N7482F

Substantial
None

HUGHES 269CS/N: 170576

Accident Details

Date
Saturday, June 10, 2017
NTSB Number
CEN17LA229
Location
Tallulah, LA
Event ID
20170613X14632
Coordinates
32.351665, -91.027778
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to reset the cyclic trim before takeoff, which resulted in ground resonance.

Aircraft Information

Registration
Make
HUGHES
Serial Number
170576
Engine Type
Reciprocating
Model / ICAO
269C
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
SCHWEIZER RSG LLC
Address
3901 N MAIN ST
City
FORT WORTH
State / Zip Code
TX 76106-2723
Country
United States

Analysis

On June 10, 2017, about 1320 central daylight time, a Hughes 269C helicopter, N7482F, was substantially damaged during a ground resonance event at the Vicksburg Tallulah Regional Airport (TVR), Tallulah, Louisiana. The pilot was not injured. The helicopter was registered to Wade and Son, Inc., and operated by the pilot as a 14 Code of Federal Regulations Part 91 instructional flight. Day visual meteorological conditions prevailed at the accident site. The flight was not operated on a flight plan. The local flight was originating at the time of the accident.The pilot reported that the cyclic trim was not re-centered before takeoff as noted on the checklist. Instead, it remained at a nearly full forward position from the previous flight. The engine start and run-up were normal. At full power for takeoff, the helicopter began to vibrate. The pilot "rolled the throttle off" and lowered the collective; however, the vibrations became worse and the helicopter "began to destroy itself." He noted that if the cyclic had been centered, the vibrations would have stopped. However, with the trim full forward, the rotor blades began hitting the stops causing the vibrations. The pilot added that there were no malfunctions or failures with the helicopter before the accident.

The helicopter came to rest upright on the airport ramp. A postaccident 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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN17LA229