ASN Wikibase Occurrence # 385381
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Date: | Tuesday 3 October 2000 |
Time: | 14:30 LT |
Type: | Aerospatiale AS350BA |
Owner/operator: | Vortex Helicopters, LLC |
Registration: | N189ND |
MSN: | 2152 |
Year of manufacture: | 1988 |
Total airframe hrs: | 5764 hours |
Engine model: | Turbomeca ARRIEL 1B |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | El Cajon, CA -
United States of America
|
Phase: | Landing |
Nature: | Ferry/positioning |
Departure airport: | (KSEE) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:While positioning the helicopter from the ground to a storage cart, the pilot lost directional, made a hard landing, and the tail boom struck the ground. Prior to the loss of directional control, the pilot saw something depart the tail section. He attributed the loss of directional control to a tail rotor failure. He initiated an autorotation over the landing cart. He maneuvered away from the cart in order to land on the ground and prevent a partial landing on the cart. The on-scene investigation revealed the aft drive shaft coupling was detached from the tail rotor drive shaft. Three bolts retain the coupling. One bolt was found attached to the coupling, another bolt was found on the ground, and the third bolt, and two of the retaining nuts, were not located. Neither bolt exhibited stripped threads or deformation. The last maintenance performed on the helicopter was by the previous owner. A track and balance of the tail rotor system was performed about 48 flight hours prior to the accident. According to the manufacturer's maintenance instructions, the balancing is accomplished by placement of washers under the nuts that are used to secure the bolts that attach to the aft drive shaft coupling. These are the same nuts that were not located at the accident site. Maintenance instructions also specify that the bolts in this area should be checked for proper torque and safety after an inspection.
Probable Cause: Improper torquing procedure of the aft tail rotor drive shaft coupling by maintenance personnel after tracking the tail rotor.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | LAX01LA009 |
Status: | Investigation completed |
Duration: | 1 year 1 month |
Download report: | Final report |
|
Sources:
NTSB LAX01LA009
Location
Revision history:
Date/time | Contributor | Updates |
04-Apr-2024 18:00 |
ASN Update Bot |
Added |
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