20000722020829A

Accident · Substantial damage

FAA accident report · Bell 206A-1 · Bennettsville, NC · July 22, 2000

Date
July 22, 2000 · 13:00 local
Place
Bennettsville, NC
Phase of flight
To Vertical (Helicopter Only)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N136C
NTSB investigation
NTSBMIA00LA227
Reported as
Bell 206A1
People aboard
1
Fatal injuries
0
Pilot’s flight hours
483 total15 in this make and model16 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)The pilot lost control on lift off. The aircraft made a hard swerving right turn and landed on right side resulting in substantial damage. The aircraft had two passengers on board, both weighting over 200 pounds. The pilot weighed approximately 300 pounds and the fuel was nearly to the top. (.4) according to the pilot and one passenger, the rotorcraft lifted off the airstrip to about a 2 to 3 foot hover, and immediately commenced a violent right spin that terminated with the landing skid and nose colliding with the terrain. The main rotor severed the tail boom and collided with the terrain, resulting in the rotorcraft rolling over on its right side. The FAA reported the wreckage revealed no evidence of mechanical failure, and that the rotorcraft was within its maximum takeoff weight and loading limits. The density altitude was 2,206 feet.

As the FAA filed it

(-23)THE PILOT LOST CONTROL ON LIFT OFF. THE AIRCRAFT MADE A HARD SWERVING RIGHT TURN AND LANDED ON RIGHT SIDE RESULTING IN SUBSTANTIAL DAMAGE. THE AIRCRAFT HAD TWO PASSENGERS ON BOARD, BOTH WEIGHTING OVER 200 POUNDS. THE PILOT WEIGHED APPROXIMATELY 300 POUNDS AND THE FUEL WAS NEARLY TO THE TOP. (.4) ACCORDING TO THE PILOT AND ONE PASSENGER, THE ROTORCRAFT LIFTED OFF THE AIRSTRIP TO ABOUT A 2 TO 3 FOOT HOVER, AND IMMEDIATELY COMMENCED A VIOLENT RIGHT SPIN THAT TERMINATED WITH THE LANDING SKID AND NOSE COLLIDING WITH THE TERRAIN. THE MAIN ROTOR SEVERED THE TAIL BOOM AND COLLIDED WITH THE TERRAIN, RESULTING IN THE ROTORCRAFT ROLLING OVER ON ITS RIGHT SIDE. THE FAA REPORTED THE WRECKAGE REVEALED NO EVIDENCE OF MECHANICAL FAILURE, AND THAT THE ROTORCRAFT WAS WITHIN ITS MAXIMUM TAKEOFF WEIGHT AND LOADING LIMITS. THE DENSITY ALTITUDE WAS 2,206 FEET.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.