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ASN Wikibase Occurrence # 41008
Last updated: 15 November 2019
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Date:29-JUN-2000
Time:09:35
Type:Silhouette image of generic UH1 model; specific model in this crash may look slightly different
Bell HH-1K (Garlick)
Owner/operator:RPI Helicopters
Registration: N896RP
C/n / msn: 157198
Fatalities:Fatalities: 1 / Occupants: 1
Other fatalities:0
Aircraft damage: Written off (damaged beyond repair)
Category:Accident
Location:Live Oak, CA -   United States of America
Phase: En route
Nature:Agricultural
Departure airport:Yuba City, CA (O52)
Destination airport:
Investigating agency: NTSB
Narrative:
The restricted category helicopter was operating on an agricultural application flight. The pilot radioed his ground crew words to the effect that he was experiencing a structural failure. Witnesses heard the helicopter make a loud noise and when they looked up it was falling straight down from about 100 feet agl. The tail boom and tail rotor assembly were found together about 300 feet from the fuselage wreckage. The main rotor blades remained attached to the main rotor hub. The tail boom separated from the forward fuselage about 6 feet forward of the horizontal stabilizer in proximity of one of the tail rotor drive shaft couplings. The tail boom skin sections were separated at right angles to the tail boom axis, and exhibited tension tearing on the left side and compression buckling on the right side. The skin separation surfaces exhibited a shiny, uniform, bright gray appearance. The tail boom skin thickness in the area of the separation matched the manufacturer's drawing specifications. The separation surfaces of the anti-torque control tube were collapsed and exhibited a uniform shiny appearance. Circumferential scrape marks and paint transfer on the drive shaft near the coupling resembled marks on the top of the tail boom adjacent to the point of separation. The star spline gear teeth of the coupling were worn at a 45-degree angle, accompanied by circumferential gouging about 1/8-inch deep on the adjoining collar. When compared with other couplings on the drive shaft, the interior cavity of this coupling appeared dry and did not exhibit appreciable lubricant (grease). No wire or other external object impact marks were observed on the tail boom.
Probable Cause: The inadequate lubrication of the tail rotor drive shaft coupling by unknown maintenance personnel that resulted in the in-flight failure and separation of the helicopter's tail boom.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20001212X21281&key=1


Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:23 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Nov-2017 14:18 TB Updated [Aircraft type, Operator, Source, Narrative]
12-Dec-2017 18:50 ASN Update Bot Updated [Operator, Source, Narrative]

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