20071123827409A

Accident · Substantial damage

FAA accident report · Hiller UH-12E · Somerton, AZ · November 23, 2007

Date
November 23, 2007 · 19:30 local
Place
Somerton, AZ
Phase of flight
Low Level Operations
Operating rules
Agricultural (Part 137)
Operator
RBKG
Damage
Substantial damage
Aircraft
N104EA
NTSB investigation
NTSBSEA08LA038
Reported as
Hiller UH12E
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,200 total160 in this make and model50 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.

(-23) On November 23, 2007, about 1930 MST, a Hiller UH-12E helicopter, N104EA, sustained substantial damage during a forced landing following an in-flight separation of a control rotor, about three miles northeast of yuma, Arizona. The helicopter is registered to tri-rotor spray and chemical of ulysses, Kansas, and operated under the provisions of title 14, CFR part 137. The commercial pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the aerial application flight that originated near yuma approximately 10 minutes prior to the accident. According to the pilot, he was conducting an aerial application on a crop. As the helicopter flew over a set of power lines, the pilot felt an extreme vibration and initiated a forced landing. Post-accident examination of the helicopter, by the pilot and operator, revealed that a control rotor had separated from the rotor system. The separated control rotor was found in the area where the vibration started.

As the FAA filed it

(-23) ON NOVEMBER 23, 2007, ABOUT 1930 MST, A HILLER UH-12E HELICOPTER, N104EA, SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING FOLLOWING AN IN-FLIGHT SEPARATION OF A CONTROL ROTOR, ABOUT THREE MILES NORTHEAST OF YUMA, ARIZONA. THE HELICOPTER IS REGISTERED TO TRI-ROTOR SPRAY AND CHEMICAL OF ULYSSES, KANSAS, AND OPERATED UNDER THE PROVISIONS OF TITLE 14, CFR PART 137. THE COMMERCIAL PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE AERIAL APPLICATION FLIGHT THAT ORIGINATED NEAR YUMA APPROXIMATELY 10 MINUTES PRIOR TO THE ACCIDENT. ACCORDING TO THE PILOT, HE WAS CONDUCTING AN AERIAL APPLICATION ON A CROP. AS THE HELICOPTER FLEW OVER A SET OF POWER LINES, THE PILOT FELT AN EXTREME VIBRATION AND INITIATED A FORCED LANDING. POST-ACCIDENT EXAMINATION OF THE HELICOPTER, BY THE PILOT AND OPERATOR, REVEALED THAT A CONTROL ROTOR HAD SEPARATED FROM THE ROTOR SYSTEM. THE SEPARATED CONTROL ROTOR WAS FOUND IN THE AREA WHERE THE VIBRATION STARTED.

NTSB investigation

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