over the 10 MHz to 3 GHz frequency range with existing probe technology. The probe is mechanically scanned according to a programmed pattern in a plane parallel or perpendicular to the IC surface and the data is computer processed to provide a color-enhanced representation of field strength at the scan frequency. This procedure is applicable to measurements from an IC mounted on any circuit board that is accessible to the scan probe. For comparisons, the standardized test board shall be used.
2016-09-13
WIP Standard
AIR5060B
The purpose of this document is to provide reference material for establishing compatibility of electronic gas turbine engine control systems and associated components with the electromagnetic environment and achieving compliance with associated airworthiness requirements.
2016-09-07
WIP Standard
AS20708/31B
No Scope Available
2016-09-07
WIP Standard
AS20708/39C
This specification covers the detail requirements for control transformer synchro, type 19CTB4b, 90 volt, 400 cycle.
2016-08-17
WIP Standard
ARP4553B
This SAE Aerospace Recommended Practice (ARP) is intended to provide design and qualification requirements for self-displacing hydraulic accumulators.

These requirements are intended to be included in the Producrement Specification for the accumulator. Those requirements identified by the use of "shall" are considered to be essential requirements; those requirements identified by the use of "should" are considered to be optional requirements for inclusion in the Specificaiton at the discretion of the Purchaser.

In addition, test methods for production acceptance and qualification purposes are provided.

The accumulator is intended for use in military aerospace hydraulic systems with rated pressures of up to 8000 psi (55,158 kPa) and of the following types as specified in SAE AS 5440: Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature; Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature.

CURRENT
2016-08-01
Standard
AIR6236A
This AIR provides guidance to the EMI test facility on how to check performance of the following types of EMI test equipment: Current probe Line Impedance Stabilization Network (LISN) Directional coupler Attenuator Cable loss Low noise preamplifier Rod antenna base Passive antennas All performance checks can be performed without software. A computer may be required to generate an electronic or hard copy of data. This is not to say that custom software might not be helpful; just that the procedures documented herein specifically eschew the necessity of automated operation.
Viewing 1 to 30 of 439

Filter

  • Standard
    439