20120517007979I

Incident · Minor damage

FAA incident report · Bell Helicopter Textron 206L-1 · Grand Canyon, AZ · May 17, 2012

Date
May 17, 2012 · 14:30 local
Place
Grand Canyon, AZ
Airport
Old Airport At Red Butte
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Operator
PG9A
Damage
Minor damage
Aircraft
N2072M
Reported as
Bell Helicopter Textron 206L-1
Reported engine
Allison 250 SER 250HP
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,033 total1,370 in this make and model51 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.

During a practice autorotation, the instructor failed to roll on throttle in a timely manner in order to perform a power recovery to a hover. The aircraft touched down and rocked forward. The incident was not noticed at the time and the flight instruction continued. After the flight, it was discovered that one of the main rotor blades struck one of the tail boom vertical stabilizers. The vertical stabilizer experienced minor damage and scuff marks were visible on the main rotor blade under camber .

As the FAA filed it

DURING A PRACTICE AUTOROTATION, THE INSTRUCTOR FAILED TO ROLL ON THROTTLE IN A TIMELY MANNER IN ORDER TO PERFORM A POWER RECOVERY TO A HOVER. THE AIRCRAFT TOUCHED DOWN AND ROCKED FORWARD. THE INCIDENT WAS NOT NOTICED AT THE TIME AND THE FLIGHT INSTRUCTION CONTINUED. AFTER THE FLIGHT, IT WAS DISCOVERED THAT ONE OF THE MAIN ROTOR BLADES STRUCK ONE OF THE TAIL BOOM VERTICAL STABILIZERS. THE VERTICAL STABILIZER EXPERIENCED MINOR DAMAGE AND SCUFF MARKS WERE VISIBLE ON THE MAIN ROTOR BLADE UNDER CAMBER .

Other reports on N2072M · 4

Matched to the same aircraft by N-number and date.