20240614018579A

Accident · Substantial damage

FAA accident report · Eberhart Terry A ROTORWAY EXEC 162F · Alva, FL · June 14, 2024

Date
June 14, 2024 · 18:30 local
Place
Alva, FL
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N99TE
NTSB investigation
NTSBERA24LA263
Reported as
Eberhart Terry A Rotorway Exec 162F
Reported engine
Rotorway RW152
People aboard
2
Fatal injuries
0
Other injuries
0

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.

On June 14, 2024 an expiermental helicopter flew from , Alva, Florida to 87FL. After one pass of the airport the helicopter entered what was described as an loss of tail rotor effectiveness(lte) at approx. 100FT. Upon the emergency recovery of the lte event the helicopter set down on a canal berm and rolled into the canal near airport 87FL. The helocopter's main rotor blades, tail rotor blades, tail boom, and windshield were damaged substainaly. No injuries, 2 pilots on board exited the helicopter safely. Upon review of the bolt assembly in the tail boom on July 2 ,2024. The right side of the tail rotor drive belt jam nut had become loose more than 3 inches possibly from vibrations in the tail boom. This allowed the self-locking nylon nut to loosen approximately 3-4 full turns. This assembly in experimental helicopter rotorway exec 162F keeps tension on the pulley belt system that runs the tail rotor. Leading to an loss of tail rotor effectiveness.

As the FAA filed it

ON JUNE 14, 2024 AN EXPIERMENTAL HELICOPTER FLEW FROM , ALVA, FLORIDA TO 87FL. AFTER ONE PASS OF THE AIRPORT THE HELICOPTER ENTERED WHAT WAS DESCRIBED AS AN LOSS OF TAIL ROTOR EFFECTIVENESS(LTE) AT APPROX. 100FT. UPON THE EMERGENCY RECOVERY OF THE LTE EVENT THE HELICOPTER SET DOWN ON A CANAL BERM AND ROLLED INTO THE CANAL NEAR AIRPORT 87FL. THE HELOCOPTER'S MAIN ROTOR BLADES, TAIL ROTOR BLADES, TAIL BOOM, AND WINDSHIELD WERE DAMAGED SUBSTAINALY. NO INJURIES, 2 PILOTS ON BOARD EXITED THE HELICOPTER SAFELY. UPON REVIEW OF THE BOLT ASSEMBLY IN THE TAIL BOOM ON JULY 2 ,2024. THE RIGHT SIDE OF THE TAIL ROTOR DRIVE BELT JAM NUT HAD BECOME LOOSE MORE THAN 3 INCHES POSSIBLY FROM VIBRATIONS IN THE TAIL BOOM. THIS ALLOWED THE SELF-LOCKING NYLON NUT TO LOOSEN APPROXIMATELY 3-4 FULL TURNS. THIS ASSEMBLY IN EXPERIMENTAL HELICOPTER ROTORWAY EXEC 162F KEEPS TENSION ON THE PULLEY BELT SYSTEM THAT RUNS THE TAIL ROTOR. LEADING TO AN LOSS OF TAIL ROTOR EFFECTIVENESS.

NTSB investigation

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