20121020028999A

Accident · Destroyed

FAA accident report · William D Hunthrop AUTOGYRO MTO SPORT · Cresson, TX · October 20, 2012

Date
October 20, 2012 · 10:46 local
Place
Cresson, TX
Airport
Bourland Field
Phase of flight
Takeoff: Rotation
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N589DH
NTSB investigation
NTSBCEN13CA017
Reported as
William D Hunthrop Autogyro MTO Sport
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
11 in this make and model11 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.

Pilot was doing pattern work in recently built gyroplane. Winds exceeded crosswind limitation specified by flight instructor in pilot's logbook. Winds were 30 degrees differential at 14 gusting 20 knots. His limitation was 9 knots. The limitation did not stipulate this limitation as a crosswind limitation.

Pilot landed with a side load and went into the grass along edge of runway. Pilot got the aircraft back on runway and began another takeoff roll. Pilot attempted to rotate but due to either low main rotor RPM or a flat blade angle, the main rotor blades struck the runway behind aircraft numerous times, shearing off two feet or so of the main rotor. The aircraft became unstable and veered off the runway, coming to rest on its side. The pilot sustained serious injuries.

As the FAA filed it

PILOT WAS DOING PATTERN WORK IN RECENTLY BUILT GYROPLANE. WINDS EXCEEDED CROSSWIND LIMITATION SPECIFIED BY FLIGHT INSTRUCTOR IN PILOT'S LOGBOOK. WINDS WERE 30 DEGREES DIFFERENTIAL AT 14 GUSTING 20 KNOTS. HIS LIMITATION WAS 9 KNOTS. THE LIMITATION DID NOT STIPULATE THIS LIMITATION AS A CROSSWIND LIMITATION.

PILOT LANDED WITH A SIDE LOAD AND WENT INTO THE GRASS ALONG EDGE OF RUNWAY. PILOT GOT THE AIRCRAFT BACK ON RUNWAY AND BEGAN ANOTHER TAKEOFF ROLL. PILOT ATTEMPTED TO ROTATE BUT DUE TO EITHER LOW MAIN ROTOR RPM OR A FLAT BLADE ANGLE, THE MAIN ROTOR BLADES STRUCK THE RUNWAY BEHIND AIRCRAFT NUMEROUS TIMES, SHEARING OFF TWO FEET OR SO OF THE MAIN ROTOR. THE AIRCRAFT BECAME UNSTABLE AND VEERED OFF THE RUNWAY, COMING TO REST ON ITS SIDE. THE PILOT SUSTAINED SERIOUS INJURIES.

NTSB investigation

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