20170318021609I

Incident · Minor damage

FAA incident report · Bell 412EP · Decatur, TX · March 18, 2017

Date
March 18, 2017 · 09:10 local
Place
Decatur, TX
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Operator
UX9R
Damage
Minor damage
Aircraft
N87AM
Reported as
Bell 412EP
Reported engine
Pratt & Whitney Canada PT6T-3D
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, commercial pilot, flight instructor

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 March 18, 2017 at 0910 at the united rotorcraft facility in Decatur, Texas, a maintenance run on a Bell 412 was being performed by one technician and one contract pilot. The engine cowlings were removed. Per the test, the helicopter became airborne 2-3 feet. The technician saw a ladder had been left nearby and alerted the pilot who knowingly turned the helicopter left to avoid the perceived danger as the tail rotor struck the nearby facility perimeter fence removing approx. 6 inches of each tail rotor blade. The helicopter rotated twice in a clockwise direction before the pilot landed it safely. No injuries, but there was composite tail rotor blade damage. The helicopter did not intend to perform a flight, it was a maintenance test result.

As the FAA filed it

ON MARCH 18, 2017 AT 0910 AT THE UNITED ROTORCRAFT FACILITY IN DECATUR, TEXAS, A MAINTENANCE RUN ON A BELL 412 WAS BEING PERFORMED BY ONE TECHNICIAN AND ONE CONTRACT PILOT. THE ENGINE COWLINGS WERE REMOVED. PER THE TEST, THE HELICOPTER BECAME AIRBORNE 2-3 FEET. THE TECHNICIAN SAW A LADDER HAD BEEN LEFT NEARBY AND ALERTED THE PILOT WHO KNOWINGLY TURNED THE HELICOPTER LEFT TO AVOID THE PERCEIVED DANGER AS THE TAIL ROTOR STRUCK THE NEARBY FACILITY PERIMETER FENCE REMOVING APPROX. 6 INCHES OF EACH TAIL ROTOR BLADE. THE HELICOPTER ROTATED TWICE IN A CLOCKWISE DIRECTION BEFORE THE PILOT LANDED IT SAFELY. NO INJURIES, BUT THERE WAS COMPOSITE TAIL ROTOR BLADE DAMAGE. THE HELICOPTER DID NOT INTEND TO PERFORM A FLIGHT, IT WAS A MAINTENANCE TEST RESULT.