This report defines the guidelines for a COMMON TERMINATION METHOD for aerospace vehicle electrical wiring systems and shows how designers can select a minimum number of different parts, among preferred connecting devices that will satisfy all system requirements while achieving the objective of minimum cost in procurement, assembly and maintenance without compromising quality or reliability.
Splices furnished in accordance with this specification shall be one type, disconnect splice assembly, of the sizes shown in Figure 1 as specified (see 6.2).
This specification covers tools used to install tiedown straps on wire bundles and for installing connector accessory shield termination bands (see 6.1).