No fatalities

10 Jun 2017: HUGHES 269C (N7482F) — Tallulah, LA

Tallulah, LA, United States

On 10 Jun 2017, a HUGHES 269C (registration N7482F) was involved in an aviation accident near Tallulah, LA. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to reset the cyclic trim before takeoff, which resulted in ground resonance. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Hughes 269C helicopter was substantially damaged during a ground resonance event after takeoff at Vicksburg Tallulah Regional Airport in Louisiana. The pilot was not injured.

Accident Details

On June 10, 2017, at approximately 1320 central daylight time, a Hughes 269C helicopter bearing registration N7482F sustained substantial damage in a ground resonance event at Vicksburg Tallulah Regional Airport (TVR) in Tallulah, Louisiana. The helicopter, owned by Wade and Son, Inc., was being operated by the pilot under 14 Code of Federal Regulations Part 91 as an instructional flight. Day visual meteorological conditions prevailed at the time of the accident, and the flight was not operated on a flight plan. The local flight was originating when the incident occurred.

Pilot's Account

According to the pilot, the cyclic trim had not been re-centered before takeoff as specified in the checklist, remaining in a nearly full forward position from a previous flight. The engine start and run-up were normal. As the pilot applied full power for takeoff, the helicopter began to vibrate. He rolled the throttle off and lowered the collective, but the vibrations worsened, and the helicopter "began to destroy itself." The pilot noted that if the cyclic had been centered, the vibrations would have stopped; however, with the trim full forward, the rotor blades struck the stops, causing the vibrations. He added that there were no malfunctions or failures with the helicopter before the accident.

Postaccident Examination

After the helicopter came to rest upright on the airport ramp, an examination revealed that the engine had partially separated from the airframe and the main rotor gearbox had separated from the rear bulkhead. The landing skid dampers appeared intact, with no visible damage or fluid leakage.

Contributing factors

Pilot