Probable cause
Main rotor contact with the tail boom for unknown reasons, resulting in the separation of the tail boom.
NTSB analysis
The pilot and passenger were returning to their home airport after dropping off a family member at another airport. The passenger stated that the helicopter yawed to the right and began to spin out of control immediately before the accident. The helicopter descended and impacted into a canal, where it was located in about 20 ft of water.
Postaccident examination of the wreckage revealed evidence of main rotor contact with the tail boom, resulting the separation of a portion of the tail boom in flight. Separation of the tail boom, and the resultant loss of tail rotor thrust, would lead to a sudden right yaw, consistent with the passenger’s description. There was no evidence of a malfunction of the main rotor system, flight control system, or a loss of engine power that could have resulted in the main rotor’s contact with the tail boom. Because the helicopter was not equipped with, nor was required to be equipped with, a flight data recorder or a cockpit image recorder, the pilot’s flight control inputs leading up to the main rotor’s contact with the tail boom is unknown.
Text from the NTSB. Open the NTSB docket for ERA24FA075 for the full record.
Event
- Date
- Dec 27, 2023
- Type
- Accident
- Place
- Miami, Florida
- Nearest airport
- Miami Exec (TMB)
- Highest injury
- Fatal
- Fatal injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Hughes Helicopters Inc 369E
- N-number
- N757TB
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
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.