20020524023659A

Accident · Substantial damage

FAA accident report · Bell 206L1 · Ftlauderdale, FL · May 24, 2002

Date
May 24, 2002 · 13:00 local
Place
Ftlauderdale, FL
Operating rules
Air taxi and commuter (Part 135)
Operator
P8HA
Damage
Substantial damage
Aircraft
N80PH
NTSB investigation
NTSBMIA02FA100
Reported as
Bell 206L1

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) Power turbine section of engine failed inflight. Pilot heard loud bang while flying along the beach. Pilot performed an autorotation and did a hard landing on the beach. Pilot evacuated the aircraft along with his passenger. No apparent injuries. The landing gear skids broke off, the pilot's chin bubble was cracked, the tail boom was bent and an engine fire was evident. Engine cowling, the fuselage, and one main rotor blade were damaged by flying turbine blades.

As the FAA filed it

(-23) POWER TURBINE SECTION OF ENGINE FAILED INFLIGHT. PILOT HEARD LOUD BANG WHILE FLYING ALONG THE BEACH. PILOT PERFORMED AN AUTOROTATION AND DID A HARD LANDING ON THE BEACH. PILOT EVACUATED THE AIRCRAFT ALONG WITH HIS PASSENGER. NO APPARENT INJURIES. THE LANDING GEAR SKIDS BROKE OFF, THE PILOT'S CHIN BUBBLE WAS CRACKED, THE TAIL BOOM WAS BENT AND AN ENGINE FIRE WAS EVIDENT. ENGINE COWLING, THE FUSELAGE, AND ONE MAIN ROTOR BLADE WERE DAMAGED BY FLYING TURBINE BLADES.

NTSB investigation

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