Probable cause
The pilot’s failure to maintain a proper autorotation profile during deceleration that resulted in the tail rotor assembly impacting the ground.
NTSB analysis
During a proficiency flight, the pilot was demonstrating an autorotation, and the nonflying pilot was following on the flight controls. While holding the flare to land, an excessive amount of aft cyclic was abruptly applied, and the tailskid and tail rotor contacted the ground. The pilot leveled the helicopter and completed the autorotation. The helicopter spun about 90° to the right before it came to a stop. The tail rotor assembly, tail boom, horizontal and vertical stabilizers, and tail rotor drive shaft couplings sustained substantial damage.
The operator reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation.
Text from the NTSB. Open the NTSB docket for WPR24LA028 for the full record.
Event
- Date
- Nov 6, 2023
- Type
- Accident
- Place
- Mesa, Arizona
- Nearest airport
- Falcon Fld (FFZ)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Md Helicopters Inc 369FF
- N-number
- N369FF
- Category
- Helicopter
- Year built
- 2009
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Other work use
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.