Refine Your Search

Date

Date

Topic

Topic

Electrical systems Standard Metallurgy AE-8C1 Connectors Committee Magnesium alloys Electrical, Electronics, and Avionics Powder metallurgy

Search Results

Viewing 1 to 20 of 1355
123Next >Last >>
Sort by title
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
2024-01-16
CURRENT
AIR6151C
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

Reaffirmation Ballot
2023-09-28
WIP
F2023C1Reaffirm
Reaffirmation Ballot for AS85049/147A and AS85049/152A
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
2002-10-21
HISTORICAL
AIR4567A
This SAE Aerospace Information Report (AIR) establishes guidelines for evaluating composite electrical connectors and accessories.
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.
123Next >Last >>
X