This specification establishes requirements for plastic convoluted tubing that provides mechanical protection and support for electric wire bundles. The continuous operating temperatures range from -67°F (-55°C) to 500°F (260°C) (see 6.1).
This SAE Aerospace Recommended Practice (ARP) specifies the methods, equipment, and materials to be used in the installation, mounting, and testing of receptacle connectors used in pressure differential applications requiring an effective connector seal.
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.
This ARP specifies the methods, equipment, and materials to be used in the installation, mounting, and testing of receptacle connectors used in pressure differential applications requiring an effective connector seal.
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.
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.
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.