Standard
CABLE AND PLUG ASSEMBLY, EXTERNAL POWER 115/200 VOLTS 3 PHASE, SINGLE POINT REFUELING
2022-08-05
CURRENT
AS24208B
Search Results
Standard
CABLE ASSEMBLY EXTERNAL ELECTRIC POWER, AIRCRAFT 115/200 VOLT, 400 HERTZ
2021-08-05
CURRENT
AS90328A
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC, JET STARTING
2022-08-17
CURRENT
AS25019C
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC, JET STARTING
2022-05-16
HISTORICAL
AS25019B
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC, OPERATING POWER
2022-11-22
HISTORICAL
AS90347B
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, SINGLE-JACKETED 270 VDC, 90 KW
2015-04-16
HISTORICAL
AS7974/5
Standard
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, SINGLE-JACKETED 270 VDC, 90 KW
2017-07-07
CURRENT
AS7974/5A
Standard
CONDUIT, FLEXIBLE, RADIO FREQUENCY SHIELDING
2022-01-12
CURRENT
AS25064B
Standard
CONDUIT, FLEXIBLE, RADIO FREQUENCY SHIELDING
2016-11-11
HISTORICAL
AS25064A
Standard
CONDUIT, FLEXIBLE, RADIO FREQUENCY SHIELDING
2009-11-22
HISTORICAL
AS25064
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
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
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
Etching of Fluoropolymer Insulations
2019-06-11
CURRENT
ARP6167
This SAE Aerospace Recommended Practice (ARP) describes the etching of fluoropolymer electrical wire insulations to ensure that all facets of the process from the chemistry to the processing, to the storage and handling are well defined.
Standard
Guidelines for Harness Critical Clamp Locator Marker Installation on Electrical Cable Assemblies
2019-06-11
CURRENT
ARP5614
This ARP specifies the recommended methods of marking electrical wiring and harnesses to aid in the positioning/routing of electrical wiring, harnesses and cable assemblies.
Standard
Guidelines for Wire Identification Marking Using the Hot Stamp Process
2010-08-05
HISTORICAL
ARP5369A
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables.
Standard
Guidelines for Wire Identification Marking Using the Hot Stamp Process
2004-12-27
HISTORICAL
ARP5369
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables.
Standard
Guidelines for Wire Identification Marking Using the Hot Stamp Process
2016-12-01
CURRENT
ARP5369B
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables.
Standard
Legibility of Print on Aerospace Wires and Cables
2013-06-27
HISTORICAL
ARP5607A
The purpose of this report is to provide recommendations for marking wire and cable insulations to meet legibility requirements. This information is generic and applies to any type of wire marking system, such as an ultraviolet (UV) laser marking system or an inkjet or other ink based wire marking system. This report is limited to the legibility of human-readable characters and does not address bar code or other machine-readable symbols. In this report, the term wire refers to jacketed cables and fiber optic cables in addition to individual wires. This report defines the factors that affect the legibility of markings on wiring. Two generic types of variables affect legibility: stimulus variables and environmental variables. Stimulus variables are those factors involving the mark itself.
