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CURRENT
2017-04-20
Standard
AS20708/68B
Scope is unavailable.
CURRENT
2017-04-20
Standard
AS20708/62B
Scope is unavailable.
CURRENT
2017-04-20
Standard
AS20708/76B
Scope is unavailable.
CURRENT
2017-04-20
Standard
AS20708/70B
No Scope Available
CURRENT
2017-04-20
Standard
AS20708/78B
Scope is unavailable.
CURRENT
2017-04-19
Standard
AS20708/66B
No Scope Available
CURRENT
2017-04-19
Standard
AS20708/79B
No Scope Available
CURRENT
2017-04-19
Standard
AS20708/80B
SCOPE IS UNAVAILABLE.
2017-04-18
WIP Standard
AS20708/139B
No scope available.
CURRENT
2017-04-18
Standard
AS20708/74B
No Scope Available
CURRENT
2017-04-18
Standard
AS20708/67B
No Scope Available
2017-04-18
WIP Standard
AS20708/81B
No Scope Available
2017-04-18
WIP Standard
AS20708/94C
This specification covers the detail requirements for 115 volt, 60 and 400 Hz, size 23 synchros.
2017-04-18
WIP Standard
AS20708/131B
no scope available
2017-04-18
WIP Standard
AS20708/500B
No Scope Available
2017-04-10
WIP Standard
J1752/3
This measurement procedure defines a method for measuring the electromagnetic radiation from an integrated circuit (IC). The IC being evaluated is mounted on an IC test printed circuit board (PCB) that is clamped to a mating port (referred to as a wall port) cut in the top or bottom of a TEM or wideband TEM (GTEM) cell. The test board is not in the cell as in the conventional usage but becomes a part of the cell wall. This method is applicable to any TEM or GTEM cell modified to incorporate the wall port; however, the measured RF voltage is affected by the septum to test board (wall) spacing. This procedure was developed using a 1 GHz TEM cell with a septum to wall spacing of 45 mm and a GTEM cell with average septum to wall spacing of 45 mm over the port area. Other cells may not produce identical spectral output but may be used for comparative measurements, subject to their frequency and sensitivity limitations.
2017-04-05
WIP Standard
ARP6078A
The Aerospace Recommended Practices of this document are intended for nitrogen-based Flammability Reduction Means (FRM) implemented on transport category, turbine powered airplanes. The recommended practices herein, therefore, relate only to the transport category aircraft, and focus specifically on contemporary inerting systems equipment. Such systems are referred to a Fuel Tank Inerting Systems (FTIS) in this document. This document does not cover the following: - Military aircraft applications - Air separation technologies other than hollow fiber membrane (HFM) and pressure swing adsorption (PSA) - Inerting of conventional unheated wing tanks or aircraft dry bays - Expected future technology solutions for the generation of inert gas. The advice contained in this document is aimed towards providing aircraft manufacturers with guidance on the key issues associated with contemporary aircraft fuel tank inerting systems to supplement the guidance in FAA Advisory Circular AC 25.981-2.
CURRENT
2017-04-03
Standard
AIR6127
This SAE Aerospace Information Report (AIR) considers the issue of proper design guidance for high voltage electrical systems used in aerospace applications. This document is focused on electrical discharge mechanisms including partial discharge and does not address personnel safety. Key areas of concern when using high voltage in aerospace applications are power conversion devices, electrical machines, connectors and cabling/wiring. The interaction between components and subsystems will be discussed. The AIR is intended for application to high voltage systems used in aerospace vehicles operating to a maximum altitude of 30000 m (approximately 100000 feet), and maximum operating voltages of below 1500 VRMS (AC)/1500 V peak (DC). These upper voltage limits have been incorporated because this report focuses on extending the operating voltage of non-propulsive electrical systems beyond that of existing aerospace systems.
CURRENT
2017-03-21
Standard
AS20708/46B
CURRENT
2017-03-21
Standard
AS20708/50B
CURRENT
2017-03-21
Standard
AS20708/52B
CURRENT
2017-03-21
Standard
AS20708/53B
CURRENT
2017-03-21
Standard
AS20708/55B
CURRENT
2017-03-21
Standard
AS20708/56B
CURRENT
2017-03-20
Standard
AS20708/47B
CURRENT
2017-03-20
Standard
AS20708/49B
CURRENT
2017-03-20
Standard
AS20708/48B
CURRENT
2017-03-20
Standard
AS20708/54B
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).
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