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Vehicle dynamics Vehicles and equipment AE-8C1 Connectors Committee Rollover accidents Aircraft operations

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Standard

Torque, Threaded Application, Electrical Connector, Accessory and Terminal Board Installation
2013-01-03
HISTORICAL
AIR6151A
This SAE Aerospace Information Report (AIR) is intended to provide guidelines to tightening methods and torque values as applied to electrical connectors, related hardware and switches, relays, circuit breakers and A-A-59125 type terminal boards. The connectors and associated hardware discussed herein, are typically manufactured from aluminum alloy, high grade engineering thermoplastics or corrosion resistant steel and typically plated with a protective/conductive coating. These guidelines may be used where no rules have been mandated either contractually or otherwise.
Standard

Torque, Threaded Application, Electrical Connector, Accessory and Terminal Board Installation
2019-03-05
HISTORICAL
AIR6151B
This SAE Aerospace Information Report (AIR) is intended to provide guidelines to tightening methods and torque values as applied to electrical connectors, related hardware and switches, relays, circuit breakers and A-A-59125 type terminal boards. The connectors and associated hardware discussed herein, are typically manufactured from aluminum alloy, high grade engineering thermoplastics or corrosion resistant steel and typically plated with a protective/conductive coating. These guidelines may be used where no rules have been mandated either contractually or otherwise.
Standard

Torque, Threaded Application, Electrical Connector and Accessory Installation
2011-05-18
HISTORICAL
AIR6151
This SAE Aerospace Information Report (AIR) is intended to provide guidelines to tightening methods and torque values as applied to electrical connectors and related hardware. The connectors and associated hardware discussed herein, are typically manufactured from aluminum alloy, high grade engineering thermoplastics or corrosion resistant steel and typically plated with a protective/conductive coating. These guidelines may be used where no rules have been mandated either contractually or otherwise.
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

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.
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

MILITARY COMPOSITE ELECTRICAL CONNECTORS
1994-02-01
HISTORICAL
AIR4567
This SAE Aerospace Information Report (AIR) establishes guidelines for evaluating composite electrical connectors and accessories.
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 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

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

Contacts, Electrical Connector, General Specification for
2022-01-28
CURRENT
AS39029E
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1) with stranded conductor wire. The contacts shall be capable of operating within the temperature range as specified (see 3.1).
Standard

Contacts, Electrical Connector, General Specification For
2011-01-13
HISTORICAL
AS39029B
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1) with stranded conductor wire. The contacts shall be capable of operating within the temperature range as specified (see 3.1).
Standard

Contacts, Electrical Connector, General Specification For
2006-06-29
HISTORICAL
AS39029A
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1) with stranded conductor wire. The contacts shall be capable of operating within the temperature range as specified (see 3.1).
Standard

Contacts, Electrical Connector, General Specification For
2017-01-19
HISTORICAL
AS39029D
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1) with stranded conductor wire. The contacts shall be capable of operating within the temperature range as specified (see 3.1).
Standard

Contacts, Electrical Connector, General Specification For
2011-11-22
HISTORICAL
AS39029C
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1) with stranded conductor wire. The contacts shall be capable of operating within the temperature range as specified (see 3.1).
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.
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