20100728039219A

Accident · Destroyed

FAA accident report · Garlick Hel OH-58A+ · Newport, TN · July 28, 2010

Date
July 28, 2010 · 08:05 local
Place
Newport, TN
Phase of flight
Ground/Ramp/Ma
Operating rules
Agricultural (Part 137)
Damage
Destroyed
Aircraft
N48LA
NTSB investigation
NTSBERA10LA379
Reported as
Garlick Hel OH-58A+
Reported engine
Rolls-Royce 250-C20C
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
400 total90 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.

The pilot was increasing rotor blade pitch while in the take-off phase of flight. While still on the ground, helicopter experienced a rotor blade failure. Approximately a two foot section of the red blade tip separated from the main rotor blade; this separation created an imbalance of the rotor system. The imbalance caused the helicopter to pitch up, forcing the tail rotor into the ground. With the helicopter in a pitch up attitude, the rotor blades impacted the forward section of the fuselage, causing extensive damage to the cockpit section. The imbalance was of sufficent magnitude as to cause the transmission and rotor head assembly to break away from the transmission mounts. The helicopter was destroyed. No injuries to the pilot.

As the FAA filed it

THE PILOT WAS INCREASING ROTOR BLADE PITCH WHILE IN THE TAKE-OFF PHASE OF FLIGHT. WHILE STILL ON THE GROUND, HELICOPTER EXPERIENCED A ROTOR BLADE FAILURE. APPROXIMATELY A TWO FOOT SECTION OF THE RED BLADE TIP SEPARATED FROM THE MAIN ROTOR BLADE; THIS SEPARATION CREATED AN IMBALANCE OF THE ROTOR SYSTEM. THE IMBALANCE CAUSED THE HELICOPTER TO PITCH UP, FORCING THE TAIL ROTOR INTO THE GROUND. WITH THE HELICOPTER IN A PITCH UP ATTITUDE, THE ROTOR BLADES IMPACTED THE FORWARD SECTION OF THE FUSELAGE, CAUSING EXTENSIVE DAMAGE TO THE COCKPIT SECTION. THE IMBALANCE WAS OF SUFFICENT MAGNITUDE AS TO CAUSE THE TRANSMISSION AND ROTOR HEAD ASSEMBLY TO BREAK AWAY FROM THE TRANSMISSION MOUNTS. THE HELICOPTER WAS DESTROYED. NO INJURIES TO THE PILOT.

NTSB investigation

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