Skip to content

CEN13CA053

2012-11-06 · Bryan, Texas, United States · None · 1 aircraft · Status: Completed

Airport CFD

N131AA has since been reassigned. It is now registered to a different aircraft (PIPER PA-46-600TP, built 2019), which was not involved in this event.

Aircraft involved

Probable cause & findings

The pilot’s over-correction in an attempt to stabilize the helicopter during liftoff.

Factual narrative

The pilot who held a commercial pilot certificate with single-engine land airplane ratings was receiving training to obtain a helicopter rating. The pilot had 31 hours of helicopter flight time and the accident occurred on his second solo flight. The pilot reported he was attempting to takeoff from a wet grass area when the accident occurred. He stated that when he increased the collective to lift off, the helicopter began to roll to the right with the right skid still on the ground. He moved the cyclic to the left and the helicopter responded by rolling to the left with the left skid contacting the ground. The pilot then applied right cyclic and the helicopter again rolled to the right. The right skid contacted the ground and the helicopter rolled over onto it's right side. As a result of the accident, the main rotor blades and the helicopter fuselage were substantially damaged. The pilot reported that there were no preimpact mechanical failures/malfunctions that would have precluded normal operation. The pilot was receiving training to obtain a helicopter rating; he had 31 hours of helicopter flight time, and the accident occurred on his second solo flight. The pilot reported that he was attempting to take off from a wet grass area and that when he increased the collective to lift off, the helicopter began to roll to the right with the right skid still on the ground. He moved the cyclic to the left and the helicopter responded by rolling to the left with the left skid contacting the ground. The pilot then applied right cyclic and the helicopter again rolled to the right. The right skid contacted the ground, and the helicopter rolled over onto its right side. As a result of the accident, the main rotor blades and the helicopter fuselage were substantially damaged. The pilot reported that there were no preimpact 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-(general)-(general)-Incorrect use/operation - C

Verbatim from NTSB's published report. Source file NTSB_2012_CEN13CA053.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.