Accident Schweizer 269C N3623U,
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ASN Wikibase Occurrence # 295619
 
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Date:Saturday 28 June 2003
Time:16:15 LT
Type:Silhouette image of generic H269 model; specific model in this crash may look slightly different    
Schweizer 269C
Owner/operator:K
Registration: N3623U
MSN: 1568
Total airframe hrs:3667 hours
Engine model:Lycoming HIO-360-D1A
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Bountiful, Utah -   United States of America
Phase: Unknown
Nature:Private
Departure airport:Bountiful-Salt Lake Skypark, UT (BTF/KBTF)
Destination airport:Bountiful-Salt Lake Skypark, UT (BTF/KBTF)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot was hover taxiing from the west side of the airport to his hangar on the east side. He said he had lifted the helicopter "up to about a three-foot hover," when the cyclic started to rotate "in about a six to eight inch circle" in his hand. The pilot reported he heard a "low pitch or frequency oscillation." The pilot said, "The helicopter started a strong uncontrollable roll to the left. I tried to push the cyclic to the right but found no change in stopping the roll or direction of movement." The pilot said that he knew there were airplanes and people in the direction the helicopter was heading. The pilot said he decided to put the helicopter down on its side to stop any further movement. A witness saw the helicopter lift off the ramp to approximately 3 to 5 feet. The tail rotor then struck the ramp and the helicopter impacted on its left side. An examination of the helicopter showed substantial damage to the main rotor blades, tail rotor, skids, and cockpit area. An examination of the helicopter's systems revealed no anomalies. The wind conditions in the area, approximately 30 minutes prior to the accident were 350 degrees at 11 knots with gusts to 16 knots. According to the mechanic who had performed the previous annual inspection on the helicopter, when in hover, the helicopter would experience a small amount of stick swirl. The mechanic said that "if you work it, it [the swirl] will go away."

Probable Cause: the pilot not maintaining aircraft control during the aerial taxi. Factors contributing to the accident were the oscillating cyclic, the pilot's diverted attention, and the gusting crosswind.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN03LA115
Status: Investigation completed
Duration: 6 months
Download report: Final report

Sources:

NTSB DEN03LA115

Revision history:

Date/timeContributorUpdates
13-Oct-2022 10:42 ASN Update Bot Added

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