20180511005259A

Accident · Substantial damage

FAA accident report · Bell OH-58C · Somerton, AZ · May 11, 2018

Date
May 11, 2018 · 20:05 local
Place
Somerton, AZ
Airport
Tri-Rotor Ag Services Airport
Phase of flight
Other, Specify
Operating rules
Agricultural (Part 137)
Operator
71TG
Damage
Substantial damage
Aircraft
N82857
NTSB investigation
NTSBWPR18LA140
Reported as
Bell OH-58C
Reported engine
Allison T63 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
16,000 total2,500 in this make and model100 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 lifted off at AZ25 for aerial application with 12-15 gallons of fuel and 98 gallons of product. After the first pass the pilot started a turn back to the field at approximately 20 knots and 45 degrees of bank. During the turn, the stick began to shake. The pilot completed the maneuver and leveled off. The stick shaking intensified and the low Rotor RPM illuminated. The pilot recalls the master warning also being lit. He continued on an east heading looking for a landing location. As the Rotor RPM continued to decrease he decided to set the helicopter down but still had forward momentum. On contact with the ground, the main Rotor flexed and struck the tail section, severing it from the fuselage. The helicopter yawed to the right with the left front skid making contact with the ground. This caused the helicopter to pitch up and roll onto its right side.

As the FAA filed it

THE PILOT LIFTED OFF AT AZ25 FOR AERIAL APPLICATION WITH 12-15 GALLONS OF FUEL AND 98 GALLONS OF PRODUCT. AFTER THE FIRST PASS THE PILOT STARTED A TURN BACK TO THE FIELD AT APPROXIMATELY 20 KNOTS AND 45 DEGREES OF BANK. DURING THE TURN, THE STICK BEGAN TO SHAKE. THE PILOT COMPLETED THE MANEUVER AND LEVELED OFF. THE STICK SHAKING INTENSIFIED AND THE LOW ROTOR RPM ILLUMINATED. THE PILOT RECALLS THE MASTER WARNING ALSO BEING LIT. HE CONTINUED ON AN EAST HEADING LOOKING FOR A LANDING LOCATION. AS THE ROTOR RPM CONTINUED TO DECREASE HE DECIDED TO SET THE HELICOPTER DOWN BUT STILL HAD FORWARD MOMENTUM. ON CONTACT WITH THE GROUND, THE MAIN ROTOR FLEXED AND STRUCK THE TAIL SECTION, SEVERING IT FROM THE FUSELAGE. THE HELICOPTER YAWED TO THE RIGHT WITH THE LEFT FRONT SKID MAKING CONTACT WITH THE GROUND. THIS CAUSED THE HELICOPTER TO PITCH UP AND ROLL ONTO ITS RIGHT SIDE.

NTSB investigation

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