20260903011919A

Accident · Substantial damage

FAA accident report · Bell OH-58A · Phoenix, AZ · September 3, 2026

Date
September 3, 2026 · 08:45 local
Place
Phoenix, AZ
Phase of flight
Other, Specify
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N480FT
NTSB investigation
NTSBWPR26LA328
Reported as
Bell OH-58A
Reported engine
Rolls-Royce 250-C20C
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
22,500 total

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.

PIC stated he and another pilot departed from Phoenix deer valley airport (dvt) to practice hovering autorotations. PIC completed one hovering autorotation followed by other pilot completing one. PIC stated that at approximately 0845 local time, he began the third hovering autorotation. PIC began the maneuver and at approximately 200 ft AGL at 60 KTS, PIC rolled throttle to full power and “joined the rotor RPM needle with the engines RPM needle”. PIC began flair at approximately 40-50 ft AGL and pulled in collective at approximately 10 ft AGL with the goal of settling at about a 3-5 ft AGL hover. During this, the low rotor RPM horn sounded, and PIC stated that he did not receive an engine response after increasing throttle. PIC then pulled in more collective resulting in an impact with the ground resulting in substantial damage to the aircraft. This resulted in the main rotor along with the tail rotor and gearbox separating from the aircraft.

The aircraft was recovered to a secure facility for further examination. Awaiting NTSB coordination with airframe and engine manufacturers to perform teardown. Report will be amended following teardown.

As the FAA filed it

PIC STATED HE AND ANOTHER PILOT DEPARTED FROM PHOENIX DEER VALLEY AIRPORT (DVT) TO PRACTICE HOVERING AUTOROTATIONS. PIC COMPLETED ONE HOVERING AUTOROTATION FOLLOWED BY OTHER PILOT COMPLETING ONE. PIC STATED THAT AT APPROXIMATELY 0845 LOCAL TIME, HE BEGAN THE THIRD HOVERING AUTOROTATION. PIC BEGAN THE MANEUVER AND AT APPROXIMATELY 200 FT AGL AT 60 KTS, PIC ROLLED THROTTLE TO FULL POWER AND “JOINED THE ROTOR RPM NEEDLE WITH THE ENGINES RPM NEEDLE”. PIC BEGAN FLAIR AT APPROXIMATELY 40-50 FT AGL AND PULLED IN COLLECTIVE AT APPROXIMATELY 10 FT AGL WITH THE GOAL OF SETTLING AT ABOUT A 3-5 FT AGL HOVER. DURING THIS, THE LOW ROTOR RPM HORN SOUNDED, AND PIC STATED THAT HE DID NOT RECEIVE AN ENGINE RESPONSE AFTER INCREASING THROTTLE. PIC THEN PULLED IN MORE COLLECTIVE RESULTING IN AN IMPACT WITH THE GROUND RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT. THIS RESULTED IN THE MAIN ROTOR ALONG WITH THE TAIL ROTOR AND GEARBOX SEPARATING FROM THE AIRCRAFT.

THE AIRCRAFT WAS RECOVERED TO A SECURE FACILITY FOR FURTHER EXAMINATION. AWAITING NTSB COORDINATION WITH AIRFRAME AND ENGINE MANUFACTURERS TO PERFORM TEARDOWN. REPORT WILL BE AMENDED FOLLOWING TEARDOWN.

NTSB investigation

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