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GAA20CA063

2019-11-10 · Lebanon, Indiana, United States · Minor · 1 aircraft · Status: Completed

Airport 6I4

Aircraft involved

Probable cause & findings

The pilot's failure to maintain proper clearance from a tractor trailer during landing.

Factual narrative

The helicopter pilot reported that he did a low-reconnaissance flight over the intended landing site, just to the east of a building. Shortly after, he realized that the landing site was changed to the west side of the building. He maneuvered the helicopter to a hover over a new landing site west of the building, about 75 feet above the ground, and started a vertical decent. During the decent, a company mechanic seated in left seat of the cockpit told the pilot of an obstacle to the left of the helicopter. He acknowledged seeing the obstacle and continued to descend. Shortly after touchdown, as the pilot reduced the throttle setting to idle, the main rotor blades struck an empty tractor trailer, the helicopter yawed, and the tail rotor blades struck the trailer. The helicopter sustained substantial damage to the main rotor and tail rotor systems. The director of operations reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The pilot reported that he conducted a low-reconnaissance flight in the helicopter over the intended landing site, which was just east of a building. Shortly after, he realized that the landing site had changed to west of the building. He maneuvered the helicopter to a hover over the new landing site about 75 ft above ground level and started a vertical descent. During the descent, a company mechanic seated in the left seat told the pilot of an obstacle left of the helicopter. He acknowledged seeing the obstacle and continued to descend. Shortly after touchdown, as the pilot reduced the throttle setting to idle, the main rotor blades struck a tractor trailer, the helicopter yawed, and the tail rotor blades struck the trailer. The helicopter sustained substantial damage to the main rotor and tail rotor systems. The director of operations reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Environmental issues-Physical environment-Object/animal/substance-Ground vehicle-Effect on equipment - C
  • C Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Pilot - C
  • — Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Maintenance personnel

Verbatim from NTSB's published report. Source file NTSB_2019_GAA20CA063.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.