| 摘要 |
An aircraft battery lockout device is used to isolate the connector assembly for the aircraft's wiring harness from the battery power receptacle. In one embodiment the device comprises a cover, lock, and insulative material. The cover is locked onto the battery power receptacle. The insulative material provides electrical isolation between the locking device and the battery power receptacle. In a second embodiment the device is locked onto the connector assembly.
|
