20220630011539A

Accident · Substantial damage

FAA accident report · Bell Helicopter Textron Canada 206L-4 · Idabel, OK · June 30, 2022

Date
June 30, 2022 · 09:00 local
Place
Idabel, OK
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N378JC
NTSB investigation
NTSBCEN22LA294
Reported as
Bell Helicopter Textron Canada 206L-4
Reported engine
Rolls-Royce 250-C30P
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, commercial pilot, flight instructor
Pilot’s flight hours
4,015 total800 in this make and model100 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.

On June 30, 2022 at 0900 CDT, a pilot and flight instructor were performing practice autorotations to runway 2 at the Idabel airport. After touchdown on the runway, the pilot trainee abruptly lowered the collective while the main rotor was at a low rotor RPM. The main rotor blade flapped excessively causing the blade to flap downward striking and severing the tailboom causing substantial damage to the aircraft. There was no post crash fire. There were no injuries to the pilot and instructor pilot. Weather conditions at the time of the accident were visual meteorlogical conditions.

As the FAA filed it

ON JUNE 30, 2022 AT 0900 CDT, A PILOT AND FLIGHT INSTRUCTOR WERE PERFORMING PRACTICE AUTOROTATIONS TO RUNWAY 2 AT THE IDABEL AIRPORT. AFTER TOUCHDOWN ON THE RUNWAY, THE PILOT TRAINEE ABRUPTLY LOWERED THE COLLECTIVE WHILE THE MAIN ROTOR WAS AT A LOW ROTOR RPM. THE MAIN ROTOR BLADE FLAPPED EXCESSIVELY CAUSING THE BLADE TO FLAP DOWNWARD STRIKING AND SEVERING THE TAILBOOM CAUSING SUBSTANTIAL DAMAGE TO THE AIRCRAFT. THERE WAS NO POST CRASH FIRE. THERE WERE NO INJURIES TO THE PILOT AND INSTRUCTOR PILOT. WEATHER CONDITIONS AT THE TIME OF THE ACCIDENT WERE VISUAL METEORLOGICAL CONDITIONS.

NTSB investigation

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