Standard
CABLE ASSEMBLY EXTERNAL ELECTRIC POWER, AIRCRAFT 115/200 VOLT, 400 HERTZ
2009-09-03
HISTORICAL
AS90328
Search Results
Standard
HUBS, CONDUIT CONNECTION, STANDARD DIMENSIONS
2020-07-14
HISTORICAL
AS10051A
Standard
Conduit, Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations
2021-04-08
HISTORICAL
AS6136A
This specification covers the requirements for flexible shielded electrical conduit for aircraft installations.
Standard
Conduit, Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations
1998-08-01
HISTORICAL
AS6136
This specification covers the requirements for shielded electrical conduit for aircraft installations.
Standard
HUBS, CONDUIT CONNECTION, STANDARD DIMENSIONS
2023-05-22
CURRENT
AS10051B
Standard
Conduit, Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations
2023-05-22
CURRENT
AS6136B
This specification covers the requirements for flexible shielded electrical conduit for aircraft installations.
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT 28 VOLT DC, OPERATING POWER
2009-09-03
HISTORICAL
AS90347
Standard
FERRULE, FLEXIBLE CONDUIT, RADIO FREQUENCY SHIELDING
2021-11-16
CURRENT
AS25065B
Standard
CONDUIT ASSEMBLY, NUT, FLEXIBLE, RADIO FREQUENCY SHIELDING
2021-11-19
CURRENT
AS25066A
Standard
Cable Assemblies and Attachable Plugs, External Electrical Power, Aircraft, General Specification For
2019-04-10
WIP
AS7974B
This specification applies to complete cable assemblies (using either molded on or attachable plugs) used to connect external electric power to aircraft and to attachable plugs used as replacement for plugs damaged in service.
Standard
Cable Assemblies and Attachable Plugs, External Electrical Power, Aircraft, General Specification For
1998-01-01
HISTORICAL
AS7974
This specification applies to complete cable assemblies (using either molded on or attachable plugs) used to connect external electric power to aircraft and to attachable plugs used as replacement for plugs damaged in service.
Standard
Cable Assemblies and Attachable Plugs, External Electrical Power, Aircraft, General Specification For
2010-12-17
CURRENT
AS7974A
This specification applies to complete cable assemblies (using either molded on or attachable plugs) used to connect external electric power to aircraft and to attachable plugs used as replacement for plugs damaged in service.
Standard
Assembly and Soldering Criteria for High Quality/High Reliability Soldered Wire and Cable Termination in Aerospace Vehicles
2004-12-29
HISTORICAL
AS4461A
This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices, for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device.
Standard
Assembly and Soldering Criteria for High Quality/High Reliability Soldering Wire and Cable Termination in Aerospace Vehicles
2012-08-30
HISTORICAL
AS4461B
This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices, for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device.
Standard
Assembly and Soldering Criteria for High Quality/High Reliability Soldering Wire and Cable Termination in Aerospace Vehicles
2021-07-23
CURRENT
AS4461D
This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices, for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device.
Standard
Development, Verification, and Validation of a Thermal Model for Determining Current Derating Design Limits of Aerospace Wires and Wire Bundles
2021-08-18
CURRENT
ARP7987
The thermal modeling guidelines and best practices provided in this document are applicable to powered aerospace vehicle wires and wire bundles in thermal environments ranging from -65 to +260 °C (-85 to +500 °F) and pressures ranging from sea level to space vacuum. Currently the ARP only considers steady state and direct current conditions. The effects of wiring terminations and connectors are not addressed. Both can significantly impact the overall current derating and safety margins for a wiring system.
Standard
Transmission Lines, Transverse Electromagnetic Mode
2004-05-25
HISTORICAL
ARP81490
This document covers the general requirements for Transverse Electromagnetic Mode (TEM) Transmission Lines (see 6.4.14) intended for use in airborne systems.
Standard
Transmission Lines, Transverse Electromagnetic Mode
2020-10-30
CURRENT
ARP81490B
This document covers the general recommendations for Transverse Electromagnetic Mode (TEM) Transmission Lines intended for use in airborne systems (see 6.2.14). For U.S military applications, TEM Transmission Lines shall meet the requirements in accordance with MIL-T-81490. The follow index lists the recommended requirements and methods covered by the Aerospace Recommended Practice (ARP):
Standard
Wiring Aerospace Vehicle
2000-04-01
HISTORICAL
AS50881A
This specification covers all aspects from the selection through installation of wiring and wiring devices used in aerospace vehicles. Aerospace vehicles include airplanes, helicopters, lighter-than-air vehicles, and missiles.
