BELL OH-58C near Panama City, FL — 2011-05-27
- Date
- 2011-05-27
- Location
- Panama City, FL, USA
- Airport
- PFN
- Aircraft
- BELL OH-58C
- Registration
- N82772
- Category
- Helicopter
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Hover
Probable cause
The drooping electrical conduit, which snagged the vertical fin and resulted in the pilot's inability to control the helicopter. Contributing to the accident was the operator's decision to have the pilot fly the helicopter out of the hangar.
NTSB narrative
The pilot was hover taxiing the helicopter straight out of an old, temporary hangar, as he had done numerous times. He estimated that the helicopter was about 3 feet above the ground, the last few feet of the tail were still inside the hangar, and he heard a loud bang. He started to lower the collective, but could not control the helicopter, which tipped over on its left side as it impacted the ground. Photographs showed that the main rotor blades had separated from the mast. The vertical tail fin had scrape marks on its top and the upper leading edge had an almost horizontal line several inches below the top. The tail rotor blades, which did not extend above the top of the vertical fin, were pristine. The hangar door overhead frame had three sets of scrape marks, with one angled about 30 degrees to the right and two sets angled about 20 to 25 degrees to the left. Electrical conduit would have normally been secured above the hangar door frame, but was drooped below it, separated and coiled. Remnants of the conduit, and the fact that the main rotor blade tips would have rotated above the vertical tail fin, indicate that the conduit likely had drooped below the hangar frame after the main rotor passage, then snagged the top of the vertical fin. The multiple sets of scrape marks at different angles on the underside of the overhead hangar frame indicate that the helicopter then likely pivoted several times while snagged, as the pilot lost control. No preexisting mechanical malfunctions were noted with the helicopter.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have checked for obstructions before hover-taxiing out of the hangar.
NTSB coding
Evidence available
- Photos
- 11 docket documents
Docket documents11
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Crewman Statementinterview
- Pilot Statementinterview
- Photo 1 - Helicopter on Its Side (Courtesy of Bay County Sheriff's Office)photos
- Photo 2 - Hangar; General Impact Area and Other Helicopter Inside (Courtesy of Bay County Sheriff's Office)photos
- Photo 3 - Broken Tailcone and Tail Rotor Drive Shaft (Courtesy of Bay County Sheriff's Office)photos
- Photo 4 - Aft Portion of Separated Tail Rotor Drive Shaft (with Rotational Scoring) (Courtesy of Pilot)photos
- Photo 5 - Upward View of Overhead Hangar Frame (Courtesy of Bay County Sheriff's Office)photos
- Photo 6 - Additional Upward View of Overhead Hangar Frame with Additional Marks (Courtesy of Bay County Sheriff's Office)photos
- Photo 7 - Hangar Door Area with Drooping Conduit; No Damage to Hangar Door (Courtesy of Bay County Sheriff's Office)photos
- Photo 8 - Damage to Vertical Fin; Almost Horizontal Line Leading Edge Near Top (Courtesy of Bay County Sheriff's Office)photos
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