20230820016009A

Accident · Substantial damage

FAA accident report · Rickey L Dyer SR AR-1 · Pecan Plantatio, TX · August 20, 2023

Date
August 20, 2023 · 08:00 local
Place
Pecan Plantatio, TX
Phase of flight
Takeoff: Rotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N57AR
NTSB investigation
NTSBCEN23LA386
Reported as
Rickey L Dyer SR AR-1
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
290 total30 in this make and model30 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.

Two independent witnesses stated the pilot started the takeoff roll with the rotor in a horizontal position, instead of pitched back as required for the rotor to store energy for flight. The witnesses both stated the takeoff roll was much longer than usual (1000+ feet), and when the pilot pitched the rotor up, the aircraft pitched up, gained about 30 to 40 feet above ground, rolled to the left, and impacted the runway. The left main wheel was broken off at the strut mount. The aircraft continued to roll to the left and the rotors contacted the ground. The fuselage departed the runway on its left side, trapping the pilot’s left arm under the rear windshield. The aircraft came to rest 1400 feet from the departure point of the runway.

As the FAA filed it

TWO INDEPENDENT WITNESSES STATED THE PILOT STARTED THE TAKEOFF ROLL WITH THE ROTOR IN A HORIZONTAL POSITION, INSTEAD OF PITCHED BACK AS REQUIRED FOR THE ROTOR TO STORE ENERGY FOR FLIGHT. THE WITNESSES BOTH STATED THE TAKEOFF ROLL WAS MUCH LONGER THAN USUAL (1000+ FEET), AND WHEN THE PILOT PITCHED THE ROTOR UP, THE AIRCRAFT PITCHED UP, GAINED ABOUT 30 TO 40 FEET ABOVE GROUND, ROLLED TO THE LEFT, AND IMPACTED THE RUNWAY. THE LEFT MAIN WHEEL WAS BROKEN OFF AT THE STRUT MOUNT. THE AIRCRAFT CONTINUED TO ROLL TO THE LEFT AND THE ROTORS CONTACTED THE GROUND. THE FUSELAGE DEPARTED THE RUNWAY ON ITS LEFT SIDE, TRAPPING THE PILOT’S LEFT ARM UNDER THE REAR WINDSHIELD. THE AIRCRAFT CAME TO REST 1400 FEET FROM THE DEPARTURE POINT OF THE RUNWAY.

NTSB investigation

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