20250108000259A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R44 II · Buras, LA · January 8, 2025

Date
January 8, 2025 · 12:43 local
Place
Buras, LA
Airport
Matidora
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N430JM
NTSB investigation
NTSBCEN25LA073
Reported as
Robinson Helicopter R44 II
Reported engine
Lycoming IO-540 series
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
3,000 total53 in this make and model15 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.

After a brief flight, the helicopter came back to the runway and entered a hover to land. The winds were gusty and while attempting a right peddle turn to taxi down the runway, a gust of wind caught the tail rotor causing the helicopter to enter a loss of tail rotor effectiveness (lte). Once in lte, the helicopter control was lost, causing the tail rotor blades to contact the ground shearing off both blades, resulting in a spin to the left several times and impacted the runway in an upright condition. The impact caused substantial damage to the helicopter, broken nose to passenger and fractured back for the pilot. Both personnel exited the helicopter through the broken-out windscreen on the pilot side of the helicopter.

As the FAA filed it

AFTER A BRIEF FLIGHT, THE HELICOPTER CAME BACK TO THE RUNWAY AND ENTERED A HOVER TO LAND. THE WINDS WERE GUSTY AND WHILE ATTEMPTING A RIGHT PEDDLE TURN TO TAXI DOWN THE RUNWAY, A GUST OF WIND CAUGHT THE TAIL ROTOR CAUSING THE HELICOPTER TO ENTER A LOSS OF TAIL ROTOR EFFECTIVENESS (LTE). ONCE IN LTE, THE HELICOPTER CONTROL WAS LOST, CAUSING THE TAIL ROTOR BLADES TO CONTACT THE GROUND SHEARING OFF BOTH BLADES, RESULTING IN A SPIN TO THE LEFT SEVERAL TIMES AND IMPACTED THE RUNWAY IN AN UPRIGHT CONDITION. THE IMPACT CAUSED SUBSTANTIAL DAMAGE TO THE HELICOPTER, BROKEN NOSE TO PASSENGER AND FRACTURED BACK FOR THE PILOT. BOTH PERSONNEL EXITED THE HELICOPTER THROUGH THE BROKEN-OUT WINDSCREEN ON THE PILOT SIDE OF THE HELICOPTER.

NTSB investigation

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