Accident Aerospatiale AS350BA N189ND,
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ASN Wikibase Occurrence # 385381
 
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Date:Tuesday 3 October 2000
Time:14:30 LT
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
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:
cover
  
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/timeContributorUpdates
04-Apr-2024 18:00 ASN Update Bot Added

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