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Narrative:While the aircraft was shutting down, the flight engineer exited the aircraft, and gave the pilots the signal that the droop stops had engaged. He then climbed up on a stepladder next to the tail boom as the main rotor continued to coast down to a stop. A minute or so later, the two remaining crewmembers heard a 'thump.' The pilot-in-command (PIC) asked the copilot to go outside and find the source of the noise. When he walked toward the rear of the aircraft he found the flight engineer laying across the top of tail boom with a massive head injury. The main rotor of the CH-54A is fully articulated. The rotor system employs a series of main rotor blade droop stops. As the rotor rpm slows, centripetal force is reduced and the droop stop springs pull the stops back into ground stop position. During spool down it can take 20 seconds or more for the first through sixth stop to move into the ground stop position. The visual strobe effect, caused by the turning rotor head, can make it appear that all the stops are in place when one or more stops still have not yet been fully repositioned. Winds were gusting up to 14 knots at the time of the shutdown. Gusting winds during shutdown can cause a slow turning rotor blade to suddenly flap down independently of the remaining blades. CAUSE: the flight engineer's decision to climb a step ladder that put him in close proximity to the still turning main rotor blades. The gusting wind was a factor in the accident.
Sikorsky CH-54A (S-64A)
|C/n / msn:|| 64-057|
|Fatalities:||Fatalities: 1 / Occupants: 3|
|Airplane damage:|| None|
|Location:||Elko, NV -
United States of America
|Departure airport:||Tooele, UT (YVY)|
|Destination airport:||Yuba City, CA (O52)|
Ex CH-54A Tarhe 68-18455 US Army
||Updated [Cn, Operator, Other fatalities, Source]|
||Updated [Aircraft type]|
||Updated [Time, Source, Narrative]|
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