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Vehicle dynamics AE-8C1 Connectors Committee Aircraft

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Standard

Electrical Connectors for Aerospae, Shipboard, Ground Vehicles and Associated Equipment
2020-01-21
CURRENT
ARP1308D
The intent of this ARP is to identify electrical connectors maintained by the AE-8C1 Committee, to provide their general application characteristics, associated configuration options, and recommendations for new design (see 6.1.1), repair, and retrofit purposes (see 6.1). It is acknowledged the connectors listed herein will not completely satisfy all mobility vehicle and equipment requirements, but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors. This ARP only pertains to AS connector standards. See MIL-STD-1353 for U.S. military specification connector information.
Standard

PREFERRED ELECTRICAL CONNECTORS FOR AEROSPACE VEHICLES AND ASSOCIATED EQUIPMENT
2011-08-10
HISTORICAL
ARP1308
The intent of this ARP is to identify selected electrical connectors, their general application characteristics, and associated configuration options recommended for new design, repair, and retrofit purposes (see 6.1). It is acknowledged that those connectors listed herein will not completely satisfy all aerospace vehicle and equipment requirements but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors.
Standard

Connectors, Receptacle, External Electric Power, Aircraft, General Specification For
2009-11-18
HISTORICAL
AS81790_A3
This document has been taken directly from U.S. Military Specification MIL-C-81790A, Amendment 1 and contains only minor editorial and format changes required to bring it into conformance with the publishing requirements of SAE technical standards. The initial release of this document is intended to replace MIL-C-81790A, Amendment 1. Any part numbers established by the original specification remain unchanged. This specification covers the requirements for aircraft external electric power receptacles.
Standard

Preferred Electrical Connectors for Aerospace Vehicles and Associated Equipment
2002-03-23
HISTORICAL
ARP1308C
The intent of this ARP is to identify selected electrical connectors, their general application characteristics, and associated configuration options recommended for new design, repair, and retrofit purposes (see 6.1). It is acknowledged that those connectors listed herein will not completely satisfy all aerospace vehicle and equipment requirements but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors.
Standard

PREFERRED ELECTRICAL CONNECTORS FOR AEROSPACE VEHICLES AND ASSOCIATED EQUIPMENT
1991-11-01
HISTORICAL
ARP1308B
The intent of this ARP is to identify selected electrical connectors, their general application characteristics, and associated configuration options recommended for new design, repair, and retrofit purposes (see 6.1). It is acknowledged that those connectors listed herein will not completely satisfy all aerospace vehicle and equipment requirements but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors.
Standard

HIGH AND EXTENDED VIBRATION ENVIRONMENT
1991-11-01
HISTORICAL
AIR1557
This AIR defines aircraft vibration areas, the vibration spectrum for those areas and a coupling mechanism recommendation for circular electrical connectors.
Standard

ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF
1991-11-01
HISTORICAL
AIR1329A
This AIR defines the areas where incompatibility may exist between the selected wire and the electrical connector in which it is terminated and how to design for compatibility. Refer to ARP914 for a glossary of connection terms.
Standard

PREFERRED ELECTRICAL CONNECTORS FOR AEROSPACE VEHICLES AND ASSOCIATED EQUIPMENT
1977-10-01
HISTORICAL
ARP1308A
The intent of this ARP is to identify selected electrical connectors, their general application characteristics, and associated configuration options recommended for new design, repair, and retrofit purposes (see 6.1). It is acknowledged that those connectors listed herein will not completely satisfy all aerospace vehicle and equipment requirements but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors.
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