20020725022409A

Accident · Minor damage

FAA accident report · Bell 206L3 · July 25, 2002

Date
July 25, 2002 · 12:49 local
Operating rules
Air taxi and commuter (Part 135)
Operator
ALGA
Damage
Minor damage
Aircraft
N3174Y
NTSB investigation
NTSBFTW02LA217
Reported as
Bell 206L3
Fatal 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.

(-23) On July 25, 2002, at 1249 CDT, a Bell model 206-L3, N3174Y, registered to and operated by air logistics, l.l.c., air carrier certificate ALGA151C, experienced a loss of drive to the tail rotor assembly during cruise flight. The commercial pilot initiated an autorotational landing to the water where the helicopter rolled inverted upon landing. The commercially rated pilot and his one passenger received minor injuries upon exiting the helicopter. Visual meteorological conditions prevailed and company flight follwing was in effect. Investigation revealed #6 tail rotor shaft torsionallly fractured due to an as yet unknown object striking a tail rotor blade.

As the FAA filed it

(-23) ON JULY 25, 2002, AT 1249 CDT, A BELL MODEL 206-L3, N3174Y, REGISTERED TO AND OPERATED BY AIR LOGISTICS, L.L.C., AIR CARRIER CERTIFICATE ALGA151C, EXPERIENCED A LOSS OF DRIVE TO THE TAIL ROTOR ASSEMBLY DURING CRUISE FLIGHT. THE COMMERCIAL PILOT INITIATED AN AUTOROTATIONAL LANDING TO THE WATER WHERE THE HELICOPTER ROLLED INVERTED UPON LANDING. THE COMMERCIALLY RATED PILOT AND HIS ONE PASSENGER RECEIVED MINOR INJURIES UPON EXITING THE HELICOPTER. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND COMPANY FLIGHT FOLLWING WAS IN EFFECT. INVESTIGATION REVEALED #6 TAIL ROTOR SHAFT TORSIONALLLY FRACTURED DUE TO AN AS YET UNKNOWN OBJECT STRIKING A TAIL ROTOR BLADE.

NTSB investigation

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