(1) All cargo hooks must have a primary and secondary release mechanism designed and installed as to prevent inadvertent operation. The hooks primary and secondary release must be tested prior to each day's operation to determine that the release functions properly.
(2) No employee will be permitted to work under a hovering helicopter(s) unless the cargo hooks used comply with Federal Aviation Administration regulations governing such hooks.
[Statutory Authority: RCW
49.17.010,
49.17.040,
49.17.050,
49.17.060 and chapter
49.17 RCW. WSR 19-13-083, § 296-45-67522, filed 6/18/19, effective 8/1/19; WSR 16-10-081, § 296-45-67522, filed 5/3/16, effective 7/1/16.]